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EMB-500 AND EMB-505 FSB Report Revision 2 09/15/2010

FLIGHT STANDARDIZATION BOARD REPORT

EMBRAER- EMPRESA BRASILEIRA de AERONAUTICA S.A. MODELS EMB-500 and EMB-505

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DATE: 09/15/2010

DOUGLAS L. EDWARDS CHAIRMAN, EMBRAER PHENOM FLIGHT STANDARDIZATION BOARD

FEDERAL AVIATION ADMINISTRATION KANSAS CITY AIRCRAFT EVALUATION GROUP, MKC-AEG

901 LOCUST, ROOM 332 KANSAS CITY, MISSOURI 64106

TELEPHONE: (816) 329-3233

FAX: (816) 329-3241


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MANAGEMENT COORDINATION

____________________________________________ _______________________ Walter J. Hutchings Date Manager, Kansas City Aircraft Evaluation Group ____________________________________________ ________________________ John S. Duncan Date Manager, Air Transportation Division, AFS-200 ____________________________________________ ________________________ Mel O. Cintron Date Manager, General Aviation and Commercial Division, AFS-800


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TABLE OF CONTENTS REVISION RECORD ..............................................................................................................................................4

PURPOSE AND APPLICABILITY .......................................................................................................................5 BACKGROUND .....................................................................................................................................................8

PILOT TYPE RATING DETERMINATION .....................................................................................................13

MASTER COMMON REQUIREMENTS (MCR’S) ..........................................................................................17

FSB SPECIFICATIONS FOR INITIAL TRAINING.........................................................................................21

FSB SPECIFICATIONS FOR TRANSITION TRAINING...............................................................................26 FSB SPECIFICATIONS FOR INITIAL CHECKING ...........................................................................................29 Transition Checking Credit ..................................................................................................................................29 FSB SPECIFICATIONS FOR CURRENCY .........................................................................................................31 FSB SPECIFICATIONS FOR DEVICES AND SIMULATORS............................................................................31

OPERATOR DIFFERENCE REQUIREMENTS (ODRS) TABLES................................................................31 MISCELLANEOUS...............................................................................................................................................32 AIRCRAFT REGULATORY COMPLIANCE........................................................................................................34

ALTERNATE MEANS OF COMPLIANCE TO THIS REPORT....................................................................35

APPENDIX A1 - AIRCRAFT REGULATORY COMPLIANCE CHECKLIST, EMBRAER EMB-500.......1

DEFINITIONS..........................................................................................................................................................1

APPENDIX A2 - AIRCRAFT REGULATORY COMPLIANCE CHECKLIST, EMBRAER EMB-505.....73 APPENDIX C – ODR TABLES .................................................................................................................................1


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REVISION RECORD REVISION NUMBER

SECTION

PAGE NUMBERS

DATE

Original

All

All

1/14/2009

1 All All updated to include results of EMB-505 Flight Standardization Board

2/16/2010

2 Miscellaneous Page 33. Includes results of Class III Electronic Flight Bag Electronic Charts application evaluation.

09/15/2010


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PURPOSE AND APPLICABILITY The primary purpose of this Flight Standardization Board (FSB) Report is to specify FAA training, checking and currency requirements applicable to flight crews operating the Embraer Model 500,Phenom 100, and Model 505, Phenom 300, airplanes. This report provides guidance to operators who will be operating the EMB-500 or EMB-505 under Title 14 Code of Federal Regulations (14 CFR) Part 91, Subpart K of Part 91, and Part 135. The guidelines in this report apply to operations inspectors, principal operations inspectors (POIs), training center program managers (TCPM’s), and aircrew program managers (APM’s). This report also applies to 14 CFR 135 air carrier check airmen and instructors, airline transport pilots instructing in air transportation service, certificated flight instructors, aircrew program designees, training center evaluators (TCE’s), and 14 CFR Part 61, 135, 141 and 142 training providers. This FSB Report has been written in accordance with the requirements of Advisory Circular (AC) 120-53A. The contents of this FSB report are applicable on the effective date of its final approval and will remain effective unless amended, superseded, or withdrawn by subsequent FSB determinations. NOTE: The EMB-500 and EMB-505 meet the minimum equipment and instrumentation requirements of 14 CFR Part 135 for operations conducted with a single pilot. ACRONYMS Relevant acronyms used in this FSB Report, the Embraer Airplane Flight Manual, Quick Reference Handbooks, Pilot Operating Handbooks, and other operational documents are described below. 14 CFR Title 14 Code of Federal Regulations AC Advisory Circular ACO Aircraft Certification Office ACP Autopilot Control Panel ADC Air Data Computer ADS Air Data System AEG Aircraft Evaluation Group AEO All Engines Operating AFM Airplane Flight Manual AFS Autoflight System AGL Above Ground Level AHRS Attitude Heading Reference System A-I Anti-Ice AMS Air Management System


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ANAC Agencia National de Aviacao Civil AOA Angle of Attack AP or A/P Autopilot APM Aircrew Program Manager ATP Airline Transport Pilot ATR Automatic Thrust Reserve CAS Crew Alerting System CHDO Certificate Holding District Office CPT Cockpit Procedures Trainer CRM Crew Resource Management DME Distance Measuring Equipment EASA European Aviation Safety Agency EFIS Electronic Flight Information System ELOS Equivalent Level of Safety FAA Federal Aviation Administration FADEC Full Authority Digital Engine Controller FAR Federal Aviation Regulation FCSOV Flow Control Shutoff Valve FMA Flight Mode Annunciator FMS Flight Management System FSB Flight Standardization Board FSDO Flight Standards District Office FTD Flight Training Device GIA Garmin Integrated Avionics GPS Global Positioning System GPU Ground Power Unit ICAO International Civil Aviation Organization IFR Instrument Flight Rules ILS Instrument Landing System ITT Interturbine Temperature IESI Integrated Electronic Standby Instrument KIAS Knots Indicated Airspeed KOEL Kinds of Operation List MCRs Master Common Requirements MCT Maximum Continuous Thrust MDRs Master Difference Requirements MFD Multifunction Display MKC-AEG Kansas City Aircraft Evaluation Group NSP National Simulator Program OAT Outside Air Temperature ODRs Operator Difference Requirements OPERA Optimized Performance Analyzer PRSOV Pressure Regulator Shutoff Valve PFD Primary Flight Display PIC Pilot in Command


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PNF Pilot Not Flying POI Principal Operations Inspector PTS Practical Test Standards QRH Quick Reference Handbook RAIM Receiver Autonomous integrity Monitoring RVSM Reduced Vertical Separation Minimum SIC Second in Command SPWS Stall Protection and Warning system TAS Traffic Advisory System TIS Terrain Information System TCDS Type Certificate Data Sheet TCE Training Center Evaluator TLA Thrust Lever Angle Vac Approach Climb Speed Vap Approach Speed Vfs Final Segment Airspeed Vfe Maximum Flap Extended Airspeed Vle Maximum Landing Gear Extended Airspeed Vlo Maximum Landing Gear Operating Airspeed Vmca Minimum Control Airspeed in the Air Vmcg Minimum Control Airspeed on Ground Vmcl Minimum Control Airspeed During Landing Vmo Maximum Operating Airspeed Va Design Maneuvering Speed Vr Rotation Speed Vref Reference Landing Airspeed Vs Stall Speed Vso Stall Speed –Landing Configuration Vyse Single Engine Best Rate of Climb V1 Critical Engine Failure Speed YD Yaw Damper


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BACKGROUND EMBRAER- EMPRESA BRASILEIRA de AERONAUTICA S.A., the Manufacturer, is headquartered in Sao Jose dos Campos, Sao Paulo state, Brazil. EMB-500 The Embraer Model 500 (EMB-500), also called the PHENOM 100, is a low wing, T-tail and pressurized airplane, powered by two high by-pass ratio rear mounted turbofan engines. The tricycle landing gear is fully retractable, with single tire at each leg, to be operated on paved runways only. A glass cockpit panel has been developed with highly integrated onboard avionics. The passenger configuration consists of two seats abreast (one to each side of the aisle, aka: club seating) which allows carrying up to 5 passengers if the aircraft is operated single pilot and using the copilot seat as a passenger seat. The Embraer Model 500 is a twin-engine turbofan airplane certified in accordance with 14 CFR Part 23, in the normal category with Special Conditions requiring commuter category takeoff and landing performance. It is listed on Federal Aviation Administration (FAA) Type Certificate Data Sheet (TCDS) Number A59CE as the Model EMB-500. Embraer received their FAA type certificate on 12/12/2008. The airplane has 1160 NM range utilizing NBAA criteria with high speed cruise of .70 Mach. Takeoff field length is listed as 3, 400 feet with a landing distance of 2,699 feet. The minimum crew determination listed in the airplane flight manual (AFM) and on the TCDS is one pilot in the left seat. AFM limitations authorize a single pilot provided there is an operative autopilot. The pilot must utilize an operative headset mounted microphone. If either the autopilot or microphone is not operative, the EMB-500 must have a crew comprised of one pilot and one copilot. The EMB-500 is certified for Day, Night, VFR and IFR flight conditions to a maximum operating altitude of 41,000 feet, and is approved for flight into reduced vertical separation minimum (RVSM) airspace if the aircraft meets the minimum equipment requirements contains in the Aircraft Flight Manual, Supplement 1. The EMB-500 is also approved for flight into known icing conditions. The EMB-500 base model has a maximum certificated takeoff weight of 10, 472 pounds and a maximum landing weight of 9, 766 pounds. All models of the EMB-500 have a total seating density of up to six, with two crew seats and four passenger seats (standard). The aircraft is powered by two Pratt & Whitney, PW617F-E engines, each producing approximately 1, 700 pounds of thrust. Engines are controlled by two dual-channel, full authority digital engine controller (FADEC) units. Engines received type certification by Transport Canada and FAA on October 3, 2008. The EMB-500 fuselage and major structural components are aluminum, and the aircraft employs conventional, mechanical flight controls. There are two ram’s horn controls mounted in the center at each pilot station.


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The aircraft fuel system is a pressurized wet-wing design. Total fuel capacity is 2,850 pounds with 2,806 pounds usable. The EMB-500 relies on dual Garmin Integrated Avionics (GIA) units and an electronic power distribution system to control, monitor, and power its systems and components. The two GIA’s and all electronic aircraft system buses and components, are interwoven and fully integrated. The two GIA’s in the EMB-500 each have independent architecture for redundancy to ensure availability for several important aircraft support functions, including the autoflight system (AFS). The AFS consists of an autopilot and autotrim system, flight director, yaw damper, stall warning and stick pusher, the flight mode annunciation (FMA) and crew alerting system (CAS) message reporting. A takeoff configuration system evaluates elevator trim position, parking brake, and flap status before activating a “TAKEOFF OK” aural alert. The Prodigy Avionics System was developed by Embraer and Garmin Corporation for use in the EMB-500. It consists of two primary flight displays (PFD) and one multifunction display (MFD). Each PFD receives information from its Garmin Integrated Avionics unit. A typical EMB-500 panel layout is shown below. EMB-505 Embraer Model 505 (EMB-505), also called the PHENOM 300, is a low wing, T-tail and pressurized airplane, powered by two high by-pass ratio rear mounted turbofan engines. It retains the same fuselage cross section as the EMB-500 but is 9 feet 3 inches longer than the EMB-500. It also has 27.5 degrees of swept wing with winglets. The EMB-505 utilizes a moveable stabilizer. The cockpit displays significant commonality with the EMB-500. An additional panel has been added for the hydraulic pump control. The EMB-505 has two engine driven hydraulic pumps in lieu of a single electrically operated hydraulic pack. A panel has been added to control the Left and Right Pneumatic Bleed Systems. The EMB-505 uses hot bleed air to anti-ice the Wing and Horizontal Stabilizer. A fuel cross feed knob has been added to replace the fuel transfer button/switch. Additional test features have been added to the Test panel to test the Smoke Detector and Ice Protection Systems required by the certification rules and the ice protection.. The lighting panel has been modified to accommodate the Emergency Lights required of Commuter Category airplanes. The cabin has two rows of seats on each side of the aisle, (aka: club seating), two additional forward facing seats aft of the club seating arrangement, and an optional aft facing seat forward of the club seats aft of the in-flight entertainment/galley. Maximum seating configuration is 8 passengers if the aircraft is operated single pilot and using the copilot seat as a passenger seat. The Embraer Model 505 is a twin-engine turbofan airplane certified in accordance with 14 CFR Part 23, in the Commuter Category via an exemption. It is listed on Federal Aviation Administration (FAA) Type Certificate Data Sheet (TCDS) as the Model EMB-505. Embraer received their FAA type certificate on 12/14/2009.


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The airplane has 1800 NM range utilizing NBAA criteria with high speed cruise of .78 Mach. Takeoff field length is listed as 3, 700 feet with a landing distance of 2,315 feet. The automatic spoiler greatly enhances the stopping distance. The minimum crew determination listed in the airplane flight manual (AFM) and on the TCDS is one pilot in the left seat. AFM limitations authorize a single pilot provided there is an operative autopilot and flight director. The pilot must utilize an operative headset mounted microphone. If the autopilot, microphone, or flight director is not operative, the EMB-505 must have a crew comprised of one pilot and one copilot. The EMB-505 is certified for Day, Night, VFR and IFR flight conditions to a maximum operating altitude of 45,000 feet, and is approved for flight into Reduced Vertical Separation Minimum (RVSM) airspace if the aircraft meets the minimum equipment requirements contained in the Aircraft Flight Manual, Supplement 1. Although certified, this does not constitute operational approval which must be obtained by each operator via procedures contained in FAA handbook 8900.1. The EMB-505 is approved for flight into known icing conditions. The EMB-505 base model has a maximum certificated takeoff weight of 17, 968 pounds and a maximum landing weight of 16,865. The aircraft is powered by two Pratt & Whitney, PW535-E engines, each producing approximately 3,360 pounds of thrust. Engines are controlled by two dual-channel, full authority digital engine controller (FADEC) units. Engines received type certification by Transport Canada and the FAA. The EMB-505 fuselage and major structural components are aluminum, and the aircraft employs conventional, mechanical flight controls. The aircraft has a spoiler/speedbrake system installed that consists of two panels on each upper wing. The spoiler automatically deploys upon landing with no pilot action required. Speed brakes can not be operated coincidentally with the wing flaps. Like the EMB-500, there are two ram’s horn controls mounted in the center at each pilot station. The aircraft fuel system is a pressurized wet-wing design. Total fuel capacity is 5401 pounds with 5352 pounds usable. The EMB-505 relies on dual Garmin Integrated Avionics (GIA) units and an electronic power distribution system to control, monitor, and power its systems and components. The two GIA’s and all electronic aircraft system buses and components, are interwoven and fully integrated. The two GIA’s in the EMB-505 each have independent architecture for redundancy to ensure availability for several important aircraft support functions, including the autoflight system (AFS). The AFS consists of an autopilot and autotrim system, flight director, yaw damper, stall warning and stick pusher, the flight mode annunciation (FMA) and crew alerting system (CAS)


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message reporting. The Yaw Damper function is provided by either the yaw damper or ventral rudder system. A takeoff configuration system evaluates elevator trim position, parking brake, speed brake, and flap status before activating a “TAKEOFF OK” aural alert. The Prodigy Avionics System was developed by Embraer and Garmin Corporation for use in the EMB-500. It consists of two primary flight displays (PFD) and one multifunction display (MFD). Each PFD receives information from its Garmin Integrated Avionics unit. The system synoptic pages have been modified from the earlier EMB-500 airplanes but this modification will be incorporated into the EMB-500 in subsequent software revisions to the Prodigy System. A typical EMB-500 and EMB-505 panel layout is shown below.


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PILOT TYPE RATING DETERMINATION In accordance with 14 CFR Parts 1 and 61, two pilot type rating designations have been established. The pilot type rating designation for the EMB-500 airplane is “EMB-500”. An applicant who satisfactorily completes the practical test in this aircraft will receive an EMB-500 type rating on their airman certificate. The pilot type rating designation for the EMB-505 airplane is “EMB-505”. An applicant who satisfactorily completes the practical test in this aircraft will receive an EMB-505 type rating on their airman certificate. FSB Evaluations The FSB conducted a comparison between the EMB-500 and the EMB-505. An FSB for the EMB-500 was convened in September 2008, first at CAE SimuFlite at DFW, Texas and then relocated to Araraquarra, S. P., Brazil at the Embraer flight test facility to evaluate the EMB-500 via the T-5 test process described in Advisory Circular 120-53. In accordance with 14 CFR Parts 1 and 61, the pilot type rating designation for the EMB-500 model is EMB-500. An FSB for the EMB-505 was convened at CAE SimuFlite at DFW, Texas November 16, 2009. The FSB evaluated the EMB-505 in accordance with T-5 test process described in AC 120-53A in order to determine if a shortened transition course was appropriate for pilots transitioning from the EMB-500 to the EMB-505. FSB pilots first received recurrent training and checking in the EMB-500 airplane followed by ground and flight training in the EMB-505 airplane. A complete flight check for the EMB-505 pilot type rating was conducted by each FSB member in accordance with Airline Transport Pilot and Pilot Type Rating Practical Test Standard. Applicants transitioning from the EMB-500 to the EMB-505 may be eligible for training and checking credits in accordance with the respective paragraphs below. No person may receive the additional pilot rating without demonstrating competence in the respective airplane. EMB-500 The EMB-500 type rating is approved for pilots who satisfactorily complete the type rating practical test in the EMB-500 as a single pilot. A pilot with the EMB-500 type rating may operate the aircraft as a single pilot, or operate as a pilot in command (PIC) with a second in command (SIC) on the aircraft. A pilot with the EMB-500 type rating must have a SIC in the aircraft if it lacks an operative autopilot system, headset mounted microphone, or flight director. AFM Limitations require a SIC under these conditions. If this circumstance arises, the PIC must comply with the PIC proficiency check requirements specified by 14 CFR Section 61.58, and use a SIC that meets the qualification and training requirements of 14 CFR Section 61.55.


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EMB-500, Second in Command Required The EMB-500 type rating with a Second in Command Required limitation is approved for applicants who satisfactorily complete the type rating practical test in the EMB-500 while using a SIC. The limitation “Second in Command Required” will be placed on their airman certificate. A pilot with an EMB-500 type rating with the Second in Command Required limitation must operate the aircraft with a SIC who meets the minimum qualification and training requirements of 14 CFR Section 61.55, or have another pilot as SIC, who holds an EMB-500 type rating. In addition, the holder of an EMB-500 type rating with the Second In Command Required limitation, may not act as PIC of the EMB-500 unless, within the preceding 12 calendar months, he or she has satisfactorily completed an annual proficiency check in the EMB-500, or an aircraft requiring more than one crewmember, as required by 14 CFR Section 61.58 (a) (1) or (2). The holder of an EMB-500 type rating with the Second in Command Required limitation may have the limitation removed in accordance with guidance contained in FAA Order 8900.1, Volume 5, Chapter 2, paragraph, 5-729. To remove the limitation, it is not necessary to complete the entire practical test as a single pilot. All areas of operations/tasks approved for a flight simulator may be accomplished in that flight simulator for the purpose of removing the “Second-in-Command Required” limitation. Areas of operation include the following:

· Preflight Procedures Tasks: All. · Takeoff and Departure Phase Tasks: All. · In-flight Maneuvers Tasks: C, E, F. · Instrument Procedures Tasks: All. · Landings and Approaches to Landing Tasks: All. · Normal and Abnormal Procedures. · Emergency Procedures. · Postflight Procedures Tasks: All.

Additional areas include:

Collision Avoidance.· Communication Management.· Instrument Flight Rules (IFR) Cross-Country Flight Plan Avionics Loading.

After satisfactorily completing this practical test, the airman is granted the EMB-500 type rating and the limitation “Second in Command Required” is removed in accordance with 14 CFR Section 61.43 (b). EMB-505


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The EMB-505 type rating is approved for pilots who satisfactorily complete the type rating practical test in the EMB-505 as a single pilot. A pilot with the EMB-505 type rating may operate the aircraft as a single pilot, or operate as a pilot in command (PIC) with a second in command (SIC) on the aircraft. A pilot with the EMB-505 type rating must have a SIC in the aircraft if it lacks an operative autopilot system, headset mounted microphone, or flight director. AFM Limitations require a SIC under these conditions. If this circumstance arises, the PIC must comply with the PIC proficiency check requirements specified by 14 CFR Section 61.58, and use a SIC that meets the qualification and training requirements of 14 CFR Section 61.55. EMB-505, Second in Command Required The EMB-505 type rating with a Second in Command Required limitation is approved for applicants who satisfactorily complete the type rating practical test in the EMB-505 while using a SIC. The limitation “Second in Command Required” will be placed on their airman certificate. A pilot with an EMB-505 type rating with the Second in Command Required limitation must operate the aircraft with a SIC who meets the minimum qualification and training requirements of 14 CFR Section 61.55, or have another pilot as SIC, who holds an EMB-505 type rating. In addition, the holder of an EMB-505 type rating with the Second In Command Required limitation, may not act as PIC of the EMB-505 unless, within the preceding 12 calendar months, he or she has satisfactorily completed an annual proficiency check in the EMB-505, or an aircraft requiring more than one crewmember, as required by 14 CFR Section 61.58 (a) (1) or (2). The holder of an EMB-505 type rating with the Second in Command Required limitation may have the limitation removed in accordance with guidance contained in FAA Order 8900.1, Volume 5, Chapter 2, paragraph, 5-729. To remove the limitation, it is not necessary to complete the entire practical test as a single pilot. All areas of operations/tasks approved for a flight simulator may be accomplished in that flight simulator for the purpose of removing the “Second-in-Command Required” limitation. Areas of operation include the following:

· Preflight Procedures Tasks: All. · Takeoff and Departure Phase Tasks: All. · In-flight Maneuvers Tasks: C, E, F. · Instrument Procedures Tasks: All. · Landings and Approaches to Landing Tasks: All. · Normal and Abnormal Procedures. · Emergency Procedures. · Postflight Procedures Tasks: All.

Additional areas include:


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Collision Avoidance.· Communication Management.· Instrument Flight Rules (IFR) Cross-Country Flight Plan Avionics Loading.

After satisfactorily completing this practical test, the airman is granted the EMB-505 type rating and the limitation “Second in Command Required” is removed in accordance with 14 CFR Section 61.43 (b). EMB-500 and EMB-505 TRAINING PROGRAMS DESCRIPTION Embraer developed their training program for EMB-500 and EMB-505 pilots before any simulator was available, and all FSB and initial cadre and customer training was completed in the EMB-500 and EMB-505 airplanes. SIC training is mandatory under 14 CFR Section 61.55 for any airman, who will be serving as a SIC in the EMB-500 or EMB-505 or, when the operation requires a SIC due to a Second in Command Required limitation on the airman certificate of the PIC, or when an autopilot is not installed in the EMB-500 or 505, or is not operative. However, SIC familiarization training, required by 14 CFR Section 61.55, would not apply if the SIC holds a type rating in the EMB-500 or EMB-505,as appropriate, or is a qualified SIC in the EMB-500 or EMB-505, as appropriate, under 14 CFR Part 91 Subpart K, or Part 135. The FSB is responsible for completing evaluations of future changes to the EMB-500 and EMB-505 derivative or variant models. Other aircraft changes that the FSB may need to evaluate include, but are not limited to, engine changes, systems and instrumentation changes, and the installation of new systems. The FSB will determine the impact of future installations on training, checking and currency and revise this FSB Report as needed.


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MASTER COMMON REQUIREMENTS (MCR’s) MCR’s are requirements applicable to crew qualification which pertain to all variants of the same type or related types. This section lists all MCR’s identified by the FSB for the EMB-500 and EMB-505. MCR’s are requirements applicable to crew qualification which pertain to all variants of the same type or related types. TAKEOFFS – All takeoffs should be made with maximum power to ensure the automatic thrust reserve (ATR) system automatically arms. The use of the ATR is limited to 10 minutes. The use of maximum takeoff power in the EMB-500 and EMB-505 are restricted to five minutes. Takeoffs should be made with flaps set at the takeoff setting, Flaps 1 or Flaps 2. Pilots should be aware of the performance differences between the two takeoff configurations. . CLIMB, CRUISE AND APPROACH PROFILES – Climb, cruise and approach flight profiles, flap settings, and recommended or maximum airspeeds for the EMB-500 are accomplished in accordance with the following tables:

CLIMB AIRSPEED Normal Climb 160 KIAS At Transition Level 200 KIAS

DESCENT/APPROACH VFR MAXIMUM AIRSPEED VFE – Flaps 1 200 KIAS VFE – Flaps 2 180 KIAS VFE Flaps 3 or Full 145 KIAS VLO/VLE 250/275 KIAS

Climb, cruise and approach flight profiles, flap settings, and recommended or maximum airspeeds for the EMB-505 are accomplished in accordance with the following tables:

CLIMB AIRSPEED Normal Climb 180 KIAS At Transition Level 230 KIAS

CRUISE MAXIMUM AIRSPEED VMO 275 KIAS MMO .70 Mach


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DESCENT/APPROACH VFR MAXIMUM AIRSPEED VFE – Flaps 1 180 KIAS VFE – Flaps 2 170 KIAS VFE Flaps 3 or Full 170 KIAS VLO/VLE 250/250 KIAS

IFR APPROACH/LANDING MINIMA – In accordance with 14 CFR Section 97.3, the aircraft approach category is based on 1.3 times the stall speed in the landing configuration (Vso) at maximum certificated landing weight. Based on this criterion, the EMB-500 has a reference landing speed (VREF) of 102 KIAS. The EMB-505 used a Vref of 1.35 Vs. Based upon this the EMB-505 has a reference landing speed of 120 KIAS.

Straight in Approaches – At the maximum aircraft landing weight, with flaps in the

landing position, is used in training by EMB and is recommended by the FSB as listed in the following table.

AIRCRAFT SPEED FLAP POSITION APPROACH CATEGORY 100 KIAS Landing Flaps Category B

Circling Approaches – A minimum of 120 KIAS for all circling approaches with flaps

set in Flaps 2 position is used in training by Embraer and is recommended by the FSB during the circling maneuver. On the turn to final, the flaps should be set to landing Flaps Full position and the aircraft should be slowed to the recommended Vref speed. Single engine circling maneuvers may be trained and checked at the discretion of the training provider and/or examiner based on weight, altitude, temperature and conditions of flight.

However, when determining circling approach minima, all minimums are based on the

highest airspeed used during the circling maneuver. This will ensure that the aircraft will have adequate obstacle clearance in the maneuvering area. The minimum visibility for the circling maneuver is listed in the following table and increases with airspeed due to the increase in circling approach radii.

SPEED/CATEGORY VISIBILITY IN STATUTE MILES

Less than 91 KIAS/Cat A 1 Mile 91 to 120 KIAS/Cat B 1 Mile 121 to 140 KIAS/Cat C 1 and ½ Miles 141 to 165 IAS/Cat D 2 Miles 165 KIAS and Above/Cat E 3 Miles

CRUISE MAXIMUM AIRSPEED VMO 320 KIAS MMO .78 Mach


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LANDINGS – The FSB found no unusual landing characteristics in the EMB-500 or EMB-505. The FSB agrees that all landings should be at a slow airspeed since there are no drag devices on the EMB-500 other than flaps and brakes. The EMB-505 utilizes an automatic spoiler. Both airplanes have brakes with anti-skid protection. REJECTED LANDINGS – Rejected landings can be trained and checked with two engines operative, or one engine inoperative, following the procedures established by Embraer or other training provider. Pilots should be aware of the increased performance of the EMB-505 in both the single and two engine operation go-arounds. In the EMB-505 care must be taken not to exceed the 180 KIAS flaps 1 speed limitation. NO FLAP APPROACHES – No Flap approaches and landings were evaluated by the FSB and can be safely accomplished during training and checking. It is important to note that the final approach speed with flaps in the UP position is Vref + 30, and additional runway length, approximately 1.9 times the Vref Full Flap landing distance is required. Bank angle in both the EMB-500 and the EMB-505 is limited to 20 degrees. This results in a greater turn radius and as such it is improbable that a No Flap circling approach can be conducted without exceeding the protected obstruction area. STEEP TURNS – Steep turns must be trained and checked at 180 KIAS in the EMB-500 with a power setting of 68 to 72 N1, depending on aircraft weight, altitude and atmospheric conditions. Steep turns in the EMB-505 are recommended to be conducted at 200 KIAS. Note that some degree of roll spoiler deflection is achieved in the EMB-505 in bank angles exceeding 35 degrees. Roll spoilers will be activated in the EMB-505 during steep turns. There is no abrupt pitch change or roll when they activate. STALLS – The EMB-500 and the EMB-505 were found to have stall characteristics during flight testing which as a 14CFR Part 23 certification requirement, required a stick pusher system to be installed to mitigate these characteristics. The stick pusher in the EMB-500 is electric whereas the stick pusher in the EMB-505 is hydraulic. The EMB-505 stick pusher activation was demonstrated to be effective but less aggressive than in the EMB-500. The stick pusher in the EMB-505 must be tested before each flight after engine start. The EMB-500 sick pusher still must be tested before each flight but because it is electric it may be tested prior to engine start. The EMB-500 has no unusual stall characteristics if stall recovery is initiated at the first indication of a stall, which is well above an aerodynamic stall. The stall speed in the clean configuration, with 0 degrees angle of bank is 100 KIAS. In the landing configuration, with gear and flaps fully extended with 0 degrees of bank, the stalling speed is 77 KIAS. The FSB noted that at low altitudes stall recovery can be completed with minimal altitude loss if initiated at the first indication of a stall, which is the aural stall warning and the stall warning visual indication on the PFDs.


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An aerodynamic stall occurs at the same approximate airspeed as stick pusher activation. If the stick pusher activates, the loss of altitude during the stall recovery will be 300 to 500 feet. As a consequence, flight crews, training personnel and evaluators should be aware of the consequences of low altitude stalls. The FSB did not evaluate stalls at high altitudes. Stalls at high altitudes may require much greater loss of altitude than stalls at low altitude. The EMB-505 has no unusual stall characteristics if stall recovery is initiated at the first indication of a stall. A slight buffet may be felt before the aural stall warning is activated. The FSB noted that stall recovery at low altitude can be completed with minimal altitude loss if initiated at the first indication of a stall, which is the aural stall warning and the stall warning visual indication on the PFDs. Recovery at the first indication of buffet is also acceptable. An aerodynamic stall occurs at the same approximate airspeed as stick pusher activation. If the stick pusher activates, the loss of altitude during the stall recovery will be less than in the EMB-500. The FSB did not evaluate stalls at high altitudes. Stalls at high altitudes may require much greater loss of altitude than stalls at low altitude. UNUSUAL ATTITUDES – Unusual attitudes may be trained and checked in the aircraft as long as the induced pitch and bank remain within the parameters for non-acrobatic flight. EMERGENCY DESCENTS – It is recommended that emergency descents during training and checking in the aircraft be done at a maximum descent speed of 170 KIAS in the EMB-500 rather than 275 KIAS, which is specified in the AFM emergency procedures, and is the aircraft VMO, due to gear operating and extension speeds. Both VLE and VLO is 250 KIAS in the EMB-505 and emergency descents may be conducted to this speed. ENGINE SHUTDOWNS IN FLIGHT – For an intentional engine shutdown in flight, the throttle of the selected engine should be at idle for 2 minutes prior to shutdown and prior to selecting the engine Start/Stop knob to OFF. An airspeed allowing for a successful engine air start should be maintained for the weight/altitude/temperature condition as illustrated in the Engine Air Start Envelope in Section 3 of the AFM and the QRH. It is important to emphasize that the FADEC limiting protections are not available during an in-flight engine restart. After shutdown, the engine ITT should be permitted to cool to 100 degrees C before attempting a restart. The engine should be operated at Idle for an additional 2 minutes prior to applying engine thrust. SIMULATED ENGINE FAILURES – It is recommended that simulated engine failures be accomplished with the use of the throttle unless the aircraft is at least 3,000 feet above ground level (AGL) near a suitable airport.


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FSB SPECIFICATIONS FOR INITIAL TRAINING An applicant for an EMB-500 or the EMB-505 type rating at the ATP certificate level must meet the training requirements of 14 CFR Section 61.157 (b) or (c). For the addition of an EMB-500 or EMB-505 type rating to a pilot certificate other than at the ATP level, an applicant must meet the training requirements of the applicable sections of 14 CFR Section 61.63 (d) or (e). All initial training for the purpose of obtaining an EMB-500 or EMB-505 type rating is at Level E and in accordance with the table below:

EMB-500 OR EMB-505 INITIAL TYPE RATING

TRAINING HOURS

Aircraft Systems Ground Training See FAA Order 8900.1, Volume 3, Chapter 19, Section 5, Paragraph 3-1200, table 3-52.

Systems Integration Training 12.0 Hours Flight Training See FAA Order 8900.1,

Volume 3, Chapter 19, Section 6, Paragraph 3-1230, tables 3-60 and 3-61.

Specific recommendations regarding training in the EMB-500 and EMB-505 for ground training, cockpit integration, flight training and special emphasis training are listed below. Ground Training The FSB evaluated the ground portion of the Embraer EMB-500 type rating program in the original FSB and recommends that approved ground training curriculums and guidance regarding deviations from National Norms conform to the National Norms contained in FAA Order 8900.1, Volume 3, Chapter 19, Section 5, paragraph 3-1200, table 3-52. For the purposes of the tables, inspectors should use the Part 135 Transport and Commuter Category Family of Aircraft. This category is appropriate due to the complexity of turbojet operations and the fact that although the EMB-500 is certificated as a 14 CFR 23 Normal Category it was required to comply with the Commuter Category Takeoff and Landing Performance requirements of 14 CFR 23. The EMB-505 was certificated in the Commuter Category.


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FLIGHTCREW AIRCRAFT GROUND TRAINING HOURS NATIONAL NORMS (THRESHOLDS)

CATEGORY OF TRAINING Family of Aircraft Initial

New Hire Initial Equipment

Transition Upgrade Recurrent

Part 135 Transport and Commuter Category 72(56) 64(48) 64(48) (16) 16(8)

Initial Ground training for the EMB-500 or EMB-505 in the following subject areas is required:

a) Single Pilot Crew Resource Management b) Risk Assessment c) AFM Review d) Aircraft Limitations e) Aircraft Performance, Performance Airspeeds and Flight Profiles f) Requirement for and use of OPERA g) Weight and Balance h) Aircraft Maintenance and use of MMEL i) Aircraft General Description j) Prodigy Integrated Avionics Suite k) Aircraft Computer System l) Air Data System and AHRS m) Aircraft Engines, FADEC and ATR n) Electronic Power Distribution System o) PFD Displays and Controls p) MFD Displays and Controls q) CAS Messaging System r) System Synoptic Pages s) Warning Systems and Takeoff Configuration Protection t) Flight Controls u) Auto Flight System v) Landing Gear and Brakes w) Fuel System x) Pneumatics y) Pressurization System z) Air Conditioning aa) Oxygen System bb) Ice and Rain Protection cc) Fire Protection System dd) Preflight Procedures ee) Normal Procedures ff) Abnormal and Emergency Procedures


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gg) Generator Failure hh) DME Systems ii) RVSM Equipment Requirements and Effects of their failure on RVSM

Capability jj) Optional Systems Operation including Weather Radar, TAS and TAWS

Systems Integration Training (IPT, CPT, FTD, Simulator or Aircraft) The FSB recommends a minimum of twelve (12.0) hours of systems integration training in an approved IPT, CPT, FTD, simulator, or aircraft for all pilots undergoing initial training. These modules may be integrated in the type rating program during ground training at the discretion of Embraer, or other training provider, and should include an emphasis on the following tasks:

a. PFD/MFD Preflight Setup b. Cockpit Checklist Flow c. Instrument Approach Tuning and Setup d. Communication Tuning and Setup e. Analysis of System Synoptic Pages f. Use of Keyboard g. CAS Messaging System h. Setup of the Autopilot Control Panel (ACP) i. PFD Flight Mode Annunciations j. Programming of FMS k. Abnormal and Emergency Procedures l. Use of Composite Mode m. Generator and Electrical Bus Failures n. Prodigy Avionics System o. Optional Systems Operation including Weather Radar, TAS, TAWS

Flight Training (Approved Simulators or Aircraft) The FSB recommends that approved flight training curriculums and guidance regarding deviations from National Norms conform to the National Norms contained in FAA Order 8900.1, Volume 3, Chapter 19, Section 6, paragraph 3-1230. Table 3-60 should be used when training two pilots and table 3-61 used when a single pilot is trained. For the purposes of these tables, inspectors should use the Part 135 Transport and Commuter Category Family of Aircraft. This category is appropriate due to the complexity of turbojet operations and the fact that although the EMB-500 is certificated as a 14 CFR 23 Normal Category it was required to comply with the Commuter Category Takeoff and Landing Performance requirements of 14 CFR 23. The EMB-505 was certificated in the Commuter Category. Pertinent parts of these tables, and guidance regarding the crediting of training hours and crew pairing, current at the time of this report, are included below.


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Flight Training Hours (National Norms) Two Pilots—Flight Training Device and/or Flight Simulator

Family of Aircraft Initial New-Hire Initial Equipment Transition Upgrade Recurrent Part 135 Transport and Commuter Category

PIC - 24 SIC - 24 PIC - 20 SIC - 20 PIC - 20 SIC - 20 SIC TO PIC 8 PIC - 4 SIC – 4

NOTE: When flight training is conducted in a flight simulator or training device, it is acceptable and preferable for the flight training curriculum segment to be developed so that two pilots can be trained during a single flight training session. This includes the training of a PIC and SIC, two PICs, or two SICs at the same time. During this type of training, one pilot (pilot A) manipulates the controls of the aircraft while the other pilot (pilot B) performs the duties of the “pilot-not-flying” (PNF) the aircraft. During the same training session, the pilots reverse roles. Pilot B manipulates the controls, and pilot A performs the duties of the PNF. The duties of the PNF are typically included in the operator’s aircraft operating manuals and/or in the maneuvers and procedures document. These duties include normal, abnormal, and emergency duties (that are performed by the PNF) and the crew participation activities (crew resource management (CRM) concepts) used by the operator. Both pilots are receiving essential “crew-concept” training throughout the training session. Therefore, the total training hours accomplished during the training session can be credited to each of the participating pilots. For example, if a PIC and an SIC participated in a 4-hour flight simulator session, both pilots would receive 4 hours of training credit. This method of crediting training hours is valid only when both student pilots manipulate the controls for approximately equal amounts of time. This method of crediting training hours is not valid when the instructor is providing instruction and also is occupying one of the pilot seats of the flight simulator, flight training device,

Flight Training Hours (National Norms) One Pilot—Flight Training Device and/or Flight Simulator or When All Training is Conducted in an Aircraft

CATEGORY OF TRAINING Family of Aircraft

Initial New-Hire Initial Equipment

Transition Upgrade Recurrent

Part 135 Transport and Commuter Category

PIC - 12 SIC - 12

PIC - 10 SIC - 10

PIC - 8 SIC - 8 SIC TO PIC 6 PIC - 4 SIC - 4

Flight training for all pilots who complete the EMB-500 or EMB-505 type rating course in the airplane or simulator and should include training in the following:

a. Exterior Preflight Inspection b. Cockpit/Cabin Setup c. Aircraft Systems Tests and Checks d. Before Takeoff Procedures e. Pitch Attitude, Power Settings and Airspeed Combinations


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f. Basic and Advanced Flight Maneuvers Required for EMB-500 or EMB-505 Practical Test

g. Aircraft Traffic Pattern Operations h. Departure and Arrival Procedures i. Instrument Approaches, Missed Approach Procedures and Holding j. Engine Failure on Takeoff (i.e. V1 Cut) k. Engine Shutdown and Restart l. Single Engine Approach and Landing from Precision/Non-Precision Approaches m. Circling Approach Procedures n. Single Engine Missed Approaches o. No Flap Circling Approach p. No Flap/Partial Flap Landings q. Enroute and High Altitude Operations r. Loss of Pressurization and Use of Oxygen s. Emergency Descents t. Abnormal and Emergency Procedures u. Specific Avionics System Emergencies v. Loss of MFD/PFD w. Optional Systems Operations including Weather Radar, TAS and TAWS

Special Emphasis Training Special emphasis training includes systems or procedures training elements that are unique to the aircraft and should be given a higher degree of emphasis than regular training. The FSB has identified the following training items that are either unique to the EMB-500 or EMB-505, based on installed systems and equipment, or are important because of operational aspects associated with a single pilot crew, or flight crews with a low level of prior operating experience. Ground Training

a. High Altitude Physiology b. Donning of Oxygen Masks c. Single Pilot Resource Management, Risk Assessment and Risk Management d. Abnormal and Emergency Procedures, focusing on Avionics and Electronic Power

Distribution Systems e. Stick Pusher System f. Emergency Gear System g. Use of Backup Trim h. Operations in Icing Conditions including Handling Qualities i. OPERA


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Systems Integration Training (IPT, CPT, FTD, Simulator, or Aircraft)

a. Use of PFD, MFD and Composite Mode b. Setup of the Flight Director and Autopilot Control Panel c. Use of Keyboard d. Prodigy System Integration Training e. CAS Logic and Abnormal Procedures Training f. Avionics System Abnormal and Emergency Procedures g. Programming of FMS, (when installed) h. Donning of Oxygen Masks i. Use of Alternate Trim

Flight Training (Approved Simulator or Aircraft)

a. Use of PFD, MFD and Composite Mode b. Instrument Approaches with PFD/MFD in Composite Mode c. Use of CAS Messaging System d. High Altitude Single Pilot Operations e. Loss of all DC Power and Effect on the Aircraft f. Other Electrical System Malfunctions g. Donning of Oxygen Masks h. Use of Emergency Gear System i. Stick Pusher System j. Use of Alternate Trim k. Operations in Icing Conditions including Handling Qualities l. High Speed Approaches at Air Carrier Airports

FSB SPECIFICATIONS FOR TRANSITION TRAINING EMB-500 to EMB-505 Transition As a part of the T-5 test the FSB evaluated Embraer’s proposed ground and flight training for applicants for the EMB-505 pilot type rating for applicants that already hold the EMB-500 pilot type rating. As a result of that evaluation the FSB recommends the following:


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PREREQUISITES To be eligible for a reduced transition training qualification programs, 14 CFR Part 91 operators must meet the following: HOLD AS A MINIMUM A PRIVATE PILOT CERTIFICATE WITH EMB-500 PILOT TYPE RATING

– BE IFR CURRENT – EMB-500 RATED WITHIN LAST 12 MONTHS, OR – 61.58, 135.293, or 91.1065 CURRENT IN EMB-500, OR – 25 HOURS IN EMB-500 WITHIN LAST 6 MONTHS

GROUND TRAINING 14CFR Part 91 Operators Qualifying in Accordance with 14CFR Sections 61.63 or 61.157 8 hours of ground training is recommended as the minimum requirement. All system differences should be covered at Level B, assisted training. Special emphasis should be on the new systems, hydraulics, pneumatics, flight controls, and anti ice systems normal, abnormal, and emergency procedures. System controls and operations should be emphasized. Additionally OPERA and flight planning differences should be emphasized. Dimensions, weights, speeds, limitations should be trained but may be at a minimum Level A difference level. 14CFR Part 135 and 14CFR Subpart 91K operators POI’s of may approve reduced ground training in accordance with the ODR tables attached in Appendix C. FLIGHT TRAINING 14CFR Part 91 operators may be eligible for reduced flight training provided the following E Level Maneuvers are trained to proficiency: E LEVEL MANUEVERS

– NORMAL TAKEOFF – STALLS – V1 CUT – SINGLE ENGINE ILS – SINGLE ENGINE MISSED APPROACH – TWO ENGINE MISSED APPROACH – LANDING OR BALKED LANDING FROM A CIRCLING APPROACH – NO FLAP BALKED LANDING – NO FLAP APPROACH – SINGLE ENGINE LANDING FROM AN ILS

The FSB recommends that three two hour flights be accomplished when transitioning from the EMB-500 to EMB-505. POI’s of 14CFR Part 135 and 14CFR Part 91K operators may approve reduced flight training hours in approved operator training programs provided the above E Level maneuvers are trained to proficiency.


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EMB-505 to EMB-500 Transition The FSB recommends the following: PREREQUISITES To be eligible for reduced training transition qualification programs, 14 CFR Part 91 operators must meet the following: HOLD AS A MINIMUM A PRIVATE PILOT CERTIFICATE WITH EMB-505 PILOT TYPE RATING

– BE IFR CURRENT – EMB-505 RATED WITHIN LAST 12 MONTHS, OR – 61.58 ,135.293, or 91.1065 CURRENT IN EMB-505, OR – 25 HOURS IN EMB-505 WITHIN LAST 6 MONTHS

GROUND TRAINING 8 hours is recommended as the minimum requirement. All system differences should be covered at Level B, assisted training. Special emphasis should be on the new systems, hydraulics, pneumatics, flight controls, and anti ice systems normal, abnormal, and emergency procedures. System controls and operations should be emphasized. Additionally OPERA and flight planning differences should ne emphasized. Dimensions, weights, speeds, limitations should be trained but may be at a Level A difference level. POI’s of 14CFR Part 135 and 14CFR Subpart 91K operators may approve reduced ground training in accordance with the ODR tables attached in Appendix C. FLIGHT TRAINING 14CFR Part 91 operators may be eligible for reduced flight training provided the following E Level Maneuvers are trained to proficiency: E LEVEL MANUEVERS

– NORMAL TAKEOFF – STALLS – V1 CUT – SINGLE ENGINE ILS – SINGLE ENGINE MISSED APPROACH – TWO ENGINE MISSED APPROACH – LANDING OR BALKED LANDING FROM A CIRCLING APPROACH – NO FLAP BALKED LANDING – NO FLAP APPROACH – SINGLE ENGINE LANDING FROM AN ILS

The FSB recommends that at least a two hour flight be accomplished when transitioning from the EMB-505 to EMB-500. POI’s of 14CFR Part 135 and 14CFR Subpart 91K operators may approve reduced flight training hours in approved operator training programs provided the above E Level maneuvers are trained to proficiency.


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Special Flight Characteristics The FSB has identified a special flight characteristic in the EMB-500 and EMB-505 that all training providers and flight crews should be aware of. That special characteristic is the stick pusher system. The FSB recommends that all pilots in EMB-500 and EMB-505 training programs practice and demonstrate this system in flight, or in a simulator, and understand that an altitude loss in a stall can be significant if the stick pusher activates. In aircraft training, the FSB recommends that this training be conducted during the clean configuration stall maneuver. Be advised an altitude loss of 400-500 feet can be expected at low altitude and a secondary stall is routine on the first attempt. FSB SPECIFICATIONS FOR INITIAL CHECKING All checking required by 14 CFR Section Part 61.58, Subpart K of Part 91, and 14 CFR Part 135 is at Level E. All type rating checks required by 14 CFR Section s 61.63 or 61.157 and pilot proficiency checks required by 14 CFR Section 61.58 will be administered in accordance with the ATP and Type Rating Practical Test Standard (PTS). Satisfactory completion of an ATP practical test in the EMB-500 or EMB-505, or the addition of a EMB-500 or EMB-505 type rating to an existing ATP certificate, may be simultaneously credited for a competency check or instrument-proficiency check, as applicable, in accordance with 14 CFR Part 135 or Subpart K of Part 91, for pilots who have completed the air carrier’s, or fractional ownership company’s approved training program. Transition Checking Credit 14CFR Part 91 applicants for an EMB-505 pilot type rating conducted in accordance with 14CFR section 61.63 or 61.157 should receive no credit for maneuvers previously checked in the EMB-500 pilot type rating practical test. 14CFR Part 91 applicants for an EMB-500 pilot type rating conducted in accordance with 14CFR section 61.63 or 61.157 should receive no credit for maneuvers previously checked in the EMB-505 pilot type rating practical test. 14 CFR Part 91 applicants must accomplish a complete practical test in all Areas of Operation required by the PTS for a pilot type rating. POI’s of 14CFR Part 135 and Subpart 91K applicants may approve qualification programs that allow checking credits to applicants that have successfully completed the EMB-500 or EMB-505 practical test when transitioning to the other model. At a minimum an applicant for an EMB-505 or EMB-500 pilot type rating that already holds the EMB-500 or EMB-505 pilot type rating should be current and qualified in the operator’s approved program to act as Pilot in Command of the base model and demonstrate competence in the following maneuvers during the practical test for the additional pilot type rating being added:


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– NORMAL TAKEOFF – STALLS – V1 CUT – SINGLE ENGINE ILS – SINGLE ENGINE MISSED APPROACH – TWO ENGINE MISSED APPROACH – LANDING OR BALKED LANDING FROM A CIRCLING APPROACH – NO FLAP BALKED LANDING – NO FLAP APPROACH

Considerations for Checking in the Aircraft The FSB has identified special considerations connected with the administration of a type rating practical test in the EMB-500 or EMB-505 airplane.

1. As a general practice, the FSB recommends that examiners not pull CBs during the administration of a practical test since pulling certain CBs may induce the unwanted loss of other equipment due to the complexity of systems integration.

2. Activation of the emergency gear system should not be accomplished in the aircraft during checking. If the emergency gear system is activated the aircraft must be landed and inspected in accordance with the EMB-500 or EMB-505 Airplane Maintenance Manual.

3. Due to automatic APR functions, when closing one or both throttles during takeoff and immediately resuming takeoff with full power, the APR is ON.

4. Completing an actual engine shutdown and restart in flight disables the FADEC automatic protection feature. For practice engine restarts, examiners must monitor all engine restart indications and must be prepared to manually shut down the engine before any limitations are exceeded. Additionally, after shutdown the engine ITT should be permitted to cool to 100 degrees C before attempting a restart. The engine should be operated at Idle for an additional 2 minutes prior to applying engine thrust above idle.

5. 5. No-Flap landings may be evaluated in the aircraft and are required by FAA Order 8900.1 for 14 CFR Part 135 PIC checks. Partial or no-flap landings are also required by the Airline Transport Pilot/Type Rating PTS. If checked in the aircraft, the examiner or FAA Inspector must be attentive to the flight crew’s airspeed control and available runway length and surface condition. FAA Order 8900.1 allows the examiner or inspector to accept a no-flap landing without an actual touchdown for 14CFR Part 135 PIC checks if, in their opinion, a safe touchdown and landing to a full stop could be made.


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FSB SPECIFICATIONS FOR CURRENCY Currency will be maintained or reestablished in accordance with the requirements of 14 CFR Sections 61.55, 61.56, 61.57, 61.58 or 135.247, as applicable. All currency requirements are at Level E, which mandates that currency be accomplished in the EMB-500 or EMB-505 model or an approved EMB-500 or EMB-505 Level C or Level D simulator. Because the EMB-500 and the EMB-505 are different and separate pilot type ratings, currency is specific to each model. No credit is allowed for takeoffs or landing accomplished between the two aircraft. PIC currency will apply equally whether the pilot holds an EMB-500 or EMB-500, Second in Command Required, on their airman certificate or EMB-505, or EMB-505, Second in Command Required. FSB SPECIFICATIONS FOR DEVICES AND SIMULATORS All requests for the use of training devices or flight simulators in an operator’s training program, or at a 14CFR Part 142 approved training center, 14CFR Part 141 approved school, or other training provider, should be addressed to the appropriate FSDO. Requests for device or simulator approval should be made through the POI. Guidance is available in AC 120-40B, AC 120-45A and FAA Order 8900.1. POI’s should seek additional assistance through the FAA’s National Simulator Program (NSP) Office. The training, checking, and currency requirements of 14 CFR Part 61, Part 91 Subpart K and Part 135, as well as the ATP/Type Rating PTS, allow partial or full credit in approved training devices and flight simulators. Embraer has partnered with a 14 CFR Part 142 training provider for type rating training. MASTER DIFFERENCE REQUIREMENTS (MDRs) MDR’s are requirements applicable to crew qualification, which pertain to differences between variants of the same or related type. MDR requirements apply when differences between a base aircraft and a variant, or differences between two variants, affect flight crew knowledge, skills, or abilities related to flight safety at differences levels of Level A or greater. MDR Tables for the EMB-505 and EMB-500 are contained in Appendix B. OPERATOR DIFFERENCE REQUIREMENTS (ODRs) TABLES ODR’s are operator specific requirements necessary to address differences between a base aircraft and one or more variants in a transition or differences training program that lists compliance methods relative to training, checking and currency. ODR tables consist of design, maneuver and system difference tables.


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Difference Levels A through E in the ODR tables using the minimum training methods devices and equipment are described in the table below:

A Self Instruction “HO” = Handout, Bulletins, Manual Revisions

B Aided Instruction “S/T” = Slide/Tape presentations “CBT” = Computer Based Training “SU” = Stand-up Lectures “VT” = Video Tapes

C System Devices “ICBT” = Interactive Computer Based Training “CSS” = Cockpit System Simulators “CPT” = Cockpit Procedures Trainers “PTT” = Part Task Trainers “FTD 2-5” = Flight Training Devices (level 2-5)

D Maneuver Devices “FTD 6-7” = Flight training devices (level 6-7) “FFS A-D” = Full Flight Simulators (level D or lower )

E Simulator C or D, or Aircraft

“FFS C-D” = Full Flight Simulators (level C or D) “ACFT” = Aircraft

NOTE: An “X” in an ODR table column indicates that any of the training methods for that level are acceptable. If a specific instruction method is specified in an ODR table column, it must be used. ODR checking and currency level definitions may be found in AC 120-53.

ODR tables are an acceptable means to comply with MDR requirements based on those differences and the compliance methods shown. FSB recommended ODR tables are described in Appendix C. MISCELLANEOUS PROVING TESTS – Proving tests, which may be required by an operator to comply with the requirements of 14 CFR Section 135.145, should be conducted in accordance with FAA Order 8900.1, Volume III, Chapter 29. FORWARD OBSERVER SEAT – A forward observer seat on or near the flight deck, equipped with a headset or speaker, is required to be provided for use by the Administrator during enroute inspections by 14 CFR Section 135.75 (b) and for the administration of flight tests leading to pilot certification or operating privileges. On small jet aircraft type certificated in accordance with 14 CFR Section Part 23, there generally is no available space for the installation of a jump seat that will meet the intent of the applicable regulations.


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The right cockpit seat is the primary seat in the EMB-500 or EMB-505 that will substitute as a jump seat for the purposes of the 14CFR cited above. If the right pilot seat is occupied, an inspector will be required to sit in the nearest available seat in the cabin to perform enroute inspections or to administer a flight check if communications, oxygen, adequate lighting and ventilation are available. The aft facing passenger seat behind the passenger entry door on the aircraft left side was evaluated and considered acceptable by the FSB team. ELECTRONIC CHECKLIST- An Electronic Checklist (ECL) was included as part of the original certification of the EMB-505 and retrofitted in the EMB-500 via a Supplemental Type Certificate (STC). The checklist is viewable on the Multifunction Display. It is of the open loop type as the pilot or crewmember must acknowledge the accomplishment of all checklist items. All Normal, Abnormal, and Emergency Procedures contained in the Quick Reference Handbook are included. There are some variations of format but the information is functionally identical. The ECL was evaluated in accordance with guidance contained in Advisory Circular 120-64 and found to be compliant. The information contained in the ECL can not be modified by the operator. It is not integrated into any aircraft systems or the Crew Alerting System. Operators must continue to have the paper back up checklist available. POI’s should review AC 120-64 for Training, Checking, and Currency requirements prior to issuing operational approval for the use of the ECL by the operator’s crews. 14CFR Part 91 operators may develop training, checking, and currency requirements and ECL procedures without any additional FAA involvement. ELECTRONIC CHARTS-Three electronic chart applications have been evaluated: SafeTaxi, FliteCharts, and ChartView. SafeTaxi is provided by Garmin as standard equipment on the Phenom 100 and Phenom 300. SafeTaxi may be viewed on the MFD or on the inset screen of either PFD. The scale is changed using the range control knob. Safe Taxi is an enhanced feature that gives greater map detail as the map range is adjusted on the airport. When zoomed in (using the range and pan control knob) close enough, the airport runways (with numbers), taxiways (with identifying letters), buildings and in some cases, hot spots are displayed.The aircraft symbol moves over the airport diagram as the airplane is taxied. The SafeTaxi database covers over 700 US airports. It is updated on a 56-day cycle and always available after the expiration date. Garmin intends on having every airport in the US with a control tower in the SafeTaxi database FliteCharts are a paper version of the National Aeronautical Charting Office procedure charts and provided by Garmin. FliteCharts are:

Displayed on MFD. Have a 28 day revision cycle. Inoperative 180 days after chart expiration date. Not available outside the US. Subscription to the FliteChart service is required. FliteCharts do not have a moving display. It is an electronic display of the paper

chart.


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ChartView is the electronic version of Jeppesen terminal procedures charts. ChartView is:

Displayed on MFD as moving map. Has a 14 day revision cycle. Inoperative 70 days after chart expiration date. Chart databases are available by subscription from Jeppesen, Inc. Included

charts are: • Arrivals (STAR) • Departure Procedures (DP) • Approaches • Airport Diagrams • NOTAMs

The FSB recommends the following training: As an Interim Solution (until Web Based Training is developed) - Differences Training Module: Ground school 1 hour Desktop trainer 1/2 hour Simulator 1 hour Final Solution - Differences Training Module: Web Based Training + Simulator (All sessions) No specific checking or currency is required. AIRCRAFT REGULATORY COMPLIANCE The Aircraft Regulatory Compliance Checklist is of benefit to the FAA Certificate Holding District Office (CHDO) and assigned principal inspectors, because it identifies regulatory and operational requirements for which compliance has already been demonstrated to the FAA for a particular type aircraft or variant model. It is the responsibility of the CHDO to review compliance with FAA rules, policies and processes not covered by the Regulatory Compliance Checklist before the EMB-500 or EMB-505 is introduced into commercial service. At the time of the T-5 test no production airplane was available for the FSB to evaluate. The attached checklist, Appendix A, provides Embraer’s proposal of how the airplane type design complies with the operating rules. Various specifics (i.e. Placards, operational and maintenance documents to be supplied at the time of delivery) have yet to be confirmed by the FSB and the comment “TBD” is placed in the FSB Comment column. .


35

ALTERNATE MEANS OF COMPLIANCE TO THIS REPORT The FSB chairman should be consulted by the POI when alternate means of compliance, other than those specified in this report, are proposed. The FAA General Aviation and Commercial Division, AFS-800, or the FAA Air Transportation Division, AFS-200, must approve alternate means of compliance. If an alternate means of compliance is sought, operators will be required to submit a proposed alternate means for approval that provides an equivalent level of safety to the provisions of AC 120-53 and this FSB Report. Analysis, demonstrations, proof of concept testing, differences documentation, and/or other evidence may be required.


A-1

APPENDIX A1 - AIRCRAFT REGULATORY COMPLIANCE CHECKLIST, EMBRAER EMB-500

DEFINITIONS

Compliant: The compliance with referred item is OPERATOR’s responsibility and EMBRAER provides necessary equipment / feature / manual / information in order to

support the OPERATOR to comply with referred statement.

Not Compliant: The compliance with referred item is OPERATOR’s responsibility and EMBRAER does not provide necessary equipment / feature / manual /

information to support the OPERATOR to perform the referred operation.

Optionally Compliant: The compliance with referred item is OPERATOR’s responsibility and EMBRAER provides necessary equipment / feature / manual /

information as optional item(s) under OPERATOR’s request to support the OPERATOR to perform the referred operation.

Not Applicable: The item is not applicable to this EMBRAER aircraft model.

Operator’s Responsibility: The compliance with referred item is exclusively OPERATOR’s responsibility and there are no EMBRAER actions.

Definition: The item is a definition statement, no actions are required.

Title Only: The item is subdivided and individual sub-items analyses are presented subsequently.


A-2

EMB-500, Part 91 Compliance

Subpart A - General

ITEM TITLE COMPLIANCE REMARKS FSB FINDING

91.1 Applicability. Definition

-

Agree

91.3 Responsibility and authority of the pilot in command.

Operator’s Responsibility

-

Agree

91.5 Pilot in command of aircraft requiring more than one required pilot.


-

Agree

91.7 Civil aircraft airworthiness. Operator’s Responsibility

-

Agree

91.9 Civil aircraft flight manual, marking, and placard requirements.

Title Only

-

Required Placards and their location in AFM, MM? TBD

91.9(a) Requires operation according to AFM and Marking & Placards


-

91.9(b) Requires an AFM (or Operation Manual) on board

Compliant

EMBRAER will furnish one updated AFM copy for each factory delivered airplane.

TBD

91.9(c) Compliance with aircraft identification requirements of FAR 45

Compliant

All markings required by part 45 of this chapter are installed.

TBD

91.9(d) Helicopter operation Not Applicable

Applicable only to Helicopter Operation.

Agree

91.11 Prohibition on interference with crewmembers.


-

Agree

91.13 Careless or reckless operation. Operator’s Responsibility

-

Agree

91.15 Dropping objects. Operator’s Responsibility

-

Agree


A-3


91.17 Alcohol or drugs. Operator’s Responsibility

-

Agree

91.19 Carriage of narcotic drugs, marihuana, and depressant or stimulant drugs or substances.


-

Agree

91.21 Portable electronic devices. Operator’s Responsibility

-

Agree. PED light provided in Cabin.

91.23 Truth-in-leasing clause requirement in leases and conditional sales contracts.


-

Agree

91.25 Aviation Safety Reporting Program: Prohibition against use of reports for enforcement purposes.

Definition

-

Agree

EMB-500, Part 91 Compliance Subpart B - Flight Rules



-

Agree

91.103 Preflight action. Operator’s Responsibility

-

Agree

91.105 Flight crewmembers at stations. Compliant

All flight crew member stations are provided with the adequate restrain system according to FAR 23.785

Agree

91.107 Use of safety belts, shoulder harnesses, and child restraint systems.

Compliant

EMB-500 is provided with pilot and co-pilot seats inside the cockpit area, provided with 5-point restraint system; and passenger seats inside the cabin area, provided with 3-points restraint system.

TBD

91.109 Flight instruction; Simulated instrument flight and certain flight tests.


-

Agree

91.111 Operating near other aircraft. Operator’s Responsibility

-

Agree


A-4


91.113 Right-of-way rules: Except water operations. Operator’s Responsibility

-

Agree

91.115 Right-of-way rules: Water operations. Not Applicable

Applicable only for aircraft operating on the water.

Agree

91.117 Aircraft speed. Operator’s Responsibility

-

Agree

91.119 Minimum safe altitudes: General. Operator’s Responsibility

-

Agree

91.121 Altimeter settings. Operator’s Responsibility

-

Agree

91.123 Compliance with ATC clearances and instructions.


-

Agree

91.125 ATC light signals. Definition

-

Agree

91.126 Operating on or in the vicinity of an airport in Class G airspace.


-

Agree

91.127 Operating on or in the vicinity of an airport in Class E airspace.


-

Agree

91.129 Operations in Class D airspace. Operator’s Responsibility

-

Agree

91.130 Operations in Class C airspace. Operator’s Responsibility

-

Agree

91.131 Operations in Class B airspace. Operator’s Responsibility

-

Agree

91.133 Restricted and prohibited areas. Operator’s Responsibility

-

Agree

91.135 Operations in Class A airspace. Operator’s Responsibility

-

Agree


A-5


91.137 Temporary flight restrictions in the vicinity of disaster/hazard areas.


-

Agree

91.138 Temporary flight restrictions in national disaster areas in the State of Hawaii.


-

Agree

91.139 Emergency air traffic rules. Operator’s Responsibility

-

Agree

91.141 Flight restrictions in the proximity of the Presidential and other parties.


-

Agree

91.143 Flight limitation in the proximity of space flight operations.


-

Agree

91.144 Temporary restriction on flight operations during abnormally high barometric pressure conditions.


-

Agree

91.145 Management of aircraft operations in the vicinity of aerial demonstrations and major sporting events.


-

Agree

91.146 Passenger-carrying flights for the benefit of a charitable, nonprofit, or community event.

Definition

-

Agree

91.147 Passenger carrying flights for compensation or hire.


-

Agree

91.151 Fuel requirements for flight in VFR conditions.


-

Agree

91.153 VFR flight plan: Information required. Operator’s Responsibility

-

Agree

91.155 Basic VFR weather minimums. Operator’s Responsibility

-

Agree

91.157 Special VFR weather minimums. Operator’s Responsibility

-

Agree


A-6


91.159 VFR cruising altitude or flight level. Operator’s Responsibility

-

Agree

91.167 Fuel requirements for flight in IFR conditions.


-

Agree

91.169 IFR flight plan: Information required. Operator’s Responsibility

-

Agree

91.171 VOR equipment check for IFR operations. Operator’s Responsibility

-

Agree

91.173 ATC clearance and flight plan required. Operator’s Responsibility

-

Agree

91.175 Takeoff and landing under IFR. Operator’s Responsibility

-

Agree

91.177 Minimum altitudes for IFR operations. Operator’s Responsibility

-

Agree

91.179 IFR cruising altitude or flight level. Operator’s Responsibility

-

Agree

91.180 Operations within airspace designated as Reduced Vertical Separation Minimum airspace.


-

Agree

91.181 Course to be flown. Operator’s Responsibility

-

Agree

91.183 IFR radio communications. Operator’s Responsibility

-

Agree

91.185 IFR operations: Two-way radio communications failure.


-

Agree

91.187 Operation under IFR in controlled airspace: Malfunction reports.


-

Agree

91.189 Category II and III operations: General Not Applicable Aircraft do not have Cat II or Cat III Capabilities. Agree


A-7


operating rules.

91.191 Category II and Category III manual. Not Applicable

Aircraft do not have Cat II or Cat III Capabilities.

Agree

91.193 Certificate of authorization for certain Category II operations.

Not Applicable

Aircraft do not have Cat II Capability.

Agree

EMB-500, Part 91 Compliance Subpart C - Equipment, Instrument, and Certificate Requirements


91.201 [Reserved] Not Applicable

Item is Reserved - no requirement

Agree

91.203 Civil aircraft: Certifications required. Title Only

-

Agree

91.203(a) Civil aircraft: Certification documents required.


-

Agree

91.203(b) Civil aircraft: Experimental operation Operator’s Responsibility

-

Agree

91.203(c) Fuel tanks installed inside PAX or baggage compartments


-

Agree

91.203(d) Compliance with FAR Part 34 required Compliant

The PW617F-E engine will be certified to FAR 33 (Engine Type Certificate) Amendment 20 and the emission requirements are specified in AWM 516 (change 516-7. This is equivalent to FAR Part 34 up to and including Amendment 3), which points to the ICAO annex 16 standards.

Agree

91.205 Powered civil aircraft with standard category U.S. airworthiness certificates: Instrument and equipment requirements.

Title Only

-

Agree

91.205(a) General: Instruments and equipment must be adequate for each type of operation.


-

Agree


A-8


91.205(b) Visual flight rules (day) - VFR Title Only

-

Agree

91.205(b)(1) Visual flight rules (day) - VFR: Airspeed indicator

Compliant

Compliance is through one Primary Flight Display and one Air Data System.

Agree

91.205(b)(2) Visual flight rules (day) - VFR: Altimeter Compliant


Agree

91.205(b)(3) Visual flight rules (day) - VFR: Magnetic direction indicator

Compliant

Compliance is through one Primary Flight Display and one AHRS.

Agree

91.205(b)(4) Visual flight rules (day) - VFR:Tachometer for each engine

Compliant

There is engine parameters indication (N1 and N2) on MFD.

Agree

91.205(b)(5) Visual flight rules (day) - VFR: Oil pressure gauge for each engine using pressure system

Compliant

There is an oil pressure indication on MFD.

Agree

91.205(b)(6) Visual flight rules (day) - VFR: Temperature gauge for each liquid-cooled engine

Not Applicable

EMB-500 does not have a liquid-cooled engine.

Agree

91.205(b)(7) Visual flight rules (day) - VFR: Oil temperature gauge for each air-cooled engine

Compliant

There is an oil temperature indication on MFD.

Agree

91.205(b)(8) Visual flight rules (day) - VFR: Manifold pressure gauge for each altitude engine

Not Applicable

Applicable only for aircraft equipped with an altitude engine.

Agree

91.205(b)(9) Visual flight rules (day) - VFR: Fuel gauge indicating the quantity of fuel in each tank

Compliant

EMB-500 fuel system provides fuel quantity indication for each tank show in the Multifunction Display (MFD) - EIS

Agree

91.205(b)(10) Visual flight rules (day) - VFR: Landing gear position indicator

Compliant

Compliance is in the Multifunction Display (MFD) - EIS screen using the data sent by the Landing Gear System.

Agree

91.205(b)(11) Visual flight rules (day) - VFR: Anti-collision light system for small aircraft certified according to part 23.

Compliant

The EMB-500 aircraft is equipped with approved Anti-collision lights.

Agree

91.205(b)(12) Visual flight rules (day) - VFR: Approved Not Compliant The life vests are offered optionally. Agree


A-9


flotation gear readily available to each occupant.

Pyrotechnic signaling devices are not offered.

91.205(b)(13) Visual flight rules (day) - VFR: An approved safety belt with an approved metal-to-metal latching device for each occupant 2 years of age or older.

Compliant

Each seat is provided with a metal-to-metal latch device, as according with requirement 23.785(b).

TBD

91.205(b)(14) Visual flight rules (day) - VFR: Shoulder harness for small aircraft certified according to part 23.

Compliant

Cockpit seats are provided with 5-points restraint system, with a fuselage-mounted shoulder harness, designed to protect the occupant from serious head injury when the occupant experiences the ultimate inertia forces specified in Sec. 23.561(b)(2). According to requirement 23.785(e), each crewmember seated with restraint system fastened is able to perform all functions necessary for flight operations.

TBD

91.205(b)(15) Visual flight rules (day) - VFR: An emergency locator transmitter, if required by §91.207.

Compliant

EMB-500 has an ELT installed.

Agree

91.205(b)(16) Visual flight rules (day) - VFR: For normal, utility, and acrobatic category airplanes with a seating configuration, excluding pilot seats, of 9 or less.

Compliant

All seats comply with requirement 23.785(g). 23.785(h) is not applicable since EMB-500 is a normal category aircraft.

Agree

91.205(b)(17) Visual flight rules (day) - VFR: Shoulder harness - Rotorcraft

Not Applicable

Applicable only for rotorcraft manufactured after September 16, 1992.

Agree

91.205(c) Visual flight rules (night) - VFR Title Only

-

Agree

91.205(c)(1) Visual flight rules (night) - VFR: Instruments and equipment specified in paragraph (b) of this section.

Compliant

Item 91.205(b) compliance checked by certification

Agree

91.205(c)(2) Visual flight rules (night) - VFR: Approved position lights.

Compliant

EMB-500 is equipped with approved Position lights.

Agree

91.205(c)(3) Visual flight rules (night) - VFR: An approved aviation red or aviation white anti-collision light system.

Compliant

EMB-500 is equipped with approved Anti-collision lights.

Agree

91.205(c)(4) Visual flight rules (night) - VFR: Electric landing light.

Compliant

EMB-500 is equipped with two wing root Landing Lights.

Agree

91.205(c)(5) Visual flight rules (night) - VFR: Adequate Compliant Compliance with FAR 23.1351 (a) Agree


A-10


source of electrical energy.

Compliance with FAR 23.1351 (c)

91.205(c)(6) Visual flight rules (night) - VFR: One spare set of fuses.

Not Applicable

There are no fuses accessible to the flight crew in flight.

Agree

91.205(d) Instrument flight rules - IFR Title Only

-

Agree

91.205(d)(1) Instrument flight rules - IFR: Instruments and equipment specified.

Compliant

Compliance with 91.205(b) and 91.205(c) checked by Certification.

Agree

91.205(d)(2) Instrument flight rules - IFR: Two-way radio communications system and navigational equipment.

Compliant

EMB-500 has as baseline 2 VHF Comm/ Nav (VOR) and 2 GPS. If other communication and/or navigation devices are required due to the route to be flown it is operator’s responsibility to have selected them on the optional list (HF, ADF, DME)

Agree

91.205(d)(3) Instrument flight rules - IFR: Gyroscopic rate-of-turn indicator.

Compliant

Compliance is through the use of a third attitude system (standby - IESI).

Agree

91.205(d)(4) Instrument flight rules - IFR: Slip-skid indicator.

Compliant

Compliance is through one Primary Flight Display

Agree

91.205(d)(5) Instrument flight rules - IFR: Sensitive altimeter adjustable for barometric pressure.

Compliant


Agree

91.205(d)(6) Instrument flight rules - IFR: A clock. Compliant

Compliance is on bottom right of Primary Flight Display screen.

Agree

91.205(d)(7) Instrument flight rules - IFR: Generator or alternator.

Compliant

Compliance with FAR 23.1351 (a) Compliance with FAR 23.1351 (c)

Agree

91.205(d)(8) Instrument flight rules - IFR: Gyroscopic pitch and bank indicator.

Compliant

Compliance is through one Primary Flight Display and one Attitude and Heading Reference System.

Agree

91.205(d)(9) Instrument flight rules - IFR: Gyroscopic direction indicator (directional gyro or equivalent).

Compliant

Compliance is through one Primary Flight Display and one Attitude and Heading Reference System.

Agree

91.205(e) Flight at and above 24,000 ft MSL (FL 240). Compliant

EMB-500 is equipped with suitable RNAV system (Global Positioning System - GPS)

Agree


A-11


91.205(f) Category II operations Not Applicable

Aircraft does not have Cat II capabilities

Agree

91.205(g) Category III operations Not Applicable

Aircraft does not have Cat III capabilities

Agree

91.205(h) Exclusions Not Applicable

Refer to Part 91.205(f) and 91.205(g).

Agree

91.207 Emergency locator transmitters. Title Only

-

Agree

91.207(a) Emergency locator transmitter.

Compliant EMB-500 has an ELT installed. Agree

91.207(b) Emergency locator transmitter installation. Compliant

The structure that supports the ELT will be designed to withstand the load factors prescribed in the requirement 23.561 (b)(2).

Agree

91.207(c) Emergency locator transmitter - maintenance and operation - Batteries.


-

Agree

91.207(d) Emergency locator transmitter - maintenance and operation - inspections.

Compliant

The ELT is inspected within 12 calendar months.

Agree

91.207(e) Emergency locator transmitter - maintenance and operation - exemption - ferry flights.


-

Agree

91.207(f) Emergency locator transmitter - maintenance and operation - exemptions.


-

Agree

91.209 Aircraft Lighting System - installation and operation.

Compliant

EMB-500 aircraft is equipped with approved Position and Anti-collision lights.

Agree

91.211 Supplemental oxygen: pressurized cabin Operational altitudes and technical requirements

Title Only

-

Agree

91.211(a) General Not Applicable

Applicable only to non-pressurized aircraft

Agree


A-12


91.211(b) Pressurized cabin aircraft. Definition

The oxygen system has been sized to provide all occupants (crew and passengers) with emergency oxygen for a 10-minute descent to 10,000 feet, where supplemental oxygen is not required. EMB-500 is pressurized to 8,000 feet equivalent pressure during normal operation and the crew mask is worn and operated in the normal (dilution) setting with the additional dilution valve feature activated. The crew masks are quick donning type that can be placed on the face with one hand from the ready position within 5 seconds, supplying oxygen and properly secured and sealed.

Agree

91.213 Inoperative instruments and equipment. Title Only

-

Agree

91.213(a) Inoperative instruments and equipment - Approved Minimum Equipment List

Compliant

EMBRAER will provide all information for the MMEL certification and required maintenance/operations procedures.

Agree

91.213(b) Inoperative instruments and equipment - Use of MEL.

Compliant

The MMEL proposed by EMBRAER comply with the requirements.

Agree

91.213(c) Inoperative instruments and equipment - Use of MEL.


-

Agree

91.213(d) Inoperative instruments and equipment - Use of MEL.


-

Agree

91.213(e) Inoperative instruments and equipment - Use of MEL.


-

Agree

91.215 ATC transponder and altitude reporting equipment and use.

Title Only

-

Agree

91.215(a) ATC transponder and altitude reporting equipment and use. All airspace [operations NOT conducted under FAR 121 or 135]

Compliant

EMB-500 is equipped with a Mode S Transponder

Agree

91.215(b) ATC transponder and altitude reporting equipment and use. All airspace - operations conducted under FAR 121 or 135.

Compliant

EMB-500 is equipped with a Mode S Transponder.

Agree

91.215(c) ATC transponder and altitude reporting equipment and use. All airspace - operations


-

Agree


A-13


conducted under FAR 121 or 135.

91.215(d) ATC transponder and altitude reporting equipment and use. All airspace - operations conducted under FAR 121 or 135.


-

Agree

91.217 Data correspondence between automatically reported pressure altitude data and the pilot's altitude reference.

Title Only

-

Agree

91.217(a) Deactivation of equipment. Compliant

If required by ATC the Mode-S Transponder can stop altitude report through selection of the "ON" mode (identification only).

Agree

91.217(b) Tests and calibration. Compliant

Transmitted altitude compared with Primary Flight Display altitude does not differ more than 125 ft.

Agree

91.217(c) Altimeters and digitizers standards. Not Applicable

Compliance on item (b)

Agree

91.219 Altitude alerting system or device: Turbojet-powered civil airplanes.

Title Only

-

Agree

91.219(a) Altitude alerting system or device: Turbojet-powered civil airplane


-

Agree

91.219(b) Altitude alerting system or device: Turbojet-powered civil airplane

Compliant

The G1000 system provides an altitude alert computed inside the displays with correspondent aural warnings.

Agree

91.219(c) Altitude alerting system or device operation. Operator’s Responsibility

-

Agree

91.219(d) Altitude alerting system or device operation. Operator’s Responsibility

-

Agree

91.221 Traffic alert and collision avoidance system equipment and use.

Title Only

-

Agree

91.221(a) Traffic alert and collision avoidance system equipment and use.

Optionally Compliant

EMB-500 shall offer a TCAS I as optional system some time after initial certification.

Agree

91.221(b) Traffic alert and collision avoidance system equipment and use.


-

Agree


A-14


91.223 Terrain awareness and warning system. Title Only

-

Agree

91.223(a) Terrain Awareness and Warning System Compliant

EMB-500 has a TAWS class B as baseline.

Agree

91.223(b) Terrain Awareness and Warning System Not Applicable

Aircraft manufactured after March 29,2002

Agree

91.223(c) Terrain Awareness and Warning System - operation

Compliant

The AFM will contain appropriate procedures for the use of the terrain awareness and warning system; and proper flight crew reaction in response to the terrain awareness and warning system audio and visual warning.

Agree

91.223(d) Terrain Awareness and Warning System - operation


-

Agree

EMB-500, Part 91 Compliance Subpart D - Special Flight Operations


91.301 Reserved Not Applicable

Reserved

Agree

91.303 Aerobatic flight. Operator’s Responsibility

-

Agree

91.305 Flight test areas. Operator’s Responsibility

-

Agree

91.307 Parachutes and parachuting. Operator’s Responsibility

-

Agree

91.309 Towing: Gliders and unpowered ultralight vehicles.


-

Agree


A-15


91.311 Towing: Other than under & 91.309. Operator’s Responsibility

-

Agree

91.313 Restricted category civil aircraft: Operating limitations.


-

Agree

91.315 Limited category civil aircraft: Operating limitations.


-

Agree

91.317 Provisionally certificated civil aircraft: Operating limitations.


-

Agree

91.319 Aircraft having experimental certificates: Operating limitations.


-

Agree

91.321 Carriage of candidates in elections. Operator’s Responsibility

-

Agree

91.323 Increased maximum certificated weights for certain airplanes operated in Alaska.

Not Applicable

Applicable only to airplane type certificated under Aeronautics Bulletin No. 7-A of the U.S. Department of Commerce dated January 1, 1931, as amended, or under the normal category of part 4a of the former Civil Air Regulations

Agree

91.325 Primary category aircraft: Operating limitations.

Not Applicable

Applicable only to primary category aircraft.

Agree

91.327 Aircraft having a special airworthiness certificate in the light-sport category: Operating limitations.

Not Applicable

Applicable only to aircraft with airworthiness certificate in the light-sport category.

Agree

EMB-500, Part 91 Compliance Subpart E - Maintenance, Preventive Maintenance, and Alterations


91.401 Applicability. Not Applicable

Administrative Item.

Agree


A-16


91.403 General. Operator’s Responsibility

-

Agree

91.405 Maintenance required. Operator’s Responsibility

-

Agree

91.407 Operation after maintenance, preventive maintenance, rebuilding, or alteration.


-

Agree

91.409 Inspections. Title Only

-

Agree

91.409(a) Annual Inspection Compliant

EMB-500 is delivered with airworthiness certificate released.

Agree

91.409(b) Annual or 100-hour inspection Compliant

While the airplane is under EMBRAER responsibility, it is not operated by any person for hire, and no person give flight instruction for hire.

Agree

91.409(c) Inspections program. Definition

-

Agree

91.409(d) Progressive inspection program Compliant

The EMBRAER Recommended Scheduled Maintenance Program will be included in the Aircraft Maintenance Manual

TBD

91.409(e) Replacement times for life-limited parts Operator’s Responsibility

-

Agree

91.409(f) Inspections program - definition and selection. Compliant

EMBRAER will recommend a Scheduled Maintenance Program.

TBD

91.409(g) Inspections program - approval and change. Operator’s Responsibility

-

Agree

91.409(h) Inspections program - approval and change. Operator’s - Agree


A-17


Responsibility


Reserved

Agree

91.411 Altimeter system and altitude reporting equipment tests and inspections.

Title Only

-

Agree

91.411(a) Altimeter system and altitude reporting equipment tests and inspections.

Compliant

For each airplane delivered, the static pressure system, altimeter instrument, and automatic pressure altitude are installed, inspected and tested.

TBD

91.411(b) Altimeter system and altitude reporting equipment tests and inspections.

Compliant

The manufacturer performs the tests and inspections specified in (b) (1).

TBD

91.411(c) Altimeter system and altitude reporting equipment tests and inspections.

Compliant

Altimeter and altitude reporting equipment are approved under Technical Standard Orders.

Agree

91.411(d) Altimeter system and altitude reporting equipment tests and inspections.


-

Agree

91.413 ATC transponder tests and inspections. Title Only

-

Agree

91.413(a) ATC transponder tests and inspections. Compliant

ATC Transponder is tested and inspected within 24 calendar months.

Agree

91.413(b) ATC transponder tests and inspections. Compliant

EMBRAER perform the tests and inspections on the ATC transponder installed.

TBD

91.413(c) ATC transponder tests and inspections. Compliant

EMBRAER perform the tests and inspections on the ATC transponder installed.

TBD

91.415 Changes to aircraft inspection programs. Operator’s Responsibility

-

Agree

91.417 Maintenance records. Compliant

All information of item (a)(2) is recorded on the documentation delivered to the customer with the airplane.

TBD


A-18


91.419 Transfer of maintenance records. Compliant

All maintenance records are transferred to the customer, at the time of the sale.

TBD

91.421 Rebuilt engine maintenance records. Operator’s Responsibility

-

Agree

EMB-500, Part 91 Compliance Subpart F - Large and Turbine-Powered Multiengine Airplanes and Fractional Ownership Program Aircraft


91.501 Additional operating rules governing operation of large and turbojet-powered airplanes.


-

Agree

91.503 Flying equipment and operating information. Title Only

-

Agree

91.503(a) Flying equipment and operating information. Title Only

-

Agree

91.503(a)(1) Flying equipment and operating information Compliant

A flashlight is provided on the cockpit, installed behind the pilot seat.

Agree

91.503(a)(2) Various operational requirements Compliant

EMBRAER will prepare and furnish the operation manuals inside each factory delivered airplane.

Agree

91.503(a)(3) Various operational requirements Operator’s Responsibility

-

Agree

91.503(a)(4) Various operational requirements Operator’s Responsibility

-

Agree

91.503(a)(5) Flying equipment and operating information Compliant

EMBRAER will prepare and furnish the operation manuals, with the cockpit checklist included, inside

Agree


A-19


each factory delivered airplane.

91.503(b) Flying equipment and operating information Compliant

EMBRAER will prepare and furnish the operation manuals, with the cockpit checklist included, inside each factory delivered airplane.

TBD

91.503(c) Flying equipment and operating information Compliant


TBD

91.503(d) Various operational requirements Operator’s Responsibility

-

Agree

91.505 Familiarity with operating limitations and emergency equipment.


-

Agree

91.507 Equipment requirements: Over-the-top or night VFR operations.

Compliant

Compliance with 91.205(d). EMB-500 is equipped with two wing root Landing Lights.

Agree

91.509 Survival equipment for overwater operations. Title Only

-

Agree

91.509(a) Survival equipment for over water operations (50 nautical miles from the nearest shore).


Life vests will be provided as an optional. Life vest pouches under each seat are provided in order to allow its installation whenever required.

Agree

91.509(b) Survival equipment for overwater operations (30 minutes flying or 100 nautical miles from the nearest shore).

Title Only

-

Agree

91.509(b)(1) Survival equipment for overwater operations: life preserver


Life vests will be provided as an optional. Life vest pouches under each seat are provided in order to allow its installation whenever required.

Agree

91.509(b)(2) Survival equipment for overwater operations: life rafts Not Compliant

Installation of live rafts in case of operation over water is an operator responsibility. Space will be provided inside the passenger cabin for life raft installation follow on certification.

Agree


A-20


91.509(b)(3) Survival equipment for overwater operations: pyrotechnic signaling device


Pyrotechnic devices are installed within life-rafts. Life rafts are optional item.

Agree

91.509(b)(4) Survival equipment for overwater operations: portable emergency radio signaling device

Not Compliant

This item is not installed for aircraft delivery. Installation is an operator responsibility in case of overwater operation.

Agree

91.509(b)(5) Survival equipment for overwater operations: lifeline Not Compliant

This item is not installed for aircraft delivery. Installation is an operator responsibility in case of overwater operation.

Agree

91.509(c) Survival equipment for overwater operations (30 minutes flying or 100 nautical miles from the nearest shore).


-

Agree

91.509(d) Devices must be installed in conspicuously marked locations and easily accessible


Life vests are offered as optional items, and if installed, are conspicuously marked. Life Rafts are follow-on certification items.

Agree

91.509(e) Survival kit, appropriately equipped for the route to be flown

Not Compliant

Survival kit attached to the life raft is an operator responsibility.

Agree

91.509(f) Definition of Shore Definition

-

Agree

91.511 Radio equipment for overwater operations. Title Only

-

Agree

91.511(a) Radio equipment for over water operations Title Only

-

Agree

91.511(a)(1) Radio equipment for overwater operations: Radio communication equipment

Compliant

EMB-500 has 2 independent VHF Comm systems.

Agree

91.511(a)(2) Radio equipment for overwater operations: electronic navigational equipment

Compliant

EMB-500 has 2 VOR and 2 GPS Systems as baseline. If other navigation devices are required due to the route to be flown it is operator’s responsibility to have selected them on the optional list (ADF, DME).

Agree


A-21


91.511(b) Definition of independent receiver or electronic navigation unit as required in 91.511 (a)

Definition

-

Agree

91.511(c) Various operational requirements. Operator’s Responsibility

-

Agree

91.511(d) Various operational requirements. Operator’s Responsibility

-

Agree

91.511(e) Definition of Shore. Definition

-

Agree

91.511(f) Authorized routes to operate with an operational single long-range navigation system.


-

Agree

91.513 Emergency equipment. Title Only

-

Agree

91.513(a) Emergency equipment definition and installation Operator’s Responsibility

-

Agree

91.513(b) Emergency equipment. Introduction

-

Agree

91.513(b)(1) Emergency equipment inspection Operator’s Responsibility

-

Agree

91.513(b)(2) Emergency equipment definition and installation Compliant

Each required item of equipment is readily accessible to the flight crew.

TBD


All equipment possesses a clear indication of its method of operation, by means of an inscription of the equipment itself, or a placard.

TBD


All compartments which have emergency equipment installed on its interior are marked for its content

TBD


A-22


identification.

91.513(c) Hand fire extinguishers Compliant One fire extinguisher is provided on the cockpit area, behind the copilot seat, filled with Halon 1211/1301 blend rated for classes B and C types of fire. Since the maximum capacity of the EMB-500 is 6 passengers, a fire extinguisher inside the passenger cabin is not required.

TBD

91.513(d) First Aid kits Compliant

A first aid kit is provided inside the passenger cabin.

TBD

91.513(e) Crash Axe Not Applicable

Applicable only to aircraft with a capacity for more than 19 passengers.

Agree

91.513(f) Megaphone Not Applicable

Applicable only to airplanes with a seating capacity of more than 60.

Agree

91.515 Flight altitude rules. Operator’s Responsibility

-

Agree

91.517 Passenger information. Title Only

-

Agree

91.517(a) Passenger information Compliant

The fasten seat belts signs are installed. There is a placard stating that smoke is prohibited.

Agree

91.517(b) Crew and PAX requirements Operator’s Responsibility

-

Agree

91.517(c) Crew and PAX requirements Operator’s Responsibility

-

Agree

91.517(d) Crew and PAX requirements Operator’s Responsibility

-

Agree

91.517(e) Crew and PAX requirements Operator’s - Agree


A-23


Responsibility

91.519 Passenger briefing. Title Only

-

Agree

91.519(a) Passenger briefing Operator’s Responsibility

-

Agree

91.519(b) Passenger briefing Title Only

-

Agree

91.519(b)(1) Passenger briefing: PAX cards Compliant

Briefing cards containing the method of operation of the emergency exits are provided for all passengers.

TBD

91.519(b)(2) Passenger briefing Compliant

For all equipment installed by EMBRAER: a)instructions are provided on the equipment itself describing its operation, or b)there is a placard near the equipment installing position describing its operation, or c) Instructions are provided on the briefing card.

TBD

91.519(c) Passenger briefing: Location for PAX cards Compliant

Briefing cards are related only to the specific characteristics of the EMB-500. Briefing cards are installed on the magazine holders, adjacent to each passenger seat.

TBD

91.519(d) Passenger briefing Operator’s Responsibility

-

Agree

91.521 Shoulder harness. Not Applicable

Applicable only to transport category airplane.

Agree

91.523 Carry-on baggage. Not Applicable

Applicable only for aircraft with a seating capacity for more than 19 passengers

Agree

91.525 Carriage of cargo. Title Only

-

Agree


A-24


91.525(a) Carriage of cargo Compliant

Baggage compartments are provided, however activities related to pilot permission for use of this compartment are operator’s responsibility.

Agree

91.525(b) Carriage of cargo - Cargo loading and distribution Operator’s Responsibility

-

Agree

91.527 Operating in icing conditions. Title Only

-

Agree

91.527(a) Operating in icing conditions Operator’s Responsibility

-

Agree

91.527(b) Operating in icing conditions: flight under IFR, VFR or severe icing conditions

Compliant

EMB-500 have ice protection system installed on the following regions: Wing Leading edges; Horizontal Stabilizer Leading edges; Nacelle inlet; Windshield; Air probes.

Agree

91.527(c) Operating in icing conditions: flight under IFR, VFR or severe icing conditions

Compliant

EMB-500 have ice protection system installed on the following regions: Wing Leading edges; Horizontal Stabilizer Leading edges; Nacelle inlet; Windshield; Air probes.

Agree

91.527(d) Operating in icing conditions - non-icing forecast. Operator’s Responsibility

-

Agree

91.529 Flight engineer requirements. Not Applicable

Applicable only for aircraft type certificated with a flight engineer.

Agree

91.531 Second in command requirements. Operator’s Responsibility

-

Agree

91.533 Flight attendant requirements. Not Applicable

Applicable only to aircraft with more than 19 passengers on board.

Agree

91.535 Stowage of food, beverage, and passenger service equipment during aircraft movement on the surface, takeoff, and landing.


-

Agree


A-25


EMB-500, Part 91 Compliance Subpart G - Additional Equipment and Operating Requirements for Large and Transport Category Aircraft



Applicable only to Large and Transport Category Aircraft.

Agree

91.603 Aural speed warning device. Not Applicable

Applicable only to Transport Category Airplanes

Agree

91.605 Transport category civil airplane weight limitations. Not Applicable


Agree

91.607 Emergency exits for airplanes carrying passengers for hire.

Not Applicable

Applicable only to large aircraft type certificated under the Civil Air Regulations effective before April 9, 1957.

Agree

91.609 Flight recorders and cockpit voice recorders. Title Only

-

Agree

91.609(a) Authorized flights without equipment installed or inoperative - holder of an air carrier operating certificate or an operating certificate.


-

Agree

91.609(b) Authorized flights without equipment installed or inoperative - operator other than the holder of an air carrier or a commercial operator certificate.


-

Agree

91.609(c) Flight data and cockpit voice recorders - features. Not Applicable

Applicable only to aircraft having a passenger seating configuration, excluding any pilot seats, of 10 or more

Agree

91.609(d) Flight data and cockpit voice recorders - operation. Not Applicable

Applicability related to item 91.609(c)

Agree

91.609(e) Flight data and cockpit voice recorders Not Applicable

Initial certification of EMB-500 does not include 6 passengers configuration.

Agree


A-26


91.609(f) Cockpit voice recorder - recording and erasing features.

Not Applicable


Agree

91.609(g) Flight data and cockpit voice recorders - operator’s obligations.


-

Agree

91.609(h) Cockpit voice recorder - data required Not Applicable

EMB 500 is not required to have FDR.

Agree

91.609(i) Cockpit voice recorder - data required Not Applicable


Agree

91.609(j) Cockpit voice recorder - data link communication Not Applicable


Agree

91.611 Authorization for ferry flight with one engine inoperative.

Not Applicable

Applicable only to aircraft with three or four engines.

Agree

91.613 Materials for compartment interiors. Not Applicable

Applicable only to Large Aircraft

Agree

EMB-500, Part 91 Compliance Subpart H - Foreign Aircraft Operations and Operations of U.S.-Registered Civil Aircraft Outside of the United States; and Rules Governing Persons on Board

Such Aircraft



-

Agree

91.702 Persons on board. Definition

-

Agree


A-27


91.703 Operations of civil aircraft of U.S. registry outside of the United States.


-

Agree

91.705 Operations within airspace designated as Minimum Navigation Performance Specification Airspace.


-

Agree

91.706 Operations within airspace designed as Reduced Vertical Separation Minimum Airspace.


-

Agree

91.707 Flights between Mexico or Canada and the United States.


-

Agree

91.709 Operations to Cuba. Operator’s Responsibility

-

Agree

91.711 Special rules for foreign civil aircraft. Not Applicable

Applicable only to aircraft not registered in USA

Agree

91.713 Operation of civil aircraft of Cuban registry. Not Applicable

Applicable only to Cuban registered aircraft.

Agree

91.715 Special flight authorizations for foreign civil aircraft. Not Applicable

Applicable only to aircraft not registered in USA.

Agree

EMB-500, Part 91 Compliance Subpart I - Operating Noise Limits


91.801 Applicability: Relation to part 36. Definition

-

Agree

91.803 Part 125 operators: Designation of applicable regulations.

Not Applicable

Applicable only to Part 125 eligible aircraft.

Agree


A-28


91.805 Final compliance: Subsonic airplanes. Not Applicable

Applicable only to aircraft with MTOW of more than 75,000 pounds.

Agree

91.815 Agricultural and fire fighting airplanes: Noise operating limitations.

Not Applicable

Applicable only to propeller-driven, small airplanes having standard airworthiness certificates that are designed for "agricultural aircraft operations" or for dispensing fire fighting materials.

Agree

91.817 Civil aircraft sonic boom. Not Applicable

Applicable only to supersonic aircraft.

Agree

91.819 Civil supersonic airplanes that do not comply with part 36.

Not Applicable


Agree

91.821 Civil supersonic airplanes: Noise limits. Not Applicable


Agree

91.851 Definitions. Definition

-

Agree

91.853 Final compliance: Civil subsonic airplanes. Not Applicable

Applicable only to aircraft with MTOW superior to 75,000 pounds.

Agree

91.855 Entry and nonaddition rule. Not Applicable


Agree

91.857 Stage 2 operations outside of the 48 contiguous United States.


-

Agree

91.858 Special flight authorizations for non-revenue Stage 2 operations.

Not Applicable


Agree

91.859 Modification to meet Stage 3 or Stage 4 noise levels. Not Applicable


Agree

91.861 Base level. Operator’s Responsibility

-

Agree

91.863 Transfers of Stage 2 airplanes with base level. Operator’s Responsibility

-

Agree


A-29


91.865 Phased compliance for operators with base level. Operator’s Responsibility

-

Agree

91.867 Phased compliance for new entrants. Operator’s Responsibility

-

Agree

91.869 Carry-forward compliance. Operator’s Responsibility

-

Agree

91.871 Waivers from interim compliance requirements. Operator’s Responsibility

-

Agree

91.873 Waivers from final compliance. Operator’s Responsibility

-

Agree

91.875 Annual progress reports. Operator’s Responsibility

-

Agree

91.877 Annual reporting of Hawaiian operations. Operator’s Responsibility

-

Agree

EMB-500, Part 91 Compliance Subpart J - Waivers



Reserved.

Agree

91.903 Policy and procedures. Operator’s Responsibility

-

Agree

91.905 List of rules subject to waivers. Operator’s Responsibility

-

Agree


A-30

EMB-500, Part 91 Compliance Subpart K - Fractional Ownership Operations



-

Agree

91.1002 Compliance date. Operator’s Responsibility

-

Agree

91.1003 Management contract between owner and program manager.


-

Agree

91.1005 Prohibitions and limitations. Operator’s Responsibility

-

Agree

91.1007 Flights conducted under part 121 or part 135 of this chapter.


-

Agree

91.1009 Clarification of operational control. Operator’s Responsibility

-

Agree

91.1011 Operational control responsibilities and delegation.


-

Agree

91.1013 Operational control briefing and acknowledgment. Operator’s Responsibility

-

Agree

91.1014 Issuing or denying management specifications. Not Applicable

Administrative Instructions.

Agree

91.1015 Management specifications. Operator’s Responsibility

-

Agree

91.1017 Amending program manager's management specifications.


-

Agree

91.1019 Conducting tests and inspections. Not Applicable

Administrative.

Agree


A-31


91.1021 Internal safety reporting and incident/accident response.


-

Agree

91.1023 Program operating manual requirements. Operator’s Responsibility

-

Agree

91.1025 Program operating manual contents. Operator’s Responsibility

-

Agree

91.1027 Recordkeeping. Operator’s Responsibility

-

Agree

91.1029 Flight scheduling and locating requirements. Operator’s Responsibility

-

Agree

91.1031 Pilot in command or second in command: Designation required.


-

Agree

91.1033 Operating information required. Title Only

-

Agree

91.1033(a) Operating information required Introduction

-

Agree

91.1033(a)(1) Operating information required: cockpit checklist Compliant


TBD

91.1033(a)(2) Operating information required: emergency cockpit checklist

Compliant


TBD

91.1033(a)(3) Operating information required: aeronautical charts Operator’s Responsibility

-

Agree

91.1033(a)(4) Operating information required: navigational en route, terminal area, and instrument approach procedure charts


-

Agree


A-32


91.1033(b) Operating information required: cockpit checklist Compliant


TBD

91.1033(c) Operating information required: emergency cockpit checklist

Compliant


TBD

91.1035 Passenger awareness. Title Only

-

Agree

91.1035(a) Passenger awareness: Passenger Briefing Operator’s Responsibility

-

Agree

91.1035(b) Passenger awareness: Passenger Briefing Operator’s Responsibility

-

Agree

91.1035(c) Passenger awareness: Passenger Briefing Operator’s Responsibility

-

Agree

91.1035(d) Passenger awareness: Passenger Briefing Operator’s Responsibility

-

Agree

91.1035(e) Passenger awareness: Passenger Briefing Operator’s Responsibility

Briefing cards are provided for the passengers with instruction for the procedures described on FAR 91.1035(a).

TBD

91.1035(f) Passenger awareness: Passenger Briefing Printed Cards

Compliant

Briefing cards are provided for each passenger, containing information for the specific EMB-500 characteristics and including indication of emergency exit operation and any instruction for emergency equipments installed by the aircraft manufacturer.

TBD

91.1037 Large transport category airplanes: Turbine engine powered; Limitations; Destination and alternate airports.

Not Applicable

Applicable only to turbine engine powered large transport category airplane.

Agree

91.1039 IFR takeoff, approach and landing minimums. Operator’s Responsibility

-

Agree


A-33


91.1041 Aircraft proving and validation tests. Operator’s Responsibility

-

Agree


Reserved

Agree

91.1045 Additional equipment requirements. Title Only

-

Agree

91.1045(a) Additional equipment requirements Not Applicable

Applicable only to aircraft with a passenger-seat configuration of more than 30 seats or a payload capacity of more than 7,500 pounds.

Agree

91.1045(b) Additional equipment requirements Title Only

-

Agree

91.1045(b)(1) Additional equipment requirements: cockpit voice recorder

Not Applicable


Agree

91.1045(b)(2) Additional equipment requirements: flight recorder Not Applicable

Applicable only to multi-engine, turbine-engine powered airplane or rotorcraft having a passenger seating configuration, excluding any required crewmember seat, of 10 to 19 seats.

Agree

91.1045(b(3) Additional equipment requirements: terrain awareness and warning system

Compliant

EMB-500 has a TAWS B as baseline.

Agree

91.1045(b)(4) Additional equipment requirements: traffic alert and collision avoidance system

Not Applicable

Applicable only to turbine powered airplane that has a passenger seat configuration, excluding any pilot seat, of 10 to 30 seats.

Agree

91.1045(b)(5) Additional equipment requirements: Airborne weather radar

Not Applicable

Applicable only to aircraft with a passenger seating configuration, excluding any pilot seat, of 10 seats or more.

Agree

91.1047 Drug and alcohol misuse education program. Operator’s Responsibility

-

Agree


A-34


91.1049 Personnel. Operator’s Responsibility

-

Agree

91.1051 Pilot safety background check. Operator’s Responsibility

-

Agree

91.1053 Crewmember experience. Operator’s Responsibility

-

Agree

91.1055 Pilot operating limitations and pairing requirement. Operator’s Responsibility

-

Agree

91.1057 Flight, duty and rest time requirements: All crewmembers.


-

Agree

91.1059 Flight time limitations and rest requirements: One or two pilot crews.


-

Agree

91.1061 Augmented flight crews. Operator’s Responsibility

-

Agree

91.1062 Duty periods and rest requirements: Flight attendants. Operator’s Responsibility

-

Agree

91.1063 Testing and training: Applicability and terms used. Definition

-

Agree

91.1065 Initial and recurrent pilot testing requirements. Operator’s Responsibility

-

Agree

91.1067 Initial and recurrent flight attendant crewmember testing requirements.


-

Agree

91.1069 Flight crew: Instrument proficiency check requirements.


-

Agree

91.1071 Crewmember: Tests and checks, grace provisions, training to accepted standards.

Definition

-

Agree


A-35


91.1073 Training program: General. Operator’s Responsibility

-

Agree

91.1075 Training program: Special rules. Definition

-

Agree

91.1077 Training program and revision: Initial and final approval.


-

Agree

91.1079 Training program: Curriculum. Operator’s Responsibility

-

Agree

91.1081 Crewmember training requirements. Operator’s Responsibility

-

Agree

91.1083 Crewmember emergency training. Operator’s Responsibility

-

Agree

91.1085 Hazardous materials recognition training. Operator’s Responsibility

-

Agree

91.1087 Approval of aircraft simulators and other training devices.

Definition

-

Agree

91.1089 Qualifications: Check pilots (aircraft) and check pilots (simulator).


-

Agree

91.1091 Qualifications: Flight instructors (aircraft) and flight instructors (simulator).


-

Agree

91.1093 Initial and transition training and checking: Check pilots (aircraft), check pilots (simulator).


-

Agree

91.1095 Initial and transition training and checking: Flight instructors (aircraft), flight instructors (simulator).


-

Agree

91.1097 Pilot and flight attendant crewmember training programs.


-

Agree

91.1099 Crewmember initial and recurrent training requirements.


-

Agree


A-36


91.1101 Pilots: Initial, transition, and upgrade ground training. Operator’s Responsibility

-

Agree

91.1103 Pilots: Initial, transition, upgrade, requalification, and differences flight training.


-

Agree

91.1105 Flight attendants: Initial and transition ground training. Operator’s Responsibility

-

Agree

91.1107 Recurrent training. Operator’s Responsibility

-

Agree

91.1109 Aircraft maintenance: Inspection program. Title Only

-

Agree

91.1109(a) Aircraft maintenance: Inspection program Title Only

-

Agree

91.1109(a)(1) Aircraft maintenance: Inspection program - Instructions and procedures for the conduct of inspections

Compliant

The information will be issued in the Aircraft Maintenance Manual.

TBD

91.1109(a)(2) Aircraft maintenance: Inspection program - schedule for performing the inspections

Compliant

The recommended Scheduled Maintenance Program complies with this requirement.

TBD

91.1109(a)(3) Aircraft maintenance: Inspection program - person responsible for scheduling the inspections


-

Agree

91.1109(b) Aircraft maintenance: Inspection program Compliant

The EMBRAER Recommended Scheduled Maintenance Program will be included in the Aircraft Maintenance Manual, and the engine manufacturer will issue a Scheduled Maintenance Program too.

TBD

91.1109(c) Aircraft maintenance: Inspection program Definition

-

Agree

91.1111 Maintenance training. Operator’s Responsibility

-

Agree


A-37


91.1113 Maintenance recordkeeping. Operator’s Responsibility

-

Agree

91.1115 Inoperable instruments and equipment. Title Only

-

Agree

91.1115(a) Inoperable instruments and equipment. Title Only

-

Agree

91.1115(a)(1) Inoperable instruments and equipment: Minimum Equipment List

Compliant


Agree

91.1115(a)(2) Inoperable instruments and equipment: management specifications


-

Agree

91.1115(a)(3) Inoperable instruments and equipment: MEL Compliant


Agree

91.1115(a)(4) Inoperable instruments and equipment: records Operator’s Responsibility

-

Agree

91.1115(a)(5) Inoperable instruments and equipment: operations Operator’s Responsibility

-

Agree

91.1115(b) Inoperable instruments and equipment: MEL limitations

Compliant


Agree

91.1115(c) Inoperable instruments and equipment: special flight permit


-

Agree

91.1115(d) Inoperable instruments and equipment Definition

-

Agree

91.1411 Continuous airworthiness maintenance program use by fractional ownership program manager.

Compliant

The EMBRAER Recommended Scheduled Maintenance Program will be included in the Aircraft Maintenance Manual

TBD

91.1413 CAMP: Responsibility for airworthiness. Operator’s Responsibility - Agree


A-38


91.1415 CAMP: Mechanical reliability reports. Operator’s Responsibility

-

Agree

91.1417 CAMP: Mechanical interruption summary report. Operator’s Responsibility

-

Agree

91.1423 CAMP: Maintenance organization. Operator’s Responsibility

-

Agree

91.1425 CAMP: Maintenance, preventive maintenance, and alteration programs.


-

Agree

91.1427 CAMP: Manual requirements. Operator’s Responsibility

-

Agree

91.1429 CAMP: Required inspection personnel. Operator’s Responsibility

-

Agree

91.1431 CAMP: Continuing analysis and surveillance. Operator’s Responsibility

-

Agree

91.1433 CAMP: Maintenance and preventive maintenance training program.


-

Agree

91.1435 CAMP: Certificate requirements. Operator’s Responsibility

-

Agree

91.1437 CAMP: Authority to perform and approve maintenance.


-

Agree

91.1439 CAMP: Maintenance recording requirements. Operator’s Responsibility

-

Agree

91.1441 CAMP: Transfer of maintenance records. Operator’s Responsibility

-

Agree

91.1443 CAMP: Airworthiness release or aircraft maintenance log entry.


-

Agree


A-39


EMB-500, Part 91 Compliance Subpart L - Continued Airworthiness and Safety Improvements


91.1501 Purpose and definition Definition

-

Agree


Reserved item.

Agree

91.1505 Repairs assessment for pressurized fuselages. Not Applicable

Applicable only for Airbus Model A300 (excluding the -600 series), British Aerospace Model BAC 1-11, Boeing Model, 707, 720, 727, 737 or 747, McDonnell Douglas Model DC-8, DC-9/MD-80 or DC-10, Fokker Model F28, or Lockheed Model L-1011 airplane.

Agree

91.1507 Fuel tank system inspection program Not Applicable

Applicable only for transport category, turbine-powered airplanes with a maximum type-certificated passenger capacity of 30 or more, or maximum payload capacity of 7,500 pounds or more.

Agree

Appendix B to Part 91 - Authorizations To Exceed Mach 1 (§91.817)


Appendix B Authorization to exceed Mach 1 Not Applicable

Aircraft certified maximum speed do not exceed Mach 1

Agree

EMB-500, Part 91 Compliance Appendix C to Part 91 - Operations in the North Atlantic (NAT) Minimum Navigation Performance Specifications (MNPS) Airspace


A-40


Appendix C Operations in the North Atlantic Compliant

EMB-500 G-1000 complies with Oceanic/Remote - RNP-10 (per FAA AC 20-138A, FAA Notice 8110-60, FAA Order 8400-12A, and FAA Order 8700-1). Both GPS receivers are required to be operating and receiving usable signals except for routes requiring only one Long Range Navigation (LRN) sensor.

Agree

EMB-500, Part 91 Compliance Appendix D to Part 91 - Airports/Locations: Special Operating Restrictions


Appendix D Airports/Locations: special operating restrictions Operator’s Responsibility

-

Agree

EMB-500, Part 91 Compliance Appendix E to Part 91 - Airplane Flight Recorder Specifications


Appendix E Airplane Flight Recorder Specifications Not Applicable


Agree

EMB-500, Part 91 Compliance Appendix F to Part 91 - Helicopter Flight Recorder Specifications


Appendix F Helicopter Flight Recorder Specifications Not Applicable

Applicable to helicopter only

Agree


A-41


Appendix G to Part 91 - Operations in Reduced Vertical Separation Minimum (RVSM)


Appendix G Operations in Reduced Vertical Separation Minimum (RVSM) Airspace

Title Only

-

Agree

Appendix G.1 Definitions Definition

-

Agree

Appendix G.2(a) Aircraft approval - Applicability Operator’s Responsibility

-

Agree

Appendix G.2(b) Required documents for aircraft approval Operator’s Responsibility

-

Agree

Appendix G.2(c) Altitude-keeping equipment: All aircraft Not Applicable

EMB-500 is equipped with dual RVSM compliant Air Data Systems and a 3 axis digital autopilot that will comply with the tolerances requested.

Agree

Appendix G.2(d) Altimetry system error containment: Applications on or before 9 APR 1997.

Not Applicable

Applicable only to aircraft for which application for type certification was made on or before April 9, 1997.

Agree

Appendix G.2(e) Altimetry system error containment: Applications after 9 APR 1997.

Compliant

EMB-500 Altimetry system error containment is demonstrated to be within the required budget.

Agree

Appendix G.2(f) Altimetry system error containment: Non-group aircraft


-

Agree

Appendix G.2(g) Traffic Alert and Collision Avoidance System (TCAS) Compatibility With RVSM Operations

Compliant

EMB-500 FAA is not equipped with a TCAS 2.

Agree

Appendix G.2(h) FAA Approval Definition

-

Agree

Appendix G.3 Operator Authorization Operator’s Responsibility

-

Agree


A-42


Appendix G.4 RVSM Operations Operator’s Responsibility

-

Agree

Appendix G.5 Duration Authority Approval Operator’s Responsibility

-

Agree

Appendix G.6 Reporting Altitude Keeping Errors Operator’s Responsibility

-

Agree

Appendix G.7 Renewal or Amendment of Authority Definition

-

Agree

Appendix G.8 Airspace Designation Operator’s Responsibility

-

Agree

EMB-500, Part 135 Compliance Subpart A - General



-

Agree

135.2 Compliance schedule for operators that transition to part 121 of this chapter; certain new entrant operators.

Not Applicable

Applicability does not include aircraft with the characteristics of the EMB-500.

Agree


A-43


135.3 Rules applicable to operations subject to this part. Operator’s Responsibility

-

Agree

135.4 Applicability of rules for eligible on-demand operations.


-

Agree

135.7 Applicability of rules to unauthorized operators. Definition

-

Agree

135.12 Previously trained crewmembers. Operator’s Responsibility

-

Agree

135.19 Emergency operations. Operator’s Responsibility

-

Agree

135.21 Manual requirements. Operator’s Responsibility

-

Agree

135.23 Manual contents. Operator’s Responsibility

-

Agree

135.25 Aircraft requirements. Operator’s Responsibility

-

Agree



-

Agree

135.43 Crewmember certificates: International operations. Operator’s Responsibility

-

Agree

EMB-500, Part 135 Compliance Subpart B - Flight Operations


135.61 General. Definition

-

Agree


A-44


135.63 Recordkeeping requirements. Operator’s Responsibility

-

Agree

135.64 Retention of contracts and amendments: Commercial operators who conduct intrastate operations for compensation or hire.


-

Agree

135.65 Reporting mechanical irregularities. Operator’s Responsibility

-

Agree

135.67 Reporting potentially hazardous meteorological conditions and irregularities of communications or navigation facilities.


-

Agree

135.69 Restriction or suspension of operations: Continuation of flight in an emergency.


-

Agree

135.71 Airworthiness check. Operator’s Responsibility

-

Agree

135.73 Inspections and tests. Operator’s Responsibility

-

Agree

135.75 Inspector’s credentials: admission to pilots' compartment: Forward observer's seat.

Definition

-

Agree

135.75(a) Inspector’s credentials: Admission to pilots' compartment: Forward observer's seat.


-

Agree

135.75(b) Inspector’s credentials: Admission to pilots' compartment: Forward observer's seat.

Compliant The left-hand side, aft-facing passenger seat installed on the first row will be used as the observer seat. The oxygen system normally provided for the passengers, installed on the ceiling panel, will be available the FAA inspector use. EMB-500 Audio system provides bi-directional communication among the passengers and the flight crew through the headsets using the cockpit call switch.

TBD


A-45


135.76 DOD Commercial Air Carrier Evaluator's Credentials: Admission to Pilot’s compartment: Forward observer's seat.

Title Only

-

Agree

135.76(a) DOD Commercial Air Carrier Evaluator's Credentials: Admission to Pilot’s compartment: Forward observer's seat.


-

Agree

135.76(b) DOD Commercial Air Carrier Evaluator's Credentials: Admission to Pilot’s compartment: Forward observer's seat.

Compliant

The left-hand side, aft-facing passenger seat installed on the first row will be used as the observer seat. The oxygen system normally provided for the passengers, installed on the ceiling panel, will be available the FAA inspector use. EMB-500 Audio system provides bi-directional communication among the passengers and the flight crew through the headsets using the cockpit call switch.

TBD

135.77 Responsibility for operational control. Operator’s Responsibility

-

Agree

135.78 Instrument approach procedures and IFR landing minimums.


-

Agree

135.79 Flight locating requirements. Operator’s Responsibility

-

Agree

135.81 Informing personnel of operational information and appropriate changes.


-

Agree

135.83 Operating information required. Title Only

-

Agree

135.83(a) Operating information required Title Only

-

Agree

135.83(a)(1) Operating information required: checklist Compliant

EMBRAER will furnish a set of operation manuals set, with a cockpit checklist included, in each factory delivered airplane.

TBD

135.83(a)(2) Operating information required: emergency checklist Compliant EMBRAER will furnish a set of operation manuals, TBD


A-46


with the checklist included, in each factory delivered airplane.

135.83(a)(3) Operating information required: Aeronautical Charts Operator’s Responsibility

-

Agree

135.83(a)(4) Operating information required: navigational en route, terminal area, and approach and letdown chart


-

Agree

135.83(a)(5) Operating information required: one-engine-inoperative climb performance data

Compliant

EMBRAER will furnish a set of operational manuals, with the required performance data, inside each airplane factory delivered.

TBD

135.83(b) Operating information required: cockpit checklist contents

Compliant

EMBRAER will furnish a set of operation manuals, with the checklist included, in each factory delivered airplane.

TBD

135.83(c) Operating information required: cockpit checklist contents

Compliant

EMBRAER will furnish a set of operation manuals, with the checklist included, in each factory delivered airplane.

TBD

135.85 Carriage of persons without compliance with the passenger-carrying provisions of this part.


-

Agree

135.87 Carriage of cargo including carry-on baggage. Compliant

The fwd and aft cargo compartments and stowage compartments inside the passenger cabin are provided for cargo carriage. For the compartments that also provide storage area for emergency equipment, like the lavatory cabinet, these equipments are located in such a way that baggage installation does not obstruct access in an emergency situation, nor obstruct access to the aisle between the crew and passenger compartments or obscures passenger view of a the required signs.

TBD

135.89 Pilot requirements: Use of oxygen. Definition

EMB-500 is pressurized to 8,000 feet equivalent pressure. In the event of a decompression, emergency oxygen is provided to all occupants. Two hours for crew and 30 minutes for passengers for the descent to 10,000 feet in less than 30 minutes. The crew oxygen mask used in the EMB-500 oxygen

Agree


A-47


system is a quick donning (within 5 seconds) mask assembly, stowed in a box mounted next to the seat. The mask is continuously pressurized to provide ready access to emergency oxygen.

135.91 Oxygen for medical use by passengers. Operator’s Responsibility

-

Agree

135.93 Autopilot: Minimum altitudes for use. Compliant The autopilot minimum altitude is defined in the AFM.

Agree

135.95 Airmen: Limitations on use of services. Operator’s Responsibility

-

Agree

135.97 Aircraft and facilities for recent flight experience. Operator’s Responsibility

-

Agree

135.98 Operations in the North Polar Area Not Compliant

Due to the AHRS limitations, EMB-500 is not allowed to operate above 70° N in any longitude.

Agree

135.99 Composition of flight crew. Title Only

-

Agree

135.99(a) Composition of flight crew. Compliant

EMBRAER issues and furnishes the operational manuals, with the required minimum crew limitation, inside each airplane factory delivered.

TBD

135.99(b) Composition of flight crew Not Applicable

Applicable only to aircraft with ten passenger seats or more.

Agree

135.100 Flight crewmember duties. Operator’s Responsibility

-

Agree

135.101 Second in command required under IFR. Operator’s Responsibility

-

Agree

135.103 Reserved Not Applicable Reserved. Agree


A-48


135.105 Exception to second in command requirement: Approval for use of autopilot system.

Compliant

An autopilot system is available and approved in TC. MMEL defines the dispatchability restrictions.

Agree

135.107 Flight attendant crewmember requirement. Not Applicable

Applicable only to aircraft with passenger seating configuration of 19 or more.

Agree



-

Agree

135.111 Second in command required in category II operations. Not Applicable

Aircraft not certified for Cat II operations.

Agree

135.113 Passenger occupancy of pilot seat. Not Applicable

Applicable only to aircraft with passenger seating configuration of more than eight seats.

Agree

135.115 Manipulation of controls. Operator’s Responsibility

-

Agree

135.117 Briefing of passengers before flight. Title Only

-

Agree

135.117(a) Briefing of passengers before flight. Operator’s Responsibility

-

Agree

135.117(b) Briefing of passengers before flight. Operator’s Responsibility

-

Agree

135.117(c) Briefing of passengers before flight. Operator’s Responsibility

-

Agree

135.117(d) Briefing of passengers before flight. Operator’s Responsibility

-

Agree


A-49


135.117(e) Briefing of passengers before flight: Printed Cards. Compliant

Briefing cards are provided for each passenger, containing information for the specific EMB-500 characteristics, including indication of emergency exit operation and any instruction for emergency equipments installed by the aircraft manufacturer and whose operation is not clearly indicated on the equipment itself or any placard adjacent to the equipment installation position.

TBD

135.117(f) Briefing of passengers before flight: Approved recording playback device.

Not Compliant

EMB-500 is not provided with a recording playback device.

Agree

135.119 Prohibition against carriage of weapons. Operator’s Responsibility

-

Agree

135.120 Prohibition on interference with crewmembers Operator’s Responsibility

-

Agree

135.121 Alcoholic beverages. Operator’s Responsibility

-

Agree



-

Agree

135.123 Emergency and emergency evacuation duties. Operator’s Responsibility

-

Agree

135.125 Airplane security. Operator’s Responsibility

-

Agree

135.127 Passenger information requirements and smoking prohibitions.

Compliant

The "No Smoking" signs are provided inside the cabin.

TBD

135.128 Use of safety belts and child restraint systems. Compliant

EMB-500 is provided with pilot and co-pilot seats inside the cockpit area and provided with 5-points restraint system; and passenger seats inside the cabin area, provided with 3-points restraint system.

TBD


A-50


135.129 Exit seating. Not Applicable

Not applicable for on-demand operations with aircraft having 19 or fewer passenger seats and commuter operations with aircraft having 9 or fewer passenger seats

Agree

EMB-500, Part 135 Compliance Subpart C - Aircraft and Equipment



-

Agree

135.143 General requirements. Title Only

-

Agree

135.143(a) General requirements. Operator’s Responsibility

-

Agree

135.143(b) General requirements. Operator’s Responsibility

-

Agree

135.143(c) General requirements: Transponder. Compliant

EMB-500 Mode S transponder complies with TSO C112

Agree

135.144 Portable electronic devices. Operator’s Responsibility

-

Agree

135.145 Aircraft proving and validation tests. Operator’s Responsibility

-

Agree

135.147 Dual controls required. Compliant

Dual functional controls are available and approved in TC.

Agree

135.149 Equipment requirements: General. Title Only

-

Agree


A-51


135.149(a) Equipment requirements: General: Sensitive altimeter. Compliant

EMB-500 exceeds the requirement by having 3 altimeters.

Agree

135.149(b) Equipment requirements: General: Heating or deicing equipment for each carburetor.

Not Applicable

Applicable only to aircraft with reciprocating engines.

Agree

135.149(c) Equipment requirements: General: Gyroscopic bank-and-pitch indicators - third indicator.

Compliant

EMB-500 IESI (stand by) is the 3rd attitude indicator in compliance with 121.305

Agree

135.149(d) Equipment requirements: General: Reserved. Not Applicable

Reserved

Agree

135.149(e) Equipment requirements: General - turbine powered aircraft


Unknown requirements

Agree

135.150 Public address and crewmember interphone systems. Not Applicable

Applicable only to aircraft with passenger seating configuration, excluding any pilot seat, of more than 19

Agree

135.151 Cockpit voice recorders. Title Only

-

Agree

135.151(a) Cockpit voice recorders: Installation Requirements. Not Applicable


Agree

135.151(b) Cockpit voice recorders: Installation Requirements. Not Applicable

Applicable only to multiengine, turbine-powered airplane having a passenger seating configuration of 20 or more seats

Agree

135.151(c) Cockpit voice recorders: Accident Reporting Requirements.


-

Agree

135.151(d) Cockpit voice recorders: Boom and Mask Microphone. Not Applicable


Agree

135.151(e) Cockpit voice recorders: Recorded Data. Not Applicable


Agree

135.151(f) Cockpit voice recorders: If Flight Data Recorder is required.

Not Applicable


Agree


A-52


135.151(g)(1) Cockpit voice recorders: If Flight Data Recorder is required.

Not Applicable


Agree

135.151(g)(2) Cockpit voice recorders: If Flight Data Recorder is required (for 20 pax or more).

Not Applicable

Applicable only for aircraft with passenger configuration of 20 or more.

Agree

135.151(h) Cockpit voice recorders: Datalink communication equipment.

Not Applicable


Agree

135.152 Flight recorders. Title Only

-

Agree

135.152(a) Flight recorders: Requirements. Not Applicable

Applicable only to multi-engine, turbine-engine powered airplane or rotorcraft having a passenger seating configuration, excluding any required crewmember seat, of 10 to 19 seats

Agree

135.152(b) Flight recorders. Not Applicable

Applicable only to multiengine, turbine-powered airplane having a passenger seating configuration of 20 to 30 seats.

Agree

135.152(c) Flight recorders: Operations. Operator’s Responsibility

-

Agree

135.152(d) Flight recorders: Recorded Data Requirements. Operator’s Responsibility

-

Agree

135.152(e) Flight recorders: Accident Reporting Requirements. Operator’s Responsibility

-

Agree

135.152(f)(1) Flight recorders: Installation Requirements. Not Applicable

Applicable only to airplanes manufactured on or before August 18, 2000.

Agree

135.152(f)(2) Flight recorders: Installation Requirements. Not Applicable

Applicable only to flight data recorder system required by section 135.152

Agree

135.152(g) Flight recorders: Underwater Locator Device. Not Applicable

Applicable only to flight data recorder system required by section 135.152.

Agree

135.152(h) Flight recorders: Parameters required to be recorded. Not Applicable Applicable only to FDR required on Agree


A-53


135.152(i)or 135.152(j)

135.152(i) Flight recorders. Not Applicable

Applicable only to turbine-engine powered airplanes with a seating configuration, excluding any required crewmember seat, of 10 to 30 passenger seats, manufactured after August 18, 2000.

Agree

135.152(j) Flight recorders. Not Applicable

Applicable only to turbine-engine-powered airplanes with a seating configuration, excluding any required crewmember seat, of 10 to 30 passenger seats, that are manufactured after August 19, 2002

Agree

135.152(k) Flight recorders. Not Applicable

Applicable only to aircraft manufactured before August 18, 1997

Agree

135.152(l) Flight recorders: Requirements. Not Applicable

EMB-500 is not required to have FDR.

Agree

135.152(m) Flight recorders: Requirements. Not Applicable

EMB-500 is not required to have FDR.

Agree

135.153 Ground proximity warning system. Not Applicable

Applicable only to turbine-powered airplane having a passenger seat configuration of 10 seats or more.

Agree

135.154 Terrain awareness and warning system. Title Only

-

Agree

135.154(a) Terrain awareness and warning system: System Installation Requirements.

Title Only

-

Agree

135.154(a)(1) Terrain awareness and warning system: System Installation Requirements.

Not Applicable

Applicable only to turbine-powered airplane configured with 10 or more passenger seats.

Agree

135.154(a)(2) Terrain awareness and warning system: System Installation Requirements.

Compliant

EMB-500 has TAWS B compliant with TSO C151.

Agree

135.154(b) Terrain awareness and warning system. Not Applicable

Applicable only to airplanes manufactured on or before March 29, 2002

Agree


A-54


135.154(c) Terrain awareness and warning system: Airplane Flight Manual.

Compliant

The AFM will contain appropriate procedures for the terrain awareness and warning system use; and proper flight crew reaction in response to the terrain awareness and warning system audio and visual warnings.

Agree

135.155 Fire extinguishers: Passenger-carrying aircraft. Compliant

One fire extinguisher is provided on the cockpit area, behind the copilot seat, filled with Halon 1211/1301 blend rated for classes B and C types of fire. Since the maximum capacity of the EMB-500 is 6 passengers, a fire extinguisher inside the passenger cabin is not required.

TBD

135.157 Oxygen equipment requirements. Compliant

EMB-500 is pressurized to 8,000 feet equivalent pressure. In the event of a decompression, emergency oxygen is provided to all occupants. Two hours each crew and 30 minutes for each passenger for emergency descent to 10,000 feet are provided. The oxygen system includes a cockpit pressure display for monitoring the system status, as well as pressure sensors in the low pressure supply line. Each crew mask stowage box includes a flow indicator to show when oxygen flow is supplied to the mask. The indicator is a pneumatic "star burst" attached to the valve and visible through the door. Each passenger mask includes a flow indicator to show when oxygen is flowing to the mask. The crew mask has a 100% setting to supply undiluted oxygen at all altitudes, including those above 25,000 feet.

TBD

135.158 Pitot heat indication systems. Not Applicable

Applicable only to transport category airplanes.

Agree

135.159 Equipment requirements: Carrying passengers under VFR at night or under VFR over-the-top conditions.

Title Only

-

Agree

135.159(a) Equipment requirements: Gyroscopic rate-of-turn indicator.

Not Applicable

EMB-500 has a 3rd attitude indicator.

Agree


A-55


135.159(b) Equipment requirements: Slip skid indicator. Compliant

EMB-500 PFD presents a slip skid indicator

Agree

135.159(c) Equipment requirements: Gyroscopic bank-and-pitch indicator.

Compliant

EMB-500 PFD presents an attitude indicator driven by the Attitude and Heading Reference System

Agree

135.159(d) Equipment requirements: Gyroscopic direction indicator.

Compliant

EMB-500 PFD presents a heading indicator driven by the Attitude and Heading Reference System.

Agree

135.159(e) Equipment requirements: Generator or generators. Compliant

Compliance with FAR 23.1309 (c) Compliance with FAR 23.1351 (a) Compliance with FAR 23.1351 (c)

Agree

135.159(f) Equipment requirements: For night flights. Title Only

-

Agree

135.159(f)(1) Equipment requirements: For night flights: Anticollision light system.

Compliant

EMB-500 is equipped with approved Anti-collision lights.

Agree

135.159(f)(2) Equipment requirements: For night flights: Instrument lights.

Compliant

EMB-500 instrument lights make all instruments, switches, and gauges easily readable, the direct rays of which are shielded from the pilots' eyes;

Agree

135.159(f)(3) Equipment requirements: For night flights: Flashlight. Compliant

Flashlights are provided, installed behind each cockpit seat.

TBD

135.159(g) Equipment requirements: Continuous in-flight electrical load.

Definition

-

Agree

135.159(h) Equipment requirements: Helicopters. Not Applicable

Applicable only to helicopters

Agree

135.161 Communication and navigation equipment for aircraft operations under VFR over routes navigated by pilotage.

Compliant

EMB-500 has as baseline 2 VHF Comm/ Nav (VOR) and 2 GPS. If other communication and/or navigation devices are required due to the route to be flown it is operator’s responsibility to have

Agree


A-56


selected them on the optional list (HF, ADF, DME).

135.163 Equipment requirements: Aircraft carrying passengers under IFR.

Title Only

-

Agree

135.163(a) Equipment requirements: Aircraft carrying passengers under IFR: Vertical speed indicator.

Compliant

Each EMB-500 PFD has an Vertical Speed Indicator

Agree

135.163(b) Equipment requirements: Aircraft carrying passengers under IFR: Free-air temperature indicator.

Compliant

SAT and OAT are indicated on the PFDs from inputs sent by the Powerplant sensors.

Agree

135.163(c) Equipment requirements: Aircraft carrying passengers under IFR: Heated pitot tube for each airspeed indicator.

Compliant

EMB-500 has a heated pitot tube for each airspeed indicator.

Agree

135.163(d) Equipment requirements: Aircraft carrying passengers under IFR: Power failure warning device.

Compliant

Each Gyroscopic Instrument Power is monitored by a CAS message or its failure is evident.

Agree

135.163(e) Equipment requirements: Aircraft carrying passengers under IFR: Alternate source of static pressure.

Compliant

EMB-500 has 3 independent static source systems (3 ADS)

Agree

135.163(f) Equipment requirements: Aircraft carrying passengers under IFR: Single-engine aircraft.

Not Applicable

Applicable only to single-engine aircraft

Agree

135.163(g) Equipment requirements: Aircraft carrying passengers under IFR: Generators or alternators.

Compliant

Compliance with FAR 23.1309 (c) Compliance with FAR 23.1351 (a) Compliance with FAR 23.1351 (c)

Agree

135.163(h) Equipment requirements: Aircraft carrying passengers under IFR: Two independent sources of energy.

Compliant

The 3 attitude systems are electrically independent. AHRS1 and PFD1 are powered by EMERGENCY BUS, AHRS 2 and PFD2 are powered by DC BUS 2 and standby is powered by both DC BUS1 and EMERGENCY BUS.

Agree

135.163(i) Equipment requirements: Aircraft carrying passengers under IFR: Continuous in-flight electrical load.

Definition

-

Agree

135.165 Radio and navigational equipment: Extended overwater or IFR operations.

Title Only

-

Agree


A-57


135.165(a) Aircraft navigation equipment requirements: General. Title Only

-

Agree

135.165(a)(1) Aircraft navigation equipment requirements: General. Operator’s Responsibility

-

Agree

135.165(a)(2) Aircraft navigation equipment requirements: General. Compliant

For extended over water operation the EMB-500 is equipped with 2 independent GPS systems.

Agree

135.165(a)(3) Aircraft navigation equipment requirements: General. Compliant

EMB-500 exceeds the requirement by having 2 Marker Beacon (1 on each audio panel)and 2 ILS receivers (1 on each GIA)

Agree

135.165(a)(4) Aircraft navigation equipment requirements: General. Operator’s Responsibility

-

Agree

135.165(b) Radio and navigational equipment: Extended overwater or IFR operations


-

Agree

135.165(c) Radio and navigational equipment: Extended overwater or IFR operations: Receiver/Transmitter Definition

Compliant

EMB-500 has 2 RNAV systems (GPS)

Agree

135.165(d) Radio and navigational equipment: Extended overwater or IFR operations

Not Applicable

Applicable only to turbojet airplane having a passenger seat configuration, excluding any pilot seat, of 10 seats or more, or a multiengine airplane in a commuter operation

Agree

135.165(e) Radio and navigational equipment: Extended overwater or IFR operations


EMB-500 is equipped with 2 independent VHF Communication System. If other communication system is required for the route such as HF, it is operator’s responsibility to select it from the optional guide.

Agree

135.165(f) Radio and navigational equipment: Extended overwater or IFR operations

Compliant

EMB-500 has 2 headsets with mic and 2 speakers

TBD

135.165(g) Radio and navigational equipment: Extended overwater or IFR operations


-

Agree


A-58


135.167 Emergency equipment: Extended overwater operations.

Title Only

-

Agree

135.167(a) Emergency equipment: Extended overwater operations Introduction

-

Agree

135.167(a)(1) Emergency equipment: Extended overwater operations Optionally Compliant

Life vests are optional items.

Agree

135.167(a)(2) Emergency equipment: Extended overwater operations Not Compliant

Life rafts are follow-on certification items.

Agree

135.167(b) Emergency equipment: Extended overwater operations Not Compliant

Life rafts are follow-on certification items.

Agree

135.167(c) Emergency equipment: Extended overwater operations Not Compliant Life rafts are follow-on certification items. For the controlled life items, it is delivered to the customer a report with the useful life status.

Agree


Reserved.

Agree

135.169 Additional airworthiness requirements. Title Only

-

Agree

135.169(a) Additional airworthiness requirements Not Applicable

Applicable only to large, non-commuter category airplanes.

Agree

135.169(b) Additional airworthiness requirements. Not Applicable

Applicable only to reciprocating-engine or turbopropeller-powered small airplane that has a passenger seating configuration, excluding pilot seats, of 10 seats or more.

Agree

135.169(c) Additional airworthiness requirements. Not Applicable

Applicable only to small airplanes with a passenger seating configuration, excluding any pilot seat, of 10 seats or more,

Agree

135.169(d) Additional airworthiness requirements: Cargo or baggage compartments

Not Applicable


Agree


A-59


135.170 Materials for compartment interiors. Title Only

-

Agree

135.170(a) Materials for compartment interiors Not Applicable

Applicable only to aircraft with a supplemental type certificate issued in accordance with SFAR No. 41 for a maximum certificated takeoff weight in excess of 12,500 pounds

Agree

135.170(b) Materials for compartment interiors Not Applicable


Agree

135.170(c) Materials for compartment interiors Not Applicable


Agree

135.171 Shoulder harness installation at flight crewmember stations.

Title Only

-

Agree

135.171(a) Shoulder harness installation at flight crewmember stations

Not Applicable

EMB-500 maximum capacity is 6 passengers, excluding pilot seats.

Agree

135.171(b) Shoulder harness installation at flight crewmember stations


-

Agree

135.173 Airborne thunderstorm detection equipment requirements.

Not Applicable

Applicable only to aircraft that has a passenger seating configuration, excluding any pilot seat, of 10 seats or more in passenger-carrying operations.

Agree

135.175 Airborne weather radar equipment requirements. Not Applicable

Applicable only to large, transport category aircraft in passenger-carrying operations.

Agree

135.177 Emergency equipment requirements for aircraft having a passenger seating configuration of more than 19 passengers.

Not Applicable

Applicable only to aircraft having a passenger seating configuration, excluding any pilot seat, of more than 19 seats.

Agree

135.178 Additional emergency equipment. Not Applicable

Applicable only to airplane having a passenger seating configuration of more than 19 seats

Agree


A-60


135.179 Inoperable instruments and equipment. Compliant


Agree

135.180 Traffic Alert and Collision Avoidance System. Not Applicable


Agree

135.181 Performance requirements: Aircraft operated over-the-top or in IFR conditions.

Title Only

-

Agree

135.181(a) Performance requirements: Aircraft operated over-the-top or in IFR conditions.

Title Only

-

Agree

135.181(a)(1) Performance requirements: Aircraft operated over-the-top or in IFR conditions.

Not Applicable

Applicable only to single engine airplanes.

Agree


Compliant

EMBRAER issues and furnishes the operational manuals, with the required performance data, inside each airplane factory delivered.

TBD

135.181(b) Performance requirements: Aircraft operated over-the-top or in IFR conditions.

Not Applicable

Applicable only to multiengine helicopters

Agree

135.181(c) Performance requirements: Aircraft operated over-the-top or in IFR conditions.


-

Agree

135.181(d) Performance requirements: Aircraft operated over-the-top or in IFR conditions.


-

Agree

135.183 Performance requirements: Land aircraft operated over water.

Title Only

-

Agree

135.183(a), 135.183(b)

Performance requirements: Land aircraft operated over water.


-

Agree

135.183(c) Performance requirements: Land aircraft operated over water.

Compliant

EMBRAER issues and furnishes the operational manuals, with the required performance data, inside each airplane factory delivered.

Agree


A-61


135.183(d) Performance requirements: Land aircraft operated over water.

Not Applicable

Applicable only for helicopter.

Agree

135.185 Empty weight and center of gravity: Currency requirement.

Compliant

The empty weight and center of gravity is measured and delivery with the airplane documentation.

TBD

EMB-500, Part 135 Compliance Subpart D - VFR/IFR Operating Limitations and Weather Requirements



-

Agree

135.203 VFR: Minimum altitudes. Operator’s Responsibility

-

Agree

135.205 VFR: Visibility requirements. Operator’s Responsibility

-

Agree

135.207 VFR: Helicopter surface reference requirements. Not Applicable

Applicable only to Helicopter Operations

Agree

135.209 VFR: Fuel supply. Operator’s Responsibility

-

Agree

135.211 VFR: Over-the-top carrying passengers: Operating limitations.


-

Agree

135.213 Weather reports and forecasts. Operator’s Responsibility

-

Agree

135.215 IFR: Operating limitations. Operator’s Responsibility

-

Agree

135.217 IFR: Takeoff limitations. Operator’s Responsibility - Agree


A-62


135.219 IFR: Destination airport weather minimums. Operator’s Responsibility

-

Agree

135.221 IFR: Alternate airport weather minimums. Operator’s Responsibility

-

Agree

135.223 IFR: Alternate airport requirements. Operator’s Responsibility

-

Agree

135.225 IFR: Takeoff, approach and landing minimums. Operator’s Responsibility

-

Agree

135.227 Icing conditions: Operating limitations. Title Only

-

Agree

135.227(a) Icing conditions: Operating limitations Operator’s Responsibility

-

Agree

135.227(b) Icing conditions: Operating limitations Operator’s Responsibility

-

Agree

135.227(c) Icing conditions: Operating limitations Compliant

EMB-500 will accomplish this requirement when get type certification to fly in icing conditions inside FAR 25 Appendix C envelope. EMB-500 has ice protection system installed on the following regions: Wing Leading edges; Horizontal Stabilizer Leading edges; Nacelle inlet; Windshield; Air probes.

Agree

135.227(d) Icing conditions: Operating limitations Not Applicable

Applicable only to helicopter operations.

Agree

135.227(e) Icing conditions: Operating limitations Compliant

EMB-500 will accomplish this requirement when get type certification to fly in icing conditions inside FAR 25 Appendix C envelope. EMB-500 has ice protection system installed on the following regions: Wing Leading edges; Horizontal Stabilizer Leading edges; Nacelle inlet; Windshield; Air probes.

Agree


A-63


135.227(f) Icing conditions: Operating limitations Operator’s Responsibility

-

Agree

135.229 Airport requirements. Operator’s Responsibility

-

Agree

EMB-500, Part 135 Compliance Subpart E - Flight Crewmember Requirements



-

Agree

135.243 Pilot in command qualifications. Operator’s Responsibility

-

Agree

135.244 Operating experience. Operator’s Responsibility

-

Agree

135.245 Second in command qualifications. Operator’s Responsibility

-

Agree

135.247 Pilot qualifications: Recent experience. Operator’s Responsibility

-

Agree

135.249 Use of prohibited drugs. Operator’s Responsibility

-

Agree

135.251 Testing for prohibited drugs. Operator’s Responsibility

-

Agree

135.253 Misuse of alcohol. Operator’s Responsibility

-

Agree

135.255 Testing for alcohol. Operator’s Responsibility

-

Agree


A-64


Subpart F - Crewmember Flight Time and Duty Period Limitations and Rest Requirements



-

Agree

135.263 Flight time limitations and rest requirements: All certificate holders.


-

Agree

135.265 Flight time limitations and rest requirements: Scheduled operations.


-

Agree

135.267 Flight time limitations and rest requirements: Unscheduled one- and two-pilot crews.


-

Agree

135.269 Flight time limitation and rest requirements: Unscheduled three- and four-pilot crews.

Not Applicable

Applicable only for operations with three- or four-pilot crew.

Agree

135.271 Helicopter hospital emergency medical evacuation service (HEMES).

Not Applicable

Applicable only to Helicopter hospital emergency medical evacuation service operations.

Agree

135.273 Duty period limitations and rest time requirements. Not Applicable

Applicable only to operations with flight attendants.

Agree

EMB-500, Part 135 Compliance Subpart G - Crewmember Testing Requirements



-

Agree

135.293 Initial and recurrent pilot testing requirements. Operator’s Responsibility

-

Agree

135.295 Initial and recurrent flight attendant crewmember Not Applicable Applicable only to operations with Flight Agree


A-65


testing requirements.

Attendants.

135.297 Pilot in command: Instrument proficiency check requirements.


-

Agree

135.299 Pilot in command: Line checks: Routes and airports. Operator’s Responsibility

-

Agree


Definition

-

Agree

EMB-500, Part 135 Compliance Subpart H - Training


135.321 Applicability and terms used. Definition

-

Agree

135.323 Training program: General. Operator’s Responsibility

-

Agree

135.324 Training program: Special rules. Operator’s Responsibility

-

Agree



-

Agree

135.327 Training program: Curriculum. Operator’s Responsibility

-

Agree

135.329 Crewmember training requirements. Operator’s Responsibility

-

Agree

135.331 Crewmember emergency training. Operator’s Responsibility

-

Agree

135.335 Approval of aircraft simulators and other training Operator’s Responsibility - Agree


A-66


devices.

135.337 Qualifications: Check airmen (aircraft) and check airmen (simulator).


-

Agree



-

Agree

135.339 Initial and transition training and checking: Check airmen (aircraft), check airmen (simulator).


-

Agree



-

Agree



-

Agree



-

Agree

135.345 Pilots: Initial, transition, and upgrade ground training. Operator’s Responsibility

-

Agree

135.347 Pilots: Initial, transition, upgrade, and differences flight training.


-

Agree

135.349 Flight attendants: Initial and transition ground training. Not Applicable

Applicable only to operations with Flight Attendants.

Agree


-

Agree

135.353 Prohibited drugs. Operator’s Responsibility

-

Agree

EMB-500, Part 135 Compliance Subpart I - Airplane Performance Operating Limitations


A-67



-

Agree


-

Agree

135.364 Maximum flying time outside the United States. Operator’s Responsibility

-

Agree

135.365 Large transport category airplanes: Reciprocating engine powered: Weight limitations.

Not Applicable

Applicable only to reciprocating engine powered large transport category airplane.

Agree

135.367 Large transport category airplanes: Reciprocating engine powered: Takeoff limitations.

Not Applicable


Agree

135.369 Large transport category airplanes: Reciprocating engine powered: En route limitations: All engines operating.

Not Applicable


Agree

135.371 Large transport category airplanes: Reciprocating engine powered: En route limitations: One engine inoperative.

Not Applicable


Agree

135.373 Part 25 transport category airplanes with four or more engines: Reciprocating engine powered: En route limitations: Two engines inoperative.

Not Applicable


Agree

135.375 Large transport category airplanes: Reciprocating engine powered: Landing limitations: Destination airports.

Not Applicable


Agree

135.377 Large transport category airplanes: Reciprocating engine powered: Landing limitations: Alternate airports.

Not Applicable


Agree

135.379 Large transport category airplanes: Turbine engine powered: Takeoff limitations.

Not Applicable


Agree

135.381 Large transport category airplanes: Turbine engine powered: En route limitations: One engine inoperative.

Not Applicable


Agree

135.383 Large transport category airplanes: Turbine engine powered: En route limitations: Two engines inoperative.

Not Applicable


Agree

135.385 Large transport category airplanes: Turbine engine Not Applicable Applicable only to turbine engine powered Agree


A-68


powered: Landing limitations: Destination airports.

large transport category airplane.

135.387 Large transport category airplanes: Turbine engine powered: Landing limitations: Alternate airports.

Not Applicable


Agree

135.389 Large nontransport category airplanes: Takeoff limitations.

Not Applicable

Applicable only to large non-transport category airplane

Agree

135.391 Large nontransport category airplanes: En route limitations: One engine inoperative.

Not Applicable

Applicable only to large non-transport category airplane.

Agree

135.393 Large nontransport category airplanes: Landing limitations: Destination airports.

Not Applicable


Agree

135.395 Large nontransport category airplanes: Landing limitations: Alternate airports.

Not Applicable


Agree

135.397 Small transport category airplane performance operating limitations.


-

Agree

135.398 Commuter category airplanes performance operating limitations.

Not Applicable

Applicable only to commuter category airplanes.

Agree

135.399 Small nontransport category airplane performance operating limitations

Not Applicable

Applicable only to reciprocating-engine or turbopropeller-powered small airplane that has a passenger seating configuration, excluding pilot seats, of 10 seats or more

Agree

EMB-500 14CFR135 Compliance Subpart J - Maintenance, Preventive Maintenance, and Alterations



-

Agree

135.413 Responsibility for airworthiness. Operator’s Responsibility

-

Agree


A-69


135.415 Service difficulty reports. Operator’s Responsibility

-

Agree

135.417 Mechanical interruption summary report. Operator’s Responsibility

-

Agree

135.419 Approved aircraft inspection program. Compliant

The EMBRAER Recommended Scheduled Maintenance Program will be included in the Aircraft Maintenance Manual. The instructions and procedures required to execute the aircraft inspections will be issued in the Aircraft Maintenance Manual, and for correction of discrepancies found will be issued in the Fault Isolation Manual.

TBD

135.421 Additional maintenance requirements. Title Only

-

Agree

135.421(a) Additional maintenance requirements: Maintenance Program

Compliant

EMBRAER will recommend a Scheduled Maintenance Program.

TBD

135.421(b) Additional maintenance requirements: Manufacturer Maintenance Plan - Definition

Definition

-

Agree

135.421(c) Additional maintenance requirements Not Applicable

Applicable only to single engine aircraft to be used in passenger-carrying IFR operations.

Agree

135.421(d) Additional maintenance requirements Not Applicable


Agree

135.421(e) Additional maintenance requirements Not Applicable


Agree

135.422 Aging airplane inspections and records reviews for multiengine airplanes certificated with nine or fewer passenger seats.


-

Agree

135.423 Maintenance, preventive maintenance, and alteration organization.


-

Agree

135.425 Maintenance, preventive maintenance, and alteration programs.


-

Agree


A-70



-

Agree

135.429 Required inspection personnel. Operator’s Responsibility

-

Agree

135.431 Continuing analysis and surveillance. Operator’s Responsibility

-

Agree

135.433 Maintenance and preventive maintenance training program.


-

Agree

135.435 Certificate requirements. Operator’s Responsibility

-

Agree

135.437 Authority to perform and approve maintenance, preventive maintenance, and alterations.


-

Agree

135.439 Maintenance recording requirements. Compliant

For each new aircraft delivered, maintenance recording are issued to demonstrate that all requirements for issuance of airworthiness were complied. The total time in service of the engine, propeller, and rotor are registered in the log book.

TBD

135.441 Transfer of maintenance records. Compliant


TBD

135.443 Airworthiness release or aircraft log entry. Compliant

Each airplane is delivered with airworthiness released and all maintenance records are entry on the documentation delivered.

TBD

EMB-500, Part 135 Compliance Subpart K - Hazardous Materials Training Program



A-71


135.501 Applicability and definitions. Definition

-

Agree

135.503 Hazardous material training: General. Operator’s Responsibility

-

Agree

135.505 Hazardous materials training required. Operator’s Responsibility

-

Agree

135.507 Hazardous materials training records. Operator’s Responsibility

-

Agree

EMB-500, Part 135 Compliance Appendix A to Part 135 - Additional Airworthiness Standards for 10 or More Passenger Airplanes


Appendix A Additional Airworthiness Standards for 10 or More Passenger Airplanes

Not Applicable

Applicable only to airplanes for 10 or More Passengers.

Agree

EMB-500, Part 135 Compliance Appendix B to Part 135 - Airplane Flight Recorder Specifications


Appendix B Airplane Flight Recorder Specifications Not Applicable

FDR is not applicable to EMB-500

Agree

EMB-500, Part 135 Compliance Appendix C to Part 135 - Helicopter Flight Recorder Specifications


Appendix C Helicopter Flight Recorder Specifications Not Applicable Applicable only for helicopter flight recorder. Agree


A-72


EMB-500, Part 135 Compliance Appendix D to Part 135 - Airplane Flight Recorder Specification


Appendix D Airplane Flight Recorder Specification Not Applicable

FDR is not applicable to EMB-500

Agree

EMB-500, Part 135 Compliance Appendix E to Part 135 - Helicopter Flight Recorder Specifications


Appendix E Helicopter Flight Recorder Specifications Not Applicable

Applicable only for helicopter flight recorder.

Agree

EMB-500, Part 135 Compliance Appendix G to Part 135 - Extended Operations (ETOPS)


Appendix G Extended Operations (ETOPS) Not Applicable

Aircraft not certified for ETOPS operations.

Agree


A-73

APPENDIX A2 - AIRCRAFT REGULATORY COMPLIANCE CHECKLIST, EMBRAER EMB-505 Compliant - The compliance with referred item is OPERATOR’s responsibility and Embraer provides

necessary equipment/feature/manual/information in order to support the OPERATOR to

comply with referred statement.

Not Compliant - The compliance with referred item is OPERATOR’s responsibility and Embraer does not

provide necessary equipment/feature/manual/information to support the OPERATOR to

perform the referred operation.


A-74

Optionally

Compliant

- The compliance with referred item is OPERATOR’s responsibility and Embraer provides

necessary equipment/feature/manual/information as optional item(s) under OPERATOR’s

request to support the OPERATOR to perform the referred operation.

Not Applicable - The item is not applicable to this EMBRAER aircraft model.

Operator’s

Responsibility

- The compliance with referred item is exclusively OPERATOR’s responsibility and there

are no EMBRAER actions.

Definition - The item is a definition statement, no actions are required.

Title Only - The item is subdivided and individual subitems analyses are presented subsequently.


A-75

EMB-505 14CFR91 Compliance Subpart A - General



-

AGREE

91.3 Responsibility and authority of the pilot in command.


-

AGREE

91.5 Pilot in command of aircraft requiring more than one required pilot.


-

AGREE

91.7 Civil aircraft airworthiness.


-

AGREE

91.9 Civil aircraft flight manual, marking, and placard requirements.

Title Only

-

AGREE

91.9(a) Civil aircraft flight manual, marking, and placard requirements: Limitations, markings and placards.


-

AGREE

91.9(b) Civil aircraft flight manual, marking, and placard requirements: Manual availability.

Compliant

Embraer will furnish one updated AFM copy for each factory delivered airplane.

AGREE

91.9(c) Civil aircraft flight manual, marking, and placard requirements: Part 45.

Compliant

All markings required by part 45 of this chapter are installed.

AGREE

91.9(d) Civil aircraft flight manual, marking, and placard requirements: Helicopter operation.

Not Applicable

Applicable only to Helicopter Operation.

AGREE

91.11 Prohibition on interference with crewmembers.


-

AGREE

91.13 Careless or reckless operation.


-

AGREE

91.15 Dropping objects. Operator’s Responsibility

-

AGREE

91.17 Alcohol or drugs. Operator’s Responsibility

-

AGREE

91.19 Carriage of narcotic drugs, marihuana, and depressant or stimulant


-

AGREE


A-76


drugs or substances.

91.21 Portable electronic devices.


-

AGREE

91.23 Truth-in-leasing clause requirement in leases and conditional sales contracts.


-

AGREE

91.25 Aviation Safety Reporting Program: Prohibition against use of reports for enforcement purposes.

Definition

-

AGREE

91.27-91.99 Reserved Not Applicable

Reserved.

AGREE

EMB-505 14CFR91 Compliance Subpart B - Flight Rules

FSB FINDING



-

AGREE

91.103 Preflight action. Operator’s Responsibility

-

AGREE

91.105 Flight crewmembers at stations.

Compliant

EMB-505 is provided with pilot and co-pilot seats inside the cockpit area equipped with 5-points restraint system; and passenger seats inside the cabin area, provided with 3-points restraint system.

AGREE

91.107 Use of safety belts, shoulder harnesses, and child restraint systems.

Compliant

EMB-505 is provided with pilot and co-pilot seats inside the cockpit area, provided with 5-points restraint system; and passenger seats inside the cabin area, provided with 3-points restraint system.

AGREE

91.109 Flight instruction; Simulated instrument flight and certain flight tests.


-

AGREE

91.111 Operating near other aircraft.


-

AGREE

91.113 Right-of-way rules: Except water operations.


-

AGREE

91.115 Right-of-way rules: Water operations.

Not Applicable

Applicable only for aircraft operating on the water.

AGREE

91.117 Aircraft speed. Operator’s Responsibility

-

AGREE


A-77


91.119 Minimum safe altitudes: General.


-

AGREE

91.121 Altimeter settings. Operator’s Responsibility

-

AGREE

91.123 Compliance with ATC clearances and instructions.


-

AGREE

91.125 ATC light signals. Definition

-

AGREE

91.126 Operating on or in the vicinity of an airport in Class G airspace.


-

AGREE

91.127 Operating on or in the vicinity of an airport in Class E airspace.


-

AGREE

91.129 Operations in Class D airspace.


-

AGREE

91.130 Operations in Class C airspace.


-

AGREE

91.131 Operations in Class B airspace.


-

AGREE

91.133 Restricted and prohibited areas.


-

AGREE

91.135 Operations in Class A airspace.


-

AGREE

91.137 Temporary flight restrictions in the vicinity of disaster/hazard areas.


-

AGREE

91.138 Temporary flight restrictions in national disaster areas in the State of Hawaii.


-

AGREE

91.139 Emergency air traffic rules.


-

AGREE

91.141 Flight restrictions in the proximity of the Presidential and other parties.


-

AGREE

91.143 Flight limitation in the proximity of space flight operations.


-

AGREE

91.144 Temporary restriction on Operator’s Responsibility - AGREE


A-78


flight operations during abnormally high barometric pressure conditions.

91.145 Management of aircraft operations in the vicinity of aerial demonstrations and major sporting events.


-

AGREE

91.146 Passenger-carrying flights for the benefit of a charitable, nonprofit, or community event.

Definition

-

AGREE

91.147 Passenger carrying flights for compensation or hire.


-

AGREE


Reserved.

AGREE

91.151 Fuel requirements for flight in VFR conditions.


-

AGREE

91.153 VFR flight plan: Information required.


-

AGREE

91.155 Basic VFR weather minimums.


-

AGREE

91.157 Special VFR weather minimums.


-

AGREE

91.159 VFR cruising altitude or flight level.


-

AGREE


Reserved.

AGREE

91.167 Fuel requirements for flight in IFR conditions.


-

AGREE

91.169 IFR flight plan: Information required.


-

AGREE

91.171 VOR equipment check for IFR operations.


-

AGREE

91.173 ATC clearance and flight plan required.


-

AGREE

91.175 Takeoff and landing under IFR.


-

AGREE

91.177 Minimum altitudes for IFR operations.


-

AGREE


A-79


91.179 IFR cruising altitude or flight level.


-

AGREE

91.180 Operations within airspace designated as Reduced Vertical Separation Minimum airspace.


-

AGREE

91.181 Course to be flown. Operator’s Responsibility

-

AGREE

91.183 IFR communications. Operator’s Responsibility

-

AGREE

91.185 IFR operations: Two-way radio communications failure.


-

AGREE

91.187 Operation under IFR in controlled airspace: Malfunction reports.


-

AGREE

91.189 Category II and III operations: General operating rules.

Not Applicable

EMB-505 does not have CAT II or CAT III Capabilities.

AGREE

91.191 Category II and Category III manual.

Not Applicable

EMB-505 does not have CAT II or CAT III Capabilities.

AGREE

91.193 Certificate of authorization for certain Category II operations.

Not Applicable

EMB-505 does not have CAT II Capability.

AGREE


Reserved.

AGREE

EMB-505 14CFR91 Compliance Subpart C - Equipment, Instrument, and Certificate Requirements



Item is Reserved - no requirement

AGREE

91.203 Civil aircraft: Certifications required.

Title Only

-

AGREE

91.203(a) Civil aircraft: Certifications required: Airworthiness and U.S. registration certificates.


-

AGREE

91.203(b) Civil aircraft: Certifications required: Airworthiness certificate


-

AGREE


A-80


or special flight authorization.

91.203(c) Civil aircraft: Certifications required: Fuel tank installed within the passenger compartment or a baggage compartment.


-

AGREE

91.203(d) Civil aircraft: Certifications required: Fuel venting and exhaust emissions requirements.

Compliant

The PW535E engine is certified to 14 CFR 33 (Engine Type Certificate) and the emission requirements are specified in AWM 516 (change 516-7. This is equivalent to 14 CFR Part 34 up to and including Amendment 3), which points to the ICAO annex 16 standards.

AGREE

91.205 Powered civil aircraft with standard category U.S. airworthiness certificates: Instrument and equipment requirements.

Title Only

-

AGREE

91.205(a) Powered civil aircraft with standard category U.S. airworthiness certificates: Instrument and equipment requirements: General.


-

AGREE

91.205(b) Powered civil aircraft with standard category U.S. airworthiness certificates: Instrument and equipment requirements: Visual-flight rules (day).

Title Only

-

AGREE

91.205(b)(1) Visual-flight rules (day): Airspeed indicator.

Compliant

Comply according to 14 CFR 23.1303 (a).

AGREE

91.205(b)(2) Visual-flight rules (day): Altimeter.

Compliant

Comply according to 14 CFR 23.1303 (b)

AGREE

91.205(b)(3) Visual-flight rules (day): Magnetic direction indicator.

Compliant

Comply according to 14 CFR 23.1303 (c)

AGREE

91.205(b)(4) Visual-flight rules (day): Tachometer.

Compliant

There are engine parameters indication (N1 and N2) on MFD. Comply according to 14 CFR 23.1305 (c)(5).

AGREE

91.205(b)(5) Visual-flight rules (day): Oil pressure gauge.

Compliant

There is an oil pressure indication on MFD. Comply according to 14 CFR 23.1305 (a)(2)

AGREE

91.205(b)(6) Visual-flight rules (day): Temperature gauge.

Not Applicable

EMB-505 does not have a liquid-cooled engine.

AGREE


A-81


91.205(b)(7) Visual-flight rules (day): Oil temperature gauge.

Compliant

There is an oil temperature indication on MFD. Comply according to 14 CFR 23.1305 (a)(3).

AGREE

91.205(b)(8) Visual-flight rules (day): Manifold pressure gauge.

Not Applicable

Applicable only for aircraft equipped with an altitude engine.

AGREE

91.205(b)(9) Visual-flight rules (day): Fuel gauge.

Compliant

EMB-505 fuel system provides fuel quantity indication for each tank. Comply according to 14 CFR 23.1305 (a)(1).

AGREE

91.205(b)(10) Visual-flight rules (day): Landing gear position indicator.

Compliant

Comply according to 14 CFR 23.729 (e)

AGREE

91.205(b)(11) Visual-flight rules (day): Anticollision light system.

Compliant

EMB-505 is equipped with approved Anticollision lights.

AGREE

91.205(b)(12) Visual-flight rules (day): Flotation gear.

Not Compliant

Life vest pouches are provided under each seat for live vest installation. Installation of pyrotechnic signaling device is an operator responsibility.

AGREE

91.205(b)(13) Visual-flight rules (day): Safety belt.

Compliant

Each seat is provided with a metal-to-metal latching device, according to 14 CFR 23.785(b) requirement.

AGREE

91.205(b)(14) Visual-flight rules (day): Shoulder harness.

Not Applicable

Applicable only for 14 CFR Part 23 certified small civil airplanes.

AGREE

91.205(b)(15) Visual-flight rules (day): ELT.

Compliant


AGREE


Not Applicable

EMB-505 is a commuter category airplane.

AGREE


Not Applicable

Applicable only for rotorcraft manufactured after September 16, 1992.

AGREE

91.205(c) Powered civil aircraft with standard category U.S. airworthiness certificates: Instrument and equipment requirements: Visual flight rules (night).

Title Only

-

AGREE

91.205(c)(1) Visual flight rules (night): Instruments and equipment specified in paragraph (b).

Not Compliant

EMB-505 complies with all 91.205(b) requirements, with exception to item 91.205(b)(12).

AGREE

91.205(c)(2) Visual flight rules (night): Position lights.

Compliant

EMB-505 is equipped with approved Position lights.

AGREE

91.205(c)(3) Visual flight rules (night): Compliant EMB-505 is equipped with approved AGREE


A-82


Anticollision light system.

Anticollision lights.

91.205(c)(4) Visual flight rules (night): Electric landing light.

Compliant

EMB-505 is equipped with two Landing Lights installed in the belly fairing.

AGREE

91.205(c)(5) Visual flight rules (night): Source of electrical energy.

Compliant

Compliance with 14 CFR 23.1351(a) Compliance with 14 CFR 23.1351(c)

AGREE

91.205(c)(6) Visual flight rules (night): Spare set of fuses.

Not Applicable

There are no fuses accessible to the flight crew in flight.

AGREE

91.205(d) Powered civil aircraft with standard category U.S. airworthiness certificates: Instrument and equipment requirements: Instrument flight rules.

Title Only

-

AGREE

91.205(d)(1) Instrument flight rules: Instruments and equipment specified in paragraphs (b) and (c).

Not Compliant

EMB-505 complies with all 91.205(b) and (c) requirements, with exception to item 91.205(b)(12).

AGREE

91.205(d)(2) Instrument flight rules: Two-way radio communication and navigation equipment.

Compliant

EMB-505 has two baseline integrated units containing navigation (including a VOR/LOC/GS receiver and a GPS) and communication (VHF COM) radios. A single or dual DME, as well as a single ADF are also available as optional equipment.

AGREE

91.205(d)(3) Instrument flight rules: Gyroscopic rate-of-turn indicator.

Compliant

Gyroscopic rate-of-turn indicator replaced by a third attitude instrument system usable through flight attitudes of 360 degrees of pitch and roll. The third attitude instrument is powered by emergency bus that includes batteries, operates independently of any other attitude indicating system, is located on the instrument panel in a position usable by each pilot at his or her station and is appropriately lighted during all phases of operation.

AGREE

91.205(d)(4) Instrument flight rules: Slip-skid indicator.

Compliant

EMB-505 is equipped with a slip-skid indicator at each pilot display.

AGREE

91.205(d)(5) Instrument flight rules: Sensitive altimeter.

Compliant

Comply according to 14 CFR 23.1303 (b),(g)(2). Each altimeter is barometric adjustable.

AGREE

91.205(d)(6) Instrument flight rules: Clock.

Compliant

PFD shows a clock with hours and minutes and seconds in a digital format.

AGREE

91.205(d)(7) Instrument flight rules: Generator or alternator.

Compliant

Compliance with 14 CFR 23.1351(a). Compliance with 14 CFR 23.1351(c).

AGREE

91.205(d)(8) Instrument flight rules: Gyroscopic pitch and bank indicator.

Compliant

EMB-505 is equipped with pitch and bank indicator (artificial horizon) at each pilot display. Compliant with 14 CFR 23.1321

AGREE


A-83


(d)(1).

91.205(d)(9) Instrument flight rules: Gyroscopic direction indicator.

Compliant

EMB-505 is equipped with direction indicator (magnetic heading) at each pilot display. Compliant with 14 CFR 23.1321 (d)(4).

AGREE

91.205(e) Powered civil aircraft with standard category U.S. airworthiness certificates: Instrument and equipment requirements: Flight at and above 24,000 ft MSL (FL 240).

Compliant

EMB-505 is equipped with a suitable RNAV system.

AGREE

91.205(f) Powered civil aircraft with standard category U.S. airworthiness certificates: Instrument and equipment requirements: Category II operations.

Not Applicable

Aircraft does not have CAT II capabilities

AGREE

91.205(g) Powered civil aircraft with standard category U.S. airworthiness certificates: Instrument and equipment requirements: Category III operations.

Not Applicable

Aircraft does not have CAT III capabilities

AGREE

91.205(h) Powered civil aircraft with standard category U.S. airworthiness certificates: Instrument and equipment requirements: Exclusions.

Not Applicable

Refer to Part 91.205(f) and 91.205(g).

AGREE

91.207 Emergency locator transmitters.

Title Only

-

AGREE

91.207(a) Emergency locator transmitters: Approved automatic type.

Compliant


AGREE

91.207(b) Emergency locator transmitters: Attachment.

Compliant

The emergency locator transmitter is located on the rear fuselage and is attached to the primary structure in such a manner that the probability of damage to the transmitter in the event of crash impact is minimized.

AGREE

91.207(c) Emergency locator transmitters: Batteries.


-

AGREE

91.207(d) Emergency locator transmitters: Inspections.

Compliant

The ELT is inspected within 12 calendar months.

AGREE

91.207(e) Emergency locator transmitters: Ferry flights.


-

AGREE


A-84


91.207(f) Emergency locator transmitters: Exemptions.


-

AGREE

91.209 Aircraft lights. Compliant

EMB-505 is equipped with approved Position and Anticollision lights.

AGREE

91.211 Supplemental oxygen. Title Only

-

AGREE

91.211(a) Supplemental oxygen: General.

Not Applicable

Applicable only to non-pressurized aircraft

AGREE

91.211(b) Supplemental oxygen: Pressurized cabin aircraft.

Compliant

The oxygen system has been sized to provide all occupants (crew and passengers) with emergency oxygen for a 10-minute descent to 10,000 feet, where supplemental oxygen is not required. EMB-505 is pressurized to 8,000 feet equivalent pressure during normal operation and the crew mask is worn and operated in the normal (dilution) setting with the additional dilution valve feature activated. The crew masks are quick donning type that can be placed on the face with one hand from the ready position within 5 seconds, supplying oxygen and properly secured and sealed.

AGREE

91.213 Inoperative instruments and equipment.

Title Only

-

AGREE

91.213(a) Inoperative instruments and equipment: Minimum Equipment List.

Compliant

Embraer will provide all information for the MMEL certification and required maintenance/operations procedures.

AGREE

91.213(b) Inoperative instruments and equipment: Not included in Minimum Equipment List.

Compliant

The MMEL proposed by Embraer comply with the requirements.

AGREE

91.213(c) Inoperative instruments and equipment: Minimum Equipment List issued under subpart K, part 121, 125 or 135.


-

AGREE

91.213(d) Inoperative instruments and equipment: Operations without Minimum Equipment List.


-

AGREE

91.213(e) Inoperative instruments and equipment: Special flight permit.


-

AGREE

91.215 ATC transponder and altitude reporting equipment and use.

Compliant

EMB-505 has a baseline Mode-S transponder, TSO-C112 compliant. A second Mode-S transponder is optional.

AGREE


A-85


91.217 Data correspondence between automatically reported pressure altitude data and the pilot's altitude reference.

Title Only

-

AGREE

91.217(a) Data correspondence between automatically reported pressure altitude data and the pilot's altitude reference: Deactivation of equipment.


Operators shall follow ATC directions.

AGREE

91.217(b) Data correspondence between automatically reported pressure altitude data and the pilot's altitude reference: Tests and calibration.

Compliant

EMB-505 is equipped with a Mode S Transponder that is installed and calibrated to report altitude data within 125 ft of the data being presented to the left-seating pilot and/or being used by the auto-pilot, when the latter is active.

AGREE

91.217(c) Data correspondence between automatically reported pressure altitude data and the pilot's altitude reference: Altimeters and digitizers standards.

Compliant

Altimeters are TSO C106 compliant and have digital communication bus ARINC 429.

AGREE

91.219 Altitude alerting system or device: Turbojet-powered civil airplanes.

Title Only

-

AGREE

91.219(a) Altitude alerting system or device: Turbojet-powered civil airplanes: Operable condition.


-

AGREE

91.219(b) Altitude alerting system or device: Turbojet-powered civil airplanes: Requirements.

Compliant

EMB-505 has "Altitude Capture" and "Altitude Departure" aural messages. Aural system has "Fault" and "Fail" visual message and systems are designed to cover aircraft operational range.

AGREE

91.219(c) Altitude alerting system or device: Turbojet-powered civil airplanes: Procedures establishment and assignment.


-

AGREE

91.219(d) Altitude alerting system or device: Turbojet-powered civil airplanes: Exceptions.


-

AGREE

91.221 Traffic alert and collision avoidance system equipment and use.

Title Only

-

AGREE

91.221(a) Traffic alert and collision avoidance system equipment and use: All airspace: U.S.-registered civil aircraft.


TCAS II system is optional for US-registered EMB-505 aircraft.

AGREE


A-86


91.221(b) Traffic alert and collision avoidance system equipment and use: Traffic alert and collision avoidance system, operation required.


-

AGREE

91.223 Terrain awareness and warning system.

Title Only

-

AGREE

91.223(a) Terrain awareness and warning system: Airplanes manufactured after March 29, 2002.

Compliant

EMB-505 has a baseline Class B Terrain Awareness and Warning System (TAWS) installed.

AGREE

91.223(b) Terrain awareness and warning system: Airplanes manufactured on or before March 29, 2002.

Not Applicable

Aircraft manufactured after March 29,2002

AGREE


Compliant

The AFM will contain appropriate procedures for the use of the terrain awareness and warning system; and proper flight crew reaction in response to the terrain awareness and warning system audio and visual warning.

AGREE

91.223(d) Terrain awareness and warning system: Exceptions.


-

AGREE


Reserved.

AGREE

EMB-505 14CFR91 Compliance Subpart D - Special Flight Operations



Reserved.

AGREE

91.303 Aerobatic flight. Operator’s Responsibility

-

AGREE

91.305 Flight test areas. Operator’s Responsibility

-

AGREE

91.309 Towing: Gliders and unpowered ultralight vehicles.


-

AGREE

91.311 Towing: Other than under §91.309.


-

AGREE

91.313 Restricted category civil aircraft: Operating limitations.


-

AGREE


A-87


91.315 Limited category civil aircraft: Operating limitations.


-

AGREE

91.317 Provisionally certificated civil aircraft: Operating limitations.


-

AGREE

91.319 Aircraft having experimental certificates: Operating limitations.


-

AGREE

91.321 Carriage of candidates in elections.


-

AGREE

91.323 Increased maximum certificated weights for certain airplanes operated in Alaska.

Not Applicable

Applicable only to airplane type certificated under Aeronautics Bulletin No. 7-A of the U.S. Department of Commerce dated January 1, 1931, as amended, or under the normal category of part 4a of the former Civil Air Regulations

AGREE

91.325 Primary category aircraft: Operating limitations.

Not Applicable

Applicable only to primary category aircraft.

AGREE

91.327 Aircraft having a special airworthiness certificate in the light-sport category: Operating limitations.

Not Applicable

Applicable only to aircraft with airworthiness certificate in the light-sport category.

AGREE


Reserved.

AGREE

EMB-505 14CFR91 Compliance Subpart E - Maintenance, Preventive Maintenance, and Alterations



-

AGREE


-

AGREE

91.405 Maintenance required. Operator’s Responsibility

-

AGREE

91.407 Operation after maintenance, preventive maintenance, rebuilding, or alteration.


-

AGREE

91.409 Inspections. Title Only

-

AGREE


A-88


91.409(a) Inspections: Annual Inspection.

Compliant

EMB-505 is delivered with airworthiness certificate released.

AGREE

91.409(b) Inspections: Annual or 100-hour inspection.

Compliant

While the airplane is under Embraer responsibility, it is not operated by any person for hire, and no person give flight instruction for hire.

AGREE

91.409(c) Inspections: Exemptions. Definition

-

AGREE

91.409(d) Inspections: Progressive inspection.

Compliant

Embraer Recommended Scheduled Maintenance Program will be included in the Aircraft Maintenance Manual

AGREE

91.409(e) Inspections: Large airplanes (to which part 125 is not applicable), turbojet multiengine airplanes, turbopropeller-powered multiengine airplanes, and turbine-powered rotorcraft.


-

AGREE

91.409(f) Inspections: Selection of inspection program under paragraph (e) of this section.

Compliant

Embraer will recommend a Scheduled Maintenance Program.

AGREE

91.409(g) Inspections: Inspection program approved under paragraph (e) of this section.


-

AGREE

91.409(h) Inspections: Changes from one inspection program to another.


-

AGREE

91.410 Reserved

Not Applicable

Reserved.

AGREE

91.411 Altimeter system and altitude reporting equipment tests and inspections.

Title Only

-

AGREE

91.411(a) Altimeter system and altitude reporting equipment tests and inspections: Controlled airspace under IFR.

Compliant

For each airplane delivered, the static pressure system, altimeter instrument, and automatic pressure altitude are installed, inspected and tested.

AGREE

91.411(b) Altimeter system and altitude reporting equipment tests and inspections: Tests required by paragraph (a).

Compliant

The manufacturer perform the tests and inspections specified in (b)(1).

AGREE


A-89


91.411(c) Altimeter system and altitude reporting equipment tests and inspections: Altimeter and altitude reporting equipment approved under TSOs.

Compliant

Altimeter and altitude reporting equipment are approved under Technical Standard Orders.

AGREE

91.411(d) Altimeter system and altitude reporting equipment tests and inspections: Controlled airspace under IFR.


-

AGREE

91.413 ATC transponder tests and inspections.

Title Only

-

AGREE

91.413(a) ATC transponder tests and inspections: Compliance with appendix F of part 43.

Compliant

ATC Transponder is tested and inspected within 24 calendar months.

AGREE

91.413(b) ATC transponder tests and inspections: Installation or maintenance.

Compliant

Embraer perform the tests and inspections on the ATC transponder installed.

AGREE

91.413(c) ATC transponder tests and inspections: Tests and inspections.

Compliant

Embraer perform the tests and inspections on the ATC transponder installed.

AGREE

91.415 Changes to aircraft inspection programs.


-

AGREE

91.417 Maintenance records. Compliant

All information of item 2 is recorded on the documentation delivered to the customer with the airplane.

AGREE

91.419 Transfer of maintenance records.

Compliant


AGREE

91.421 Rebuilt engine maintenance records.


-

AGREE


Reserved.

AGREE


A-90

EMB-505 14CFR91 Compliance Subpart F - Large and Turbine-Powered Multiengine Airplanes and Fractional Ownership Program Aircraft


91.501 Applicability. Operator’s Responsibility

-

AGREE

91.503 Flying equipment and operating information.

Title Only

-

AGREE

91.503(a) Flying equipment and operating information: Accessible flying equipment and aeronautical charts and data.

Title Only

-

AGREE

91.503(a)(1) Accessible flying equipment and aeronautical charts and data: Flashlight.

Compliant

A flashlight is provided on the cockpit, installed behind the pilot seat.

AGREE

91.503(a)(2) Accessible flying equipment and aeronautical charts and data: Cockpit checklist.

Compliant

Embraer will prepare and furnish the operation manuals inside each factory delivered airplane.

AGREE

91.503(a)(3) Accessible flying equipment and aeronautical charts and data: Aeronautical charts.


-

AGREE

91.503(a)(4) Accessible flying equipment and aeronautical charts and data: Pertinent chart.


-

AGREE

91.503(a)(5) Accessible flying equipment and aeronautical charts and data: Performance data.

Compliant

Embraer operational publications will furnish the required performance data.

AGREE

91.503(b) Flying equipment and operating information: Cockpit checklist.

Compliant

Embraer will prepare and furnish the operation manuals, with the cockpit checklist included, inside each factory delivered airplane.

AGREE

91.503(c) Flying equipment and operating information: Cockpit checklist procedure.

Compliant

Embraer will prepare and furnish the operational manuals, with the emergency checklist included, inside each factory delivered airplane.

AGREE

91.503(d) Flying equipment and operating information: Equipment, charts and data use.


-

AGREE


A-91


91.505 Familiarity with operating limitations and emergency equipment.


-

AGREE

91.507 Equipment requirements: Over-the-top or night VFR operations.

Not Compliant

EMB-505 is equipped with two landing lights installed in the belly fairing. The aircraft complies with 91.205(d), excepted by item 91.205 (b)(12).

AGREE

91.509 Survival equipment for overwater operations.

Title Only

-

AGREE

91.509(a) Survival equipment for overwater operations: Life preserver or an approved flotation means.


Installation of live vests in case of operation over water is an operator responsibility. Life vest pouches are provided under each seat as provisions for life vest installation.

AGREE

91.509(b) Survival equipment for overwater operations: Survival equipment.

Title Only

-

AGREE

91.509(b)(1) Survival equipment: Life preserver.


Installation of live vests in case of operation over water is an operator responsibility. Life vest pouches are provided under each seat as provisions for life vest installation.

AGREE

91.509(b)(2) Survival equipment: Liferafts.


Installation of live rafts in case of operation over water is an operator responsibility. Space is provided inside the LH Forward Cabinet inside the passenger cabin for the installation of an optional life raft.

AGREE

91.509(b)(3) Survival equipment: Pyrotechnic signaling device.


Pyrotechnic devices are installed within life-rafts. Life rafts are optional item.

AGREE

91.509(b)(4) Survival equipment: Portable emergency radio signaling device.


A Portable ELT integrated to the optional liferaft.

AGREE

91.509(b)(5) Survival equipment: Lifeline.

Not Applicable

Applicable only for aircraft where certification for ditching under §25.801 is requested.

AGREE

91.509(c) Survival equipment for overwater operations: Deviation from paragraphs (b)(2) through (5).


-

AGREE

91.509(d) Survival equipment for overwater operations: Conspicuously marked and easily accessible.


Provisions for the installation of the items described on this paragraph are located on easily accessible places. Markings will be provided with the optional equipment.

AGREE


A-92


91.509(e) Survival equipment for overwater operations: Survival kit.


A survival kit according to Part 135 will be attached at the optional life raft.

AGREE

91.509(f) Survival equipment for overwater operations: Shore.

Definition

-

AGREE

91.511 Communication and navigation equipment for overwater operations.

Title Only

-

AGREE

91.511(a) Communication and navigation equipment for overwater operations: Operable equipment for a flight over water.

Title Only

-

AGREE

91.511(a)(1) Operable equipment for a flight over water: Radio communication equipment.

Compliant

EMB-505 has two radio communication systems installed.

AGREE

91.511(a)(2) Operable equipment for a flight over water: Electronic navigational equipment.

Compliant

EMB-505 has two integrated units containing the navigation (including VOR/LOC/GS and GPS) and communication (VHF) receivers.

AGREE

91.511(b) Communication and navigation equipment for overwater operations: Independent receiver or electronic navigation unit.

Definition

-

AGREE

91.511(c) Communication and navigation equipment for overwater operations: Malfunction or inoperative.


-

AGREE

91.511(d) Communication and navigation equipment for overwater operations: VHF and HF communications equipment.


-

AGREE

91.511(e) Communication and navigation equipment for overwater operations: Shore.

Definition

-

AGREE

91.511(f) Communication and navigation equipment for overwater operations: Gulf of Mexico, Caribbean Sea and Atlantic Ocean operation.


-

AGREE


A-93


91.513 Emergency equipment. Title Only

-

AGREE

91.513(a) Emergency equipment: Listed emergency equipment.


-

AGREE

91.513(b) Emergency equipment: Equipment requirements.

Title Only

-

AGREE

91.513(b)(1) Equipment requirements: Inspection.


-

AGREE

91.513(b)(2) Equipment requirements: Accessibility.

Compliant

Each required item of equipment is readily accessible to the flight crew.

AGREE

91.513(b)(3) Equipment requirements: Method of operation.

Compliant

All equipment is plainly marked as to its method of operation, by means of an inscription on the equipment itself.

AGREE

91.513(b)(4) Equipment requirements: Compartment or container.

Compliant

All compartments which have emergency equipment installed on its interior are marked for its content identification. The date of last inspection is informed on the documentation delivered with the airplane.

AGREE

91.513(c) Emergency equipment: Hand fire extinguishers.

Compliant

There is one hand fire extinguisher on the cockpit, behind the copilot seat, and one in the passenger cabin, at the floor level, between the last row of seats and the lavatory partition. Both are filled with Halon 1211/1301 blend rated for classes B and C types of fire.

AGREE

91.513(d) Emergency equipment: First Aid kits.

Compliant

A first aid kit is provided inside the passenger cabin.

AGREE

91.513(e) Emergency equipment: Crash axe.

Not Applicable

Applicable only to aircraft with a capacity for more than 19 passengers.

AGREE

91.513(f) Emergency equipment: Megaphone.

Not Applicable

Applicable only to airplanes with a seating capacity of more than 60.

AGREE

91.515 Flight altitude rules. Operator’s Responsibility

-

AGREE

91.517 Passenger information. Title Only

-

AGREE

91.517(a) Passenger information: Visible signs.

Compliant

No smoke and fasten seat belts ordinance signs are installed.

AGREE

91.517(b) Passenger information: Oral notification.


-

AGREE


A-94


91.517(c) Passenger information: Smoking prohibition.


-

AGREE

91.517(d) Passenger information: "Fasten seat belt" sign.


-

AGREE

91.517(e) Passenger information: Given instructions.


-

AGREE

91.519 Passenger briefing. Title Only

-

AGREE

91.519(a) Passenger briefing: Oral briefing.


-

AGREE

91.519(b) Passenger briefing: Printed cards.

Title Only

-

AGREE

91.519(b)(1) Printed cards: Emergency exits.

Compliant

Briefing cards containing the method of operation of the emergency exits are provided for all passengers.

AGREE

91.519(b)(2) Printed cards: Emergency equipment.

Compliant

For all equipment installed by Embraer: a)instructions are provided on the equipment itself describing its operation, or b)there is a placard near the equipment installing position describing its operation, or c) Instructions are provided on the briefing card.

AGREE

91.519(c) Passenger briefing: Locations.

Compliant

Briefing cards are related only to the specific characteristics of the EMB-505. Briefing cards are installed on the magazine holders, adjacent to each passenger seat.

AGREE

91.519(d) Passenger briefing: Subpart K.


-

AGREE

91.521 Shoulder harness. Not Applicable

Applicable only to transport category airplane.

AGREE

91.523 Carry-on baggage. Not Applicable

Applicable only for aircraft with a seating capacity for more than 19 passengers.

AGREE

91.525 Carriage of cargo. Title Only

-

AGREE

91.525(a) Carriage of cargo: Requirements.


Approved baggage compartments are provided inside the aircraft. Activities related to pilot permission for use of these compartments are operator's responsibility.

AGREE

91.525(b) Carriage of cargo: Cargo compartments that requires physical entry.


-

AGREE


A-95


91.527 Operating in icing conditions.

Title Only

-

AGREE

91.527(a) Operating in icing conditions: Requirements.


-

AGREE

91.527(b) Operating in icing conditions: Flight under icing conditions.

Compliant

EMB-505 has ice protection provisions that comply with the requirements in section 34 of SFAR No. 23.

AGREE

91.527(c) Operating in icing conditions: Severe icing conditions.

Compliant

EMB-505 has ice protection provisions that comply with the requirements in section 34 of SFAR No. 23.

AGREE

91.527(d) Operating in icing conditions: Forecast icing conditions.


-

AGREE

91.529 Flight engineer requirements.

Not Applicable

Applicable only for aircraft type certificated with a flight engineer.

AGREE

91.531 Second in command requirements.


-

AGREE

91.533 Flight attendant requirements.

Not Applicable

Applicable only to aircraft with more than 19 passengers on board.

AGREE



-

AGREE


Reserved.

AGREE

EMB-505 14CFR91 Compliance Subpart G - Additional Equipment and Operating Requirements for Large and Transport Category Aircraft



Applicable only to Large and Transport Category Aircraft.

AGREE

91.603 Aural speed warning device.

Not Applicable


AGREE

91.605 Transport category civil airplane weight limitations.

Not Applicable


AGREE

91.607 Emergency exits for airplanes carrying

Not Applicable

Applicable only to large aircraft type certificated under the Civil Air Regulations

AGREE


A-96


passengers for hire. effective before April 9, 1957.

91.609 Flight recorders and cockpit voice recorders.

Title Only

-

AGREE

91.609(a) Flight recorders and cockpit voice recorders: Authorized flights without equipment installed or inoperative.


-

AGREE

91.609(b) Flight recorders and cockpit voice recorders: Authorized flights without equipment installed or inoperative.


-

AGREE

91.609(c) Flight recorders and cockpit voice recorders: Flight recorder features.

Not Applicable

Applicable only to aircraft having a passenger seating configuration, excluding any pilot seats, of 10 or more

AGREE

91.609(d) Flight recorders and cockpit voice recorders: Flight recorder operation.

Not Applicable

Applicability related to item 91.609(c)

AGREE

91.609(e) Flight recorders and cockpit voice recorders: CVR features and operation.

Compliant

EMB-505 has a baseline CVDR installed compliant with 14 CFR 23.1457 (a)(1) and (2),(b),(c),(d),(e),(f),and (g), that operates continuously from the use of checklist before flight to completion of the final checklist at the end of flight.

AGREE

91.609(f) Flight recorders and cockpit voice recorders: CVR erasing features.

Compliant

Installed CVR is not erasable in flight conditions.

AGREE

91.609(g) Flight recorders and cockpit voice recorders: Flight recorders and CVR recorded information.


-

AGREE

91.609(h) Flight recorders and cockpit voice recorders: CVR requirements.

Compliant

EMB-505 has a baseline CVDR and an optional FDR that comply with 14 CFR 23.1457(d)(6).

AGREE

91.609(i) Flight recorders and cockpit voice recorders: CVR requirements.

Compliant

EMB-505 has a CVDR installed, compliant with 23.1457, that retains 2 hours of recorded audio. The CVDR is also TSO C-124b compliant.

AGREE

91.609(j) Flight recorders and cockpit voice recorders: Datalink communication.

Not Applicable

EMB-505 does not have datalink communication equipment installed.

AGREE

91.611 Authorization for ferry flight with one engine inoperative.

Not Applicable

Applicable only to aircraft with three or four engines.

AGREE


A-97


91.613 Materials for compartment interiors.

Not Applicable

Applicable only to Large Aircraft.

AGREE


Reserved.

AGREE

EMB-505 14CFR91 Compliance Subpart H - Foreign Aircraft Operations and Operations of U.S.-Registered Civil Aircraft Outside of the United States; and

Rules Governing Persons on Board Such Aircraft



-

AGREE

91.702 Persons on board. Definition

-

AGREE

91.703 Operations of civil aircraft of U.S. registry outside of the United States.


-

AGREE

91.705 Operations within airspace designated as Minimum Navigation Performance Specification Airspace.


-

AGREE

91.706 Operations within airspace designed as Reduced Vertical Separation Minimum Airspace.


-

AGREE

91.707 Flights between Mexico or Canada and the United States.


-

AGREE

91.709 Operations to Cuba. Operator’s Responsibility

-

AGREE

91.711 Special rules for foreign civil aircraft.

Not Applicable

Applicable only to aircraft not registered in USA

AGREE

91.713 Operation of civil aircraft of Cuban registry.

Not Applicable

Applicable only to Cuban registered aircraft.

AGREE

91.715 Special flight authorizations for foreign civil aircraft.

Not Applicable

Applicable only to aircraft not registered in USA.

AGREE


Reserved.

AGREE


A-98

EMB-505 14CFR91 Compliance

Subpart I - Operating Noise Limits


91.801 Applicability: Relation to part 36.

Definition

-

AGREE

91.803 Part 125 operators: Designation of applicable regulations.

Not Applicable

Applicable only to Part 125 eligible aircraft.

AGREE

91.805 Final compliance: Subsonic airplanes.

Not Applicable


AGREE


Reserved.

AGREE

91.815 Agricultural and fire fighting airplanes: Noise operating limitations.

Not Applicable

Applicable only to propeller-driven, small airplanes having standard airworthiness certificates that are designed for "agricultural aircraft operations" or for dispensing fire fighting materials.

AGREE

91.817 Civil aircraft sonic boom. Not Applicable


AGREE

91.819 Civil supersonic airplanes that do not comply with part 36.

Not Applicable


AGREE

91.821 Civil supersonic airplanes: Noise limits.

Not Applicable


AGREE


Reserved.

AGREE

91.851 Definitions. Definition

-

AGREE

91.853 Final compliance: Civil subsonic airplanes.

Not Applicable


AGREE

91.855 Entry and non addition rule.

Not Applicable


AGREE

91.857 Stage 2 operations outside of the 48 contiguous United States.


-

AGREE

91.858 Special flight authorizations for non-revenue Stage 2 operations.

Not Applicable


AGREE

91.859 Modification to meet Stage 3 or Stage 4 noise levels.

Not Applicable


AGREE


A-99


91.861 Base level. Operator’s Responsibility

-

AGREE

91.863 Transfers of Stage 2 airplanes with base level.


-

AGREE

91.865 Phased compliance for operators with base level.


-

AGREE

91.867 Phased compliance for new entrants.


-

AGREE

91.869 Carry-forward compliance.


-

AGREE

91.871 Waivers from interim compliance requirements.


-

AGREE

91.873 Waivers from final compliance.


-

AGREE

91.875 Annual progress reports. Operator’s Responsibility

-

AGREE

91.877 Annual reporting of Hawaiian operations.


-

AGREE


Reserved.

AGREE

EMB-505 14CFR91 Compliance Subpart J - Waivers



Reserved.

AGREE

91.903 Policy and procedures. Operator’s Responsibility

-

AGREE

91.905 List of rules subject to waivers.


-

AGREE


Reserved.

AGREE


A-100

EMB-505 14CFR91 Compliance Subpart K - Fractional Ownership Operations



-

AGREE

91.1002 Compliance date. Operator’s Responsibility

-

AGREE

91.1003 Management contract between owner and program manager.


-

AGREE

91.1005 Prohibitions and limitations.


-

AGREE

91.1007 Flights conducted under part 121 or part 135 of this chapter.


-

AGREE

91.1009 Clarification of operational control.


-

AGREE

91.1011 Operational control responsibilities and delegation.


-

AGREE

91.1013 Operational control briefing and acknowledgment.


-

AGREE

91.1014 Issuing or denying management specifications.

Definition

-

AGREE

91.1015 Management specifications.


-

AGREE

91.1017 Amending program manager's management specifications.


-

AGREE

91.1019 Conducting tests and inspections.

Definition

-

AGREE

91.1021 Internal safety reporting and incident/accident response.


-

AGREE

91.1023 Program operating manual requirements.


-

AGREE

91.1025 Program operating manual contents.


-

AGREE

91.1027 Recordkeeping. Operator’s Responsibility

-

AGREE

91.1029 Flight scheduling and locating requirements.


-

AGREE


A-101




-

AGREE

91.1033 Operating information required.

Title Only

-

AGREE

91.1033(a) Operating information required: Materials.

Title Only

-

AGREE

91.1033(a)(1) Materials: Cockpit checklist.

Compliant


AGREE

91.1033(a)(2) Materials: Emergency cockpit checklist.

Compliant


AGREE

91.1033(a)(3) Materials: Aeronautical charts.


-

AGREE

91.1033(a)(4) Materials: Pertinent charts.


-

AGREE

91.1033(b) Operating information required: Cockpit checklist.

Compliant

Embraer will prepare and furnish the operational manuals, with the cockpit checklist included, inside each factory delivered airplane.

AGREE

91.1033(c) Operating information required: Emergency cockpit checklist.

Compliant

Embraer will prepare and furnish the operational manuals, with the emergency checklist included, inside each factory delivered airplane.

AGREE

91.1035 Passenger awareness. Title Only

-

AGREE

91.1035(a) Passenger awareness: Oral Briefing.


-

AGREE

91.1035(b) Passenger awareness: Evacuation procedures briefing.


-

AGREE

91.1035(c) Passenger awareness: Operational control briefing.


-

AGREE

91.1035(d) Passenger awareness: Oral briefings.


-

AGREE

91.1035(e) Passenger awareness: Recording playback device.


The use of a recording playback device to deliver the oral briefing to passengers is operator's responsibility.

AGREE

91.1035(f) Passenger awareness: Compliant Briefing cards are provided for each AGREE


A-102


Printed Cards.

passenger, containing information for the specific EMB-505 characteristics and including indication of emergency exit operation and any complementary instruction for emergency equipments installed by the aircraft manufacturer.

91.1037 Large transport category airplanes: Turbine engine powered; Limitations; Destination and alternate airports.

Not Applicable


AGREE

91.1039 IFR takeoff, approach and landing minimums.


-

AGREE

91.1041 Aircraft proving and validation tests.


-

AGREE


Reserved.

AGREE

91.1045 Additional equipment requirements.

Title Only

-

AGREE

91.1045(a) Additional equipment requirements.

Not Applicable

Applicable only to aircraft with a passenger-seat configuration of more than 30 seats or a payload capacity of more than 7,500 pounds.

AGREE

91.1045(b) Additional equipment requirements.

Title Only

-

AGREE

91.1045(b)(1) Additional equipment requirements: Cockpit voice recorder.

Compliant

The aircraft has an CVR compliant with 14 CFR 23.1457 (a)(b)(c)(d)(e)(f)(g), that operates continuously from the use of checklist before flight to completion of the final checklist at the end of flight.

AGREE

91.1045(b)(2) Additional equipment requirements: Flight recorder.

Not Applicable

Applicable only to multi-engine, turbine-engine powered airplane or rotorcraft having a passenger seating configuration, excluding any required crewmember seat, of 10 to 19 seats.

AGREE

91.1045(b)(3) Additional equipment requirements: Terrain awareness and warning system.

Compliant

EMB-505 has TAWS that meets the TSO-C151b requirements for Class B equipment.

AGREE

91.1045(b)(4) Additional equipment requirements: Traffic alert and collision avoidance system.

Not Applicable


AGREE

91.1045(b)(5) Additional equipment requirements: Airborne weather radar or

Not Applicable

Applicable only to aircraft with a passenger seating configuration, excluding any pilot seat, of 10 seats or more.

AGREE


A-103


thunderstorm detection equipment.

91.1047 Drug and alcohol misuse education program.


-

AGREE

91.1049 Personnel. Operator’s Responsibility

-

AGREE

91.1051 Pilot safety background check.


-

AGREE

91.1053 Crewmember experience. Operator’s Responsibility

-

AGREE

91.1055 Pilot operating limitations and pairing requirement.


-

AGREE

91.1057 Flight, duty and rest time requirements: All crewmembers.


-

AGREE

91.1059 Flight time limitations and rest requirements: One or two pilot crews.


-

AGREE

91.1061 Augmented flight crews. Operator’s Responsibility

-

AGREE

91.1062 Duty periods and rest requirements: Flight attendants.


-

AGREE

91.1063 Testing and training: Applicability and terms used.

Definition

-

AGREE

91.1065 Initial and recurrent pilot testing requirements.


-

AGREE



-

AGREE

91.1069 Flight crew: Instrument proficiency check requirements.


-

AGREE


Definition

-

AGREE

91.1073 Training program: General.


-

AGREE

91.1075 Training program: Special rules.

Definition

-

AGREE

91.1077 Training program and Operator’s Responsibility - AGREE


A-104


revision: Initial and final approval.

91.1079 Training program: Curriculum.


-

AGREE

91.1081 Crewmember training requirements.


-

AGREE

91.1083 Crewmember emergency training.


-

AGREE

91.1085 Hazardous materials recognition training.


-

AGREE


Definition

-

AGREE

91.1089 Qualifications: Check pilots (aircraft) and check pilots (simulator).


-

AGREE



-

AGREE

91.1093 Initial and transition training and checking: Check pilots (aircraft), check pilots (simulator).


-

AGREE



-

AGREE



-

AGREE



-

AGREE

91.1101 Pilots: Initial, transition, and upgrade ground training.


-

AGREE

91.1103 Pilots: Initial, transition, upgrade, requalification, and differences flight training.


-

AGREE

91.1105 Flight attendants: Initial and transition ground training.


-

AGREE


A-105



-

AGREE

91.1109 Aircraft maintenance: Inspection program.

Title Only

-

AGREE

91.1109(a) Aircraft maintenance: Inspection program.

Title Only

-

AGREE

91.1109(a)(1) Aircraft maintenance: Inspection program: Instructions and procedures.

Compliant

The information will be issued in the Aircraft Maintenance Manual.

AGREE

91.1109(a)(2) Aircraft maintenance: Inspection program: Schedule.

Compliant

The recommended Scheduled Maintenance Program complies with this requirement.

AGREE

91.1109(a)(3) Aircraft maintenance: Inspection program: Person responsible for scheduling.


-

AGREE

91.1109(b) Aircraft maintenance: Inspection program.

Compliant

Embraer Recommended Scheduled Maintenance Program will be included in the Aircraft Maintenance Manual, and the engine manufacturer will issue a Scheduled Maintenance Program too.

AGREE

91.1109(c) Aircraft maintenance: Inspection program: Revision.

Definition

-

AGREE

91.1111 Maintenance training. Operator’s Responsibility

-

AGREE

91.1113 Maintenance recordkeeping.


-

AGREE

91.1115 Inoperable instruments and equipment.

Title Only

-

AGREE

91.1115(a) Inoperable instruments and equipment.

Title Only

-

AGREE

91.1115(a)(1) Inoperable instruments and equipment: Minimum Equipment List.

Compliant

Embraer will provide all information for the MMEL certification and required maintenance/operations procedures

AGREE

91.1115(a)(2) Inoperable instruments and equipment: Management specifications.


-

AGREE

91.1115(a)(3) Inoperable instruments and equipment: Minimum Equipment List.

Compliant


AGREE


A-106


91.1115(a)(4) Inoperable instruments and equipment: Records.


-

AGREE

91.1115(a)(5) Inoperable instruments and equipment: Operations.


-

AGREE

91.1115(b) Inoperable instruments and equipment: Minimum Equipment List limitations.

Compliant


AGREE

91.1115(c) Inoperable instruments and equipment: Special flight permit.


-

AGREE

91.1115(d) Inoperable instruments and equipment: Use of Minimum Equipment List.

Definition

-

AGREE

91.1411 Continuous airworthiness maintenance program use by fractional ownership program manager.

Compliant

Embraer Recommended Scheduled Maintenance Program will be included in the Aircraft Maintenance Manual

AGREE

91.1413 CAMP: Responsibility for airworthiness.


-

AGREE

91.1415 CAMP: Mechanical reliability reports.


-

AGREE

91.1417 CAMP: Mechanical interruption summary report.


-

AGREE

91.1423 CAMP: Maintenance organization.


-

AGREE

91.1425 CAMP: Maintenance, preventive maintenance, and alteration programs.


-

AGREE

91.1427 CAMP: Manual requirements.


-

AGREE

91.1429 CAMP: Required inspection personnel.


-

AGREE

91.1431 CAMP: Continuing analysis and surveillance.


-

AGREE

91.1433 CAMP: Maintenance and preventive maintenance training program.


-

AGREE

91.1435 CAMP: Certificate requirements.


-

AGREE


A-107


91.1437 CAMP: Authority to perform and approve maintenance.


-

AGREE

91.1439 CAMP: Maintenance recording requirements.


-

AGREE

91.1441 CAMP: Transfer of maintenance records.


-

AGREE

91.1443 CAMP: Airworthiness release or aircraft maintenance log entry.


-

AGREE

EMB-505 14CFR91 Compliance Subpart L - Continued Airworthiness and Safety Improvements


91.1501 Purpose and definition. Definition

-

AGREE


Reserved.

AGREE

91.1505 Repairs assessment for pressurized fuselages.

Not Applicable

Applicable only for Airbus Model A300 (excluding the -600 series), British Aerospace Model BAC 1-11, Boeing Model, 707, 720, 727, 737 or 747, McDonnell Douglas Model DC-8, DC-9/MD-80 or DC-10, Fokker Model F28, or Lockheed Model L-1011 airplane.

AGREE

91.1507 Fuel tank system inspection program.

Not Applicable

Applicable only for transport category, turbine-powered airplanes with a maximum type-certificated passenger capacity of 30 or more, or maximum payload capacity of 7,500 pounds or more.

AGREE

EMB-505 14CFR91 Compliance Appendix B to Part 91 - Authorizations to Exceed Mach 1 (§91.817)


Appendix B Authorizations To Exceed Mach 1 (§91.817)

Not Applicable

Aircraft certified maximum speed do not exceed Mach 1

AGREE


A-108

EMB-505 14CFR91 Compliance Appendix C to Part 91 - Operations in the North Atlantic (NAT) Minimum Navigation Performance Specifications (MNPS)

Airspace


Appendix C Operations in the North Atlantic (NAT) Minimum Navigation Performance Specifications (MNPS) Airspace

Compliant

The aircraft has approved navigation performance capability that complies with the North Atlantic (NAT) Minimum Navigational Performance Specifications (MNPS) Airspace requirements.

AGREE

EMB-505 14CFR91 Compliance Appendix D to Part 91 - Airports/Locations: Special Operating Restrictions


Appendix D Airports/Locations: Special Operating Restrictions


-

AGREE

EMB-505 14CFR91 Compliance Appendix E to Part 91 - Airplane Flight Recorder Specifications


Appendix E Airplane Flight Recorder Specifications

Not Applicable

FDR is not required for EMB-505

AGREE

EMB-505 14CFR91 Compliance Appendix G to Part 91 - Operations in Reduced Vertical Separation Minimum (RVSM) Airspace


Appendix G Operations in Reduced Vertical Separation Minimum (RVSM) Airspace

Title Only

-

AGREE

Appendix G.1 Operations in Reduced Vertical Separation Minimum (RVSM) Airspace: Definitions.

Definition

-

AGREE

Appendix G.2(a)

Aircraft Approval: Authorization.


-

AGREE

Appendix G.2(b)

Aircraft Approval: Data package.


-

AGREE


A-109

EMB-505 14CFR135 Compliance Subpart A- General



-

AGREE

135.2 Compliance schedule for operators that transition to part 121 of this chapter; certain new entrant operators.

Not Applicable

Applicability does not include aircraft with the characteristics of the EMB-505.

AGREE

135.3 Rules applicable to operations subject to this part.


-

AGREE

135.4 Applicability of rules for eligible on-demand operations.


-

AGREE

135.7 Applicability of rules to unauthorized operators.

Definition

-

AGREE

135.12 Previously trained crewmembers.


-

AGREE

135.19 Emergency operations. Operator’s Responsibility

-

AGREE


-

AGREE

135.23 Manual contents. Operator’s Responsibility

-

AGREE

135.25 Aircraft requirements. Operator’s Responsibility

-

AGREE



-

AGREE

135.43 Crewmember certificates: International operations.


-

AGREE

EMB-505 14CFR135 Compliance

Subpart B - Flight Operations


135.61 General. Definition

-

AGREE

135.63 Recordkeeping Operator’s Responsibility - AGREE


A-110


requirements.

135.64 Retention of contracts and amendments: Commercial operators who conduct intrastate operations for compensation or hire.


-

AGREE

135.65 Reporting mechanical irregularities.


-

AGREE

135.67 Reporting potentially hazardous meteorological conditions and irregularities of ground facilities or navigation aids.


-

AGREE

135.69 Restriction or suspension of operations: Continuation of flight in an emergency.


-

AGREE

135.71 Airworthiness check. Operator’s Responsibility

-

AGREE

135.73 Inspections and tests. Operator’s Responsibility

-

AGREE

135.75 Inspectors credentials: admission to pilots' compartment: Forward observer's seat.

Definition

-

AGREE

135.75(a) Inspectors credentials: Admission to pilots' compartment: Forward observer's seat.


-

AGREE

135.75(b) Inspectors credentials: Admission to pilots' compartment: Forward observer's seat.

Compliant

The left-hand side, aft-facing passenger seat installed on the first row will be used as the observer seat under the situation discussed on this paragraph. The oxygen system normally provided for the passengers, installed on the ceiling panel, will be available the FAA inspector use. A headset is available on the observer seat, allowing communication with the flight crew. It is also possible to hear the ATC communication.

AGREE

135.76 DOD Commercial Air Carrier Evaluator's Credentials: Admission to pilots compartment: Forward observer's seat.

Title Only

-

AGREE

135.76(a) DOD Commercial Air Carrier Evaluator's Credentials: Admission to pilots compartment:


-

AGREE


A-111


Forward observer's seat.

135.76(b) DOD Commercial Air Carrier Evaluator's Credentials: Admission to pilots compartment: Forward observer's seat.

Compliant

The left-hand side, aft-facing passenger seat installed on the first row will be used as the observer seat under the situation discussed on the Statement of Issue section. The oxygen system normally provided for the passengers, installed on the ceiling panel, will be available the FAA inspector use. A headset is available on the observer seat, allowing communication with the flight crew. It is also possible to hear the ATC communication.

AGREE

135.77 Responsibility for operational control.


-

AGREE

135.78 Instrument approach procedures and IFR landing minimums.


-

AGREE

135.79 Flight locating requirements.


-

AGREE

135.81 Informing personnel of operational information and appropriate changes.


-

AGREE

135.83 Operating information required.

Title Only

-

AGREE

135.83(a) Operating information required.

Title Only

-

AGREE

135.83(a)(1) Operating information required: checklist

Compliant

Embraer will furnish a set of operation manuals, with a cockpit checklist included, in each factory delivered airplane.

AGREE

135.83(a)(2) Operating information required: emergency checklist

Compliant

Embraer will furnish a set of operation manuals, with the checklist included, in each factory delivered airplane.

AGREE

135.83(a)(3) Operating information required: Aeronautical Charts


-

AGREE

135.83(a)(4) Operating information required: navigational en route, terminal area, and approach and letdown chart


-

AGREE

135.83(a)(5) Operating information required: one-engine-inoperative climb performance data

Compliant

Embraer will furnish a set of operational manuals, with the required performance data, inside each airplane factory delivered.

AGREE

135.83(b) Operating information required: cockpit

Compliant

Embraer will furnish a set of operation manuals, with the checklist included, in each

AGREE


A-112


checklist contents factory delivered airplane.

135.83(c) Operating information required: cockpit checklist contents

Compliant

Embraer will furnish a set of operation manuals, with the checklist included, in each factory delivered airplane.

AGREE

135.85 Carriage of persons without compliance with the passenger-carrying provisions of this part.


-

AGREE

135.87 Carriage of cargo including carry-on baggage.

Compliant

The fwd and aft cargo compartments and stowage compartments inside the passenger cabin are provided for cargo carriage. For the compartments that also provide storage area for emergency equipment, like the lavatory cabinet, these equipments are located in such a way that baggage installation does not obstruct access in an emergency situation, nor obstruct access to the aisle between the crew and passenger compartments or obscures passenger view of a the required signs.

AGREE

135.89 Pilot requirements: Use of oxygen.

Compliant

EMB-505 is pressurized up to 6,700 feet equivalent pressure. In the event of a decompression, emergency oxygen is provided to all occupants. Two hours for each pilot and 30 minutes for each passenger for the descent to 10,000 feet in less than 30 minutes. The crew oxygen mask used in the EMB-505 oxygen system is a quick donning (within 5 seconds) mask assembly, stowed in a box mounted next to the seat. The mask is continuously pressurized to provide ready access to emergency oxygen.

AGREE

135.91 Oxygen for medical use by passengers.


-

AGREE

135.93 Autopilot: Minimum altitudes for use.

Compliant

The AFM specifies the minimum altitude for autopilot engagement.

AGREE

135.95 Airmen: Limitations on use of services.


-

AGREE

135.97 Aircraft and facilities for recent flight experience.


-

AGREE

135.99 Composition of flight crew.

Title Only

-

AGREE

135.99(a) Composition of flight crew: Aircraft operating limitations or AFM.

Compliant

Embraer issues and furnishes the operational manuals, with the required minimum crew limitation, inside each airplane factory delivered.

AGREE


A-113


135.99(b) Composition of flight crew: Second in command.

Not Applicable

Applicable only to aircraft with ten passenger seats or more.

AGREE

135.100 Flight crewmember duties.


-

AGREE

135.101 Second in command required under IFR.


-

AGREE


Reserved.

AGREE

135.105 Exception to second in command requirement: Approval for use of autopilot system.

Compliant

An autopilot system is available and approved in TC. MMEL defines the dispatchability restrictions.

AGREE

135.107 Flight attendant crewmember requirement.

Not Applicable

Applicable only to aircraft with passenger seating configuration of 19 or more.

AGREE



-

AGREE

135.111 Second in command required in category II operations.

Not Applicable

Aircraft not certified for CAT II operations.

AGREE

135.113 Passenger occupancy of pilot seat.

Not Applicable

Applicable only to aircraft with passenger seating configuration of more than eight seats.

AGREE

135.115 Manipulation of controls. Operator’s Responsibility

-

AGREE

135.117 Briefing of passengers before flight.

Title Only

-

AGREE

135.117(a) Briefing of passengers before flight: Oral briefing.


-

AGREE

135.117(b) Briefing of passengers before flight: Assistance to move to an exit.


-

AGREE

135.117(c) Briefing of passengers before flight: Oral briefing.


-

AGREE

135.117(d) Briefing of passengers before flight: Oral briefing.


-

AGREE

135.117(e) Briefing of passengers before flight: Printed Cards.

Compliant

Briefing cards are provided for each passenger, containing information for the specific EMB-505 characteristics, including indication of emergency exit operation and any instruction for emergency equipments

AGREE


A-114


installed by the aircraft manufacturer and whose operation is not clearly indicated on the equipment itself or any placard adjacent to the equipment installation position.

135.117(f) Briefing of passengers before flight: Recording playback device.


The use of a recording playback device to deliver the oral briefing to passengers is under operator's responsibility.

AGREE

135.119 Prohibition against carriage of weapons.


-

AGREE

135.120 Prohibition on interference with crewmembers


-

AGREE

135.121 Alcoholic beverages. Operator’s Responsibility

-

AGREE



-

AGREE

135.123 Emergency and emergency evacuation duties.


-

AGREE

135.125 Airplane security. Operator’s Responsibility

-

AGREE

135.127 Passenger information requirements and smoking prohibitions.

Compliant

The "No Smoking" ordinance signs are provided inside the cabin.

AGREE

135.128 Use of safety belts and child restraint systems.

Compliant

Pilot and co-pilot seats are provided with 5-points restraint system, and passenger seats inside the cabin area are provided with 3-points restraint system. Child restraint system is operator’s responsibility.

AGREE

135.129 Exit seating. Not Applicable

Not applicable for on-demand operations with aircraft having 19 or fewer passenger seats and commuter operations with aircraft having 9 or fewer passenger seats

AGREE

EMB-505 14CFR135 Compliance Subpart C - Aircraft and Equipment



-

AGREE


A-115


135.143 General requirements. Title Only

-

AGREE

135.143(a) General requirements: Applicable regulations.


-

AGREE

135.143(b) General requirements: Approval and operable condition.


-

AGREE

135.143(c) General requirements: ATC transponder equipment.

Compliant

EMB-505 transponder is TSO-C112 (Mode S)

AGREE

135.144 Portable electronic devices.


-

AGREE

135.145 Aircraft proving and validation tests.


-

AGREE

135.147 Dual controls required. Compliant

Dual functional controls are available and approved in TC.

AGREE

135.149 Equipment requirements: General.

Title Only

-

AGREE

135.149(a) Equipment requirements: General: Sensitive altimeter.

Compliant

Comply according to 23.1303 (b),(g)(2). Each altimeter is barometric adjustable.

AGREE

135.149(b) Equipment requirements: General: Heating or deicing equipment for each carburetor.

Not Applicable

Applicable only to aircraft with reciprocating engines.

AGREE

135.149(c) Equipment requirements: General: Gyroscopic bank-and-pitch indicators.

Compliant

EMB-505 is equipped with a third attitude instrument, see details on 91.205(d)(3).

AGREE

135.149(d) Equipment requirements: General: Reserved.

Not Applicable

Reserved

AGREE

135.149(e) Equipment requirements: Any other equipment.


Unknown requirements

AGREE

135.150 Public address and crewmember interphone systems.

Not Applicable

Applicable only to aircraft with passenger seating configuration, excluding any pilot seat, of more than 19

AGREE

135.151 Cockpit voice recorders. Title Only

-

AGREE

135.151(a) Cockpit voice recorders: Installation Requirements.

Compliant

EMB-505 has a baseline CVDR installed compliant with 23.1457 (a)(1) and (2),(b),(c),(d),(e),(f),and (g), that operates continuously from the use of checklist before flight to completion of the final checklist at the end of flight.

AGREE


A-116


135.151(b) Cockpit voice recorders: Installation Requirements.

Not Applicable

Applicable only to multiengine, turbine-powered airplane having a passenger seating configuration of 20 or more seats

AGREE

135.151(c) Cockpit voice recorders: Accident Reporting Requirements.


-

AGREE

135.151(d) Cockpit voice recorders: Boom and Mask Microphone.

Compliant

Comply according to 23.1457 (a),(b),(c)

AGREE

135.151(e) Cockpit voice recorders: Recorded Data.

Compliant

Comply according to CVR manufacturer technical data.

AGREE

135.151(f) Cockpit voice recorders: If Flight Data Recorder is required.

Compliant

EMB-505 has a CVDR that complies with 23.1457(d)(6).

AGREE

135.151(g)(1) Cockpit voice recorders: If Flight Data Recorder is required.

Compliant

EMB-505 has a baseline CVDR installed, compliant with 23.1457, that operates continuously from the use of checklist before flight to completion of the final checklist at the end of flight. It retains 2 hours of recorded audio, 25 hours of data information and is TSO C-124b compliant.

AGREE

135.151(g)(2) Cockpit voice recorders: If Flight Data Recorder is required (for 20 pax or more).

Not Applicable

Applicable only for aircraft with passenger configuration of 20 or more.

AGREE

135.151(h) Cockpit voice recorders: Datalink communication equipment.

Not Applicable

EMB-505 does not have datalink communication equipment installed.

AGREE

135.152 Flight data recorders. Not Applicable

Applicable only to multi-engine, turbine-engine powered airplane or rotorcraft having a passenger seating configuration, excluding any required crewmember seat, of 10 or more seats.

AGREE

135.153 Ground proximity warning system.

Not Applicable

Applicable only to turbine-powered airplane having a passenger seat configuration of 10 seats or more.

AGREE

135.154 Terrain awareness and warning system.

Title Only

-

AGREE

135.154(a) Terrain awareness and warning system: Airplanes manufactured after March 29, 2002.

Title Only

-

AGREE

135.154(a)(1) Airplanes manufactured after March 29, 2002: Requirements for Class A equipment.

Not Applicable

Applicable only to turbine-powered airplane configured with 10 or more passenger seats.

AGREE


A-117


135.154(a)(2) Airplanes manufactured after March 29, 2002: Requirements for Class B equipment.

Compliant

EMB-505 has a baseline Class B TAWS installed.

AGREE

135.154(b) Terrain awareness and warning system: Airplanes manufactured on or before March 29, 2002.

Not Applicable

Applicable only to airplanes manufactured on or before March 29, 2002.

AGREE


Compliant

The AFM will contain appropriate procedures for the terrain awareness and warning system use; and proper flight crew reaction in response to the terrain awareness and warning system audio and visual warnings.

AGREE

135.155 Fire extinguishers: Passenger-carrying aircraft.

Compliant

EMB-505 has one hand fire extinguisher on the cockpit, behind the copilot seat, and one in the passenger cabin, at the floor level, between the last row of seats and the lavatory partition. Both are filled with Halon 1211/1301 blend rated for classes B and C types of fire.

AGREE

135.157 Oxygen equipment requirements.

Compliant

EMB-505 is pressurized to 6,670 feet equivalent pressure. In the event of a decompression, emergency oxygen is provided to all occupants. Two hours for crew and 30 minutes for passengers for the descent to 10,000 feet in less than 30 minutes. The oxygen system includes a cockpit pressure display for monitoring the system status, as well as pressure sensors in the low pressure supply line. Each crew mask stowage box includes a flow indicator to show when oxygen flow is supplied to the mask. The indicator is a pneumatic "star burst" attached to the valve and visible through the door. Each passenger mask includes a flow indicator to show when oxygen is flowing to the mask. The crew mask has a 100% setting to supply undiluted oxygen at all altitudes, including those above 25,000 feet.

AGREE

135.158 Pitot heat indication systems.

Not Applicable


AGREE

135.159 Equipment requirements: Carrying passengers under VFR at night or under VFR over-the-top conditions.

Title Only

-

AGREE

135.159(a) Equipment requirements: Carrying passengers under VFR at night or

Compliant

EMB-505 is equipped with a third attitude instrument, see details on 91.205(d)(3).

AGREE


A-118


under VFR over-the-top conditions: Gyroscopic rate-of-turn indicator.

135.159(b) Equipment requirements: Carrying passengers under VFR at night or under VFR over-the-top conditions: Slip skid indicator.

Compliant

EMB-505 is equipped with a slip-skid indicator at each pilot station.

AGREE

135.159(c) Equipment requirements: Carrying passengers under VFR at night or under VFR over-the-top conditions: Gyroscopic bank-and-pitch indicator.

Compliant

EMB-505 is equipped with pitch and bank indicator (artificial horizon) at each pilot station. Compliant with 14 CFR 23.1321 (d)(1).

AGREE

135.159(d) Equipment requirements: Carrying passengers under VFR at night or under VFR over-the-top conditions: Gyroscopic direction indicator.

Compliant

EMB-505 is equipped with direction indicator (magnetic heading) at each pilot station. Compliant with 14CFR 23.1321 (d)(4).

AGREE

135.159(e) Equipment requirements: Carrying passengers under VFR at night or under VFR over-the-top conditions: Generators.

Compliant

Compliance with 14 CFR 23.1309 (c) Compliance with 14 CFR 23.1351 (a) Compliance with 14 CFR 23.1351 (c)

AGREE

135.159(f) Equipment requirements: Carrying passengers under VFR at night or under VFR over-the-top conditions: Night flights.

Title Only

-

AGREE

135.159(f)(1) Night flights: Anticollision light system.

Compliant

EMB-505 is equipped with approved Anticollision lights.

AGREE

135.159(f)(2) Night flights: Instrument lights.

Compliant

Comply according to 14 CFR 23.1381(b)

AGREE

135.159(f)(3) Night flights: Flashlight. Compliant

Flashlights are provided, installed behind each cockpit seat.

AGREE

135.159(g) Equipment requirements: Carrying passengers under VFR at night or under VFR over-the-top conditions: Continuous in-flight electrical load.

Definition

-

AGREE

135.159(h) Equipment requirements: Carrying passengers under VFR at night or under VFR over-the-top conditions: Helicopters.

Not Applicable

Applicable only to helicopters

AGREE


A-119


135.161 Communication and navigation equipment for aircraft operations under VFR over routes navigated by pilotage.

Compliant

EMB-505 has two baseline integrated units containing navigation (including a VOR/LOC/GS receiver and a GPS) and communication (VHF COM) radios. A single or dual DME, as well as a single ADF are also available as optional equipment.

AGREE

135.163 Equipment requirements: Aircraft carrying passengers under IFR.

Title Only

-

AGREE

135.163(a) Equipment requirements: Aircraft carrying passengers under IFR: Vertical speed indicator.

Compliant

EMB-505 has a vertical speed indicator at each pilot station.

AGREE

135.163(b) Equipment requirements: Aircraft carrying passengers under IFR: Free-air temperature indicator.

Compliant

EMB-505 has a Total Air Temperature and a Static Air Temperature indicator.

AGREE

135.163(c) Equipment requirements: Aircraft carrying passengers under IFR: Heated pitot tube for each airspeed indicator.

Compliant

Each airspeed indicator has an appropriated heating system. Comply according to 14 CFR 23.1323(d).

AGREE

135.163(d) Equipment requirements: Aircraft carrying passengers under IFR: Power failure warning device.

Compliant

Each gyroscopic (electrical artificial horizon) has a power failure warning device.

AGREE

135.163(e) Equipment requirements: Aircraft carrying passengers under IFR: Alternate source of static pressure.

Compliant

EMB-505 has an alternate source (standby equipment) of altitude, airspeed and vertical speed indications.

AGREE

135.163(f) Equipment requirements: Aircraft carrying passengers under IFR: Single-engine aircraft.

Not Applicable

Applicable only to single-engine aircraft

AGREE

135.163(g) Equipment requirements: Aircraft carrying passengers under IFR: Generators or alternators.

Compliant

Compliance with 14 CFR 23.1309 (c) Compliance with 14 CFR 23.1351 (a) Compliance with 14 CFR 23.1351 (c)

AGREE

135.163(h) Equipment requirements: Aircraft carrying passengers under IFR: Independent sources of energy.

Compliant

Each gyroscopic (electrical artificial horizon) has an independent source of energy.

AGREE

135.163(i) Equipment requirements: Aircraft carrying passengers under IFR:

Definition

-

AGREE


A-120


Continuous in-flight electrical load.

135.165 Communication and navigation equipment: Extended over-water or IFR operations.

Title Only

-

AGREE

135.165(a) Communication and navigation equipment: Extended over-water or IFR operations: Aircraft navigation equipment requirements - General.

Title Only

-

AGREE

135.165(a)(1) Aircraft navigation equipment requirements - General: En route navigation aids.


-

AGREE

135.165(a)(2) Aircraft navigation equipment requirements - General: Independent navigation systems.

Compliant

EMB-505 has two baseline integrated units containing navigation (including a VOR/LOC/GS receiver and a GPS) radios. A single or dual DME, as well as a single ADF are also available as optional equipment.

AGREE

135.165(a)(3) Aircraft navigation equipment requirements - General: IFR operations.

Compliant

EMB-505 has two baseline navigation radios (including VOR/ILS and GPS receivers) and two marker beacon receivers (integrated on the audio panels).

AGREE

135.165(a)(4) Aircraft navigation equipment requirements - General: RNAV system.


-

AGREE

135.165(b) Communication and navigation equipment: Extended over-water or IFR operations: Use of a single independent navigation system for IFR operations.


-

AGREE

135.165(c) Communication and navigation equipment: Extended over-water or IFR operations: VOR navigation equipment.

Compliant

EMB-505 is equipped with a suitable RNAV system.

AGREE

135.165(d) Communication and navigation equipment: Extended over-water or IFR operations: Airplane communication equipment requirements.

Compliant

EMB-505 has two baseline integrated units containing navigation and communication (VHF COM) radios. Both communication radios have two-way voice communication capability.

AGREE

135.165(e) Communication and navigation equipment:

Not Applicable

EMB-505 category already covered on requirement 135.165(d)

AGREE


A-121


Extended over-water or IFR operations: IFR or extended over-water communications equipment requirements.

135.165(f) Communication and navigation equipment: Extended over-water or IFR operations: Additional aircraft communication equipment requirements.

Compliant

EMB-505 has two radio communication systems installed. Each system consists of: (i) One transceiver. (ii) One microphone. (iii) One headsets and one speaker.

AGREE

135.165(g) Communication and navigation equipment: Extended over-water or IFR operations: Extended over-water exceptions.


-

AGREE

135.167 Emergency equipment: Extended overwater operations.

Title Only

-

AGREE

135.167(a) Emergency equipment: Extended overwater operations.

Title Only

-

AGREE

135.167(a)(1) Emergency equipment: Extended overwater operations: Life preserver.


Life vest pouches are provided under each seat as provisions for life vest installation. A TSO'd lifevest with survival locator light is available as optional.

AGREE

135.167(a)(2) Emergency equipment: Extended overwater operations: Liferafts.


Space is provided inside the LH Forward Cabinet inside the passenger cabin for the installation of an optional life raft. Liferaft attachment means will be available to be installed inside this space as optional.

AGREE

135.167(b) Emergency equipment: Extended overwater operations: Required liferaft equipment.


Provisions for installation of all equipment required on this requirement are provided; All items listed on this requirement are provided on the optional liferaft.

AGREE

135.167(c) Emergency equipment: Extended overwater operations: Required liferaft ELT.


A Portable TSO'd ELT integrated to the optional liferaft will be available.

AGREE


Reserved.

AGREE

135.169 Additional airworthiness requirements.

Title Only

-

AGREE

135.169(a) Additional airworthiness requirements.

Not Applicable


AGREE


A-122


135.169(b) Additional airworthiness requirements.

Not Applicable

Applicable only to reciprocating-engine or turbopropeller-powered small airplane that has a passenger seating configuration, excluding pilot seats, of 10 seats or more.

AGREE

135.169(c) Additional airworthiness requirements.

Not Applicable

Applicable only to small airplanes with a passenger seating configuration, excluding any pilot seat, of 10 seats or more,

AGREE

135.169(d) Additional airworthiness requirements: Cargo or baggage compartments.

Not Applicable


AGREE

135.170 Materials for compartment interiors.

Title Only

-

AGREE

135.170(a) Materials for compartment interiors: Requirements set forth in §25.853(a).

Not Applicable

Applicable only to aircraft with a supplemental type certificate issued in accordance with SFAR No. 41 for a maximum certificated takeoff weight in excess of 12,500 pounds

AGREE

135.170(b) Materials for compartment interiors: Additional airworthiness requirements.

Not Applicable


AGREE

135.170(c) Materials for compartment interiors: Thermal/acoustic insulation materials.

Not Applicable


AGREE

135.171 Shoulder harness installation at flight crewmember stations.

Title Only

-

AGREE

135.171(a) Shoulder harness installation at flight crewmember stations.

Not Applicable

Applicable only to aircraft that has a passenger seating configuration, excluding any pilot seat, of 10 seats or more.

AGREE

135.171(b) Shoulder harness installation at flight crewmember stations.


-

AGREE

135.173 Airborne thunderstorm detection equipment requirements.

Not Applicable

Applicable only to aircraft that has a passenger seating configuration, excluding any pilot seat, of 10 seats or more in passenger-carrying operations.

AGREE

135.175 Airborne weather radar equipment requirements.

Not Applicable

Applicable only to large, transport category aircraft in passenger-carrying operations.

AGREE

135.177 Emergency equipment requirements for aircraft having a passenger seating configuration of more than 19 passengers.

Not Applicable

Applicable only to aircraft having a passenger seating configuration, excluding any pilot seat, of more than 19 seats.

AGREE


A-123


135.178 Additional emergency equipment.

Not Applicable

Applicable only to airplane having a passenger seating configuration of more than 19 seats

AGREE

135.179 Inoperable instruments and equipment.


Embraer will propose a MMEL to the Authorities and furnish, inside the operations manuals, all the required information to support the MEL elaboration. The operational manuals are furnished inside each factory delivered airplane.

AGREE

135.180 Traffic Alert and Collision Avoidance System.

Not Applicable


AGREE

135.181 Performance requirements: Aircraft operated over-the-top or in IFR conditions.

Title Only

-

AGREE

135.181(a) Performance requirements: Aircraft operated over-the-top or in IFR conditions.

Title Only

-

AGREE


Not Applicable

Applicable only to single engine airplanes.

AGREE


Compliant

Embraer issues and furnishes the operational manuals, with the required performance data, inside each airplane factory delivered.

AGREE

135.181(b) Performance requirements: Aircraft operated over-the-top or in IFR conditions.

Not Applicable

Applicable only to multiengine helicopters

AGREE

135.181(c) Performance requirements: Aircraft operated over-the-top or in IFR conditions.


-

AGREE

135.181(d) Performance requirements: Aircraft operated over-the-top or in IFR conditions.


-

AGREE

135.183 Performance requirements: Land aircraft operated over water.


-

AGREE

135.185 Empty weight and center of gravity: Currency requirement.

Compliant

The empty weight and center of gravity is measured and delivery with the airplane documentation.

AGREE


A-124

EMB-505 14CFR135 Compliance Subpart D - VFR/IFR Operating Limitations and Weather Requirements



-

AGREE

135.203 VFR: Minimum altitudes. Operator’s Responsibility

-

AGREE

135.205 VFR: Visibility requirements.


-

AGREE

135.207 VFR: Helicopter surface reference requirements.

Not Applicable

Applicable only to Helicopter Operations

AGREE

135.209 VFR: Fuel supply. Operator’s Responsibility

-

AGREE

135.211 VFR: Over-the-top carrying passengers: Operating limitations.


-

AGREE

135.213 Weather reports and forecasts.


-

AGREE

135.215 IFR: Operating limitations.


-

AGREE

135.217 IFR: Takeoff limitations. Operator’s Responsibility

-

AGREE

135.219 IFR: Destination airport weather minimums.


-

AGREE

135.221 IFR: Alternate airport weather minimums.


-

AGREE

135.223 IFR: Alternate airport requirements.


-

AGREE

135.225 IFR: Takeoff, approach and landing minimums.


-

AGREE

135.227 Icing conditions: Operating limitations.

Title Only

-

AGREE

135.227(a) Icing conditions: Operating limitations


-

AGREE

135.227(b) Icing conditions: Operating limitations


-

AGREE

135.227(c) Icing conditions: Operating limitations

Compliant

EMB-505 has ice protection provisions that comply with the requirements in section 34 of Part 135 - Appendix A.

AGREE

135.227(d) Icing conditions: Not Applicable Applicable only to helicopter operations. AGREE


A-125


Operating limitations

135.227(e) Icing conditions: Operating limitations

Compliant

EMB-505 has ice protection provisions that comply with the requirements in section 34 of Part 135 - Appendix A.

AGREE

135.227(f) Icing conditions: Operating limitations


-

AGREE

135.229 Airport requirements. Operator’s Responsibility

-

AGREE

EMB-505 14CFR135 Compliance Subpart E - Flight Crewmember Requirements



-

AGREE

135.243 Pilot in command qualifications.


-

AGREE

135.244 Operating experience. Operator’s Responsibility

-

AGREE

135.245 Second in command qualifications.


-

AGREE

135.247 Pilot qualifications: Recent experience.


-

AGREE

EMB-505 14CFR135 Compliance Subpart F - Crewmember Flight Time and Duty Period Limitations and Rest Requirements



-

AGREE

135.263 Flight time limitations and rest requirements: All certificate holders.


-

AGREE

135.265 Flight time limitations and rest requirements: Scheduled operations.


-

AGREE

135.267 Flight time limitations and Operator’s Responsibility - AGREE


A-126


rest requirements: Unscheduled one- and two-pilot crews.

135.269 Flight time limitation and rest requirements: Unscheduled three- and four-pilot crews.

Not Applicable

Applicable only for operations with three- or four-pilot crew.

AGREE

135.271 Helicopter hospital emergency medical evacuation service (HEMES).

Not Applicable

Applicable only to Helicopter hospital emergency medical evacuation service operations.

AGREE

135.273 Duty period limitations and rest time requirements.

Not Applicable

Applicable only to operations with flight attendants.

AGREE

EMB-505 14CFR135 Compliance Subpart G - Crewmember Testing Requirements



-

AGREE

135.293 Initial and recurrent pilot testing requirements.


-

AGREE


Not Applicable


AGREE

135.297 Pilot in command: Instrument proficiency check requirements.


-

AGREE

135.299 Pilot in command: Line checks: Routes and airports.


-

AGREE


Definition

-

AGREE

EMB-505 14CFR135 Compliance Subpart H - Training


135.321 Applicability and terms used.

Definition

-

AGREE

135.323 Training program: General.


-

AGREE


A-127


135.324 Training program: Special rules.


-

AGREE



-

AGREE

135.327 Training program: Curriculum.


-

AGREE

135.329 Crewmember training requirements.


-

AGREE

135.331 Crewmember emergency training.


-

AGREE



-

AGREE

135.337 Qualifications: Check airmen (aircraft) and check airmen (simulator).


-

AGREE



-

AGREE

135.339 Initial and transition training and checking: Check airmen (aircraft), check airmen (simulator).


-

AGREE



-

AGREE



-

AGREE



-

AGREE

135.345 Pilots: Initial, transition, and upgrade ground training.


-

AGREE

135.347 Pilots: Initial, transition, upgrade, and differences flight training.


-

AGREE

135.349 Flight attendants: Initial and transition ground

Not Applicable


AGREE


A-128


training.


-

AGREE

EMB-505 14CFR135 Compliance Subpart I - Airplane Performance Operating Limitations



-

AGREE

135.363 General.


-

AGREE

135.364 Maximum flying time outside the United States.


-

AGREE

135.365 Large transport category airplanes: Reciprocating engine powered: Weight limitations.

Not Applicable


AGREE

135.367 Large transport category airplanes: Reciprocating engine powered: Takeoff limitations.

Not Applicable


AGREE

135.369 Large transport category airplanes: Reciprocating engine powered: En route limitations: All engines operating.

Not Applicable


AGREE

135.371 Large transport category airplanes: Reciprocating engine powered: En route limitations: One engine inoperative.

Not Applicable


AGREE

135.373 Part 25 transport category airplanes with four or more engines: Reciprocating engine powered: En route limitations: Two engines inoperative.

Not Applicable


AGREE

135.375 Large transport category airplanes: Reciprocating engine powered: Landing limitations: Destination airports.

Not Applicable


AGREE

135.377 Large transport category airplanes: Reciprocating

Not Applicable


AGREE


A-129


engine powered: Landing limitations: Alternate airports.

135.379 Large transport category airplanes: Turbine engine powered: Takeoff limitations.

Not Applicable


AGREE

135.381 Large transport category airplanes: Turbine engine powered: En route limitations: One engine inoperative.

Not Applicable


AGREE

135.383 Large transport category airplanes: Turbine engine powered: En route limitations: Two engines inoperative.

Not Applicable


AGREE

135.385 Large transport category airplanes: Turbine engine powered: Landing limitations: Destination airports.

Not Applicable


AGREE

135.387 Large transport category airplanes: Turbine engine powered: Landing limitations: Alternate airports.

Not Applicable


AGREE

135.389 Large nontransport category airplanes: Takeoff limitations.


-

AGREE

135.391 Large nontransport category airplanes: En route limitations: One engine inoperative.


-

AGREE

135.393 Large nontransport category airplanes: Landing limitations: Destination airports.


-

AGREE

135.395 Large nontransport category airplanes: Landing limitations: Alternate airports.


-

AGREE

135.397 Small transport category airplane performance operating limitations.

Not Applicable

Applicable only to turbine engine powered small transport category airplane.

AGREE

135.398 Commuter category airplanes performance

Compliant

AFM will present the performance data.

AGREE


A-130


operating limitations.

135.399 Small nontransport category airplane performance operating limitations.

Not Applicable

Applicable only to small nontransport category airplane.

AGREE

EMB-505 14CFR135 Compliance Subpart J - Maintenance, Preventive Maintenance, and Alterations



-

AGREE

135.413 Responsibility for airworthiness.


-

AGREE

135.415 Service difficulty reports. Operator’s Responsibility

-

AGREE

135.417 Mechanical interruption summary report.


-

AGREE

135.419 Approved aircraft inspection program.

Compliant

Embraer Recommended Scheduled Maintenance Program is included in the Aircraft Maintenance Manual. The instructions and procedures required to execute the aircraft inspections will be issued in the Aircraft Maintenance Manual, and for correction of discrepancies found will be issued in the Fault Isolation Manual.

AGREE

135.421 Additional maintenance requirements.

Title Only

-

AGREE

135.421(a) Additional maintenance requirements: Maintenance Program

Compliant

Embraer will recommend a Scheduled Maintenance Program.

AGREE

135.421(b) Additional maintenance requirements: Manufacturer Maintenance Plan – Definition

Definition

-

AGREE

135.421(c) Additional maintenance requirements

Not Applicable


AGREE

135.421(d) Additional maintenance requirements

Not Applicable


AGREE

135.421(e) Additional maintenance Not Applicable Applicable only to single engine aircraft to AGREE


A-131


requirements

be used in passenger-carrying IFR operations.

135.422 Aging airplane inspections and records reviews for multiengine airplanes certificated with nine or fewer passenger seats.


-

AGREE

135.423 Maintenance, preventive maintenance, and alteration organization.


-

AGREE

135.425 Maintenance, preventive maintenance, and alteration programs.


-

AGREE


-

AGREE

135.429 Required inspection personnel.


-

AGREE

135.431 Continuing analysis and surveillance.


-

AGREE

135.433 Maintenance and preventive maintenance training program.


-

AGREE

135.435 Certificate requirements. Operator’s Responsibility

-

AGREE

135.437 Authority to perform and approve maintenance, preventive maintenance, and alterations.


-

AGREE

135.439 Maintenance recording requirements.

Compliant

For each new aircraft delivered, maintenance recording are issued to demonstrate that all requirements for issuance of airworthiness were complied. The total time in service of the engine, propeller, and rotor are registered in the log book.

AGREE

135.441 Transfer of maintenance records.

Compliant

All the maintenance records are transferred to the Customer at the time of the sale.

AGREE

135.443 Airworthiness release or aircraft maintenance log entry.

Compliant

Each airplane is delivered with airworthiness released and all maintenance records are entry on the documentation delivered.

AGREE


A-132

EMB-505 14CFR135 Compliance Subpart K - Hazardous Materials Training Program


135.501 Applicability and definitions.

Definition

-

AGREE

135.503 Hazardous material training: General.


-

AGREE

135.505 Hazardous materials training required.


-

AGREE

135.507 Hazardous materials training records.


-

AGREE

EMB-505 14CFR135 Compliance Appendix A to Part 135 - Additional Airworthiness Standards for 10 or More Passenger Airplanes


Appendix A Additional Airworthiness Standards for 10 or More Passenger Airplanes

Not Applicable

Applicable only to airplanes for 10 or more passengers.

AGREE

EMB-505 14CFR135 Compliance Appendix B to Part 135 - Airplane Flight Recorder Specifications


Appendix B Airplane Flight Recorder Specifications

Definition

-

AGREE

EMB-505 14CFR135 Compliance Appendix C to Part 135 - Helicopter Flight Recorder Specifications


Appendix C Helicopter Flight Recorder Specifications

Not Applicable


AGREE


A-133

EMB-505 14CFR135 Compliance Appendix D to Part 135 - Airplane Flight Recorder Specification


Appendix D Airplane Flight Recorder Specification

Definition

AGREE

EMB-505 14CFR135 Compliance Appendix E to Part 135 - Helicopter Flight Recorder Specifications


Appendix E Helicopter Flight Recorder Specifications

Not Applicable


AGREE

EMB-505 14CFR135 Compliance Appendix F to Part 135 - Airplane Flight Recorder Specification


Appendix F Airplane Flight Recorder Specification

Definition

-

AGREE


B-1

APPENDIX B MDR TABLES

FROM AIRPLANE

EMB-500 EMB-505

EMB-500 Not Applicable E/ E/ E

TO A

IRPL

AN

E

EMB-505 E/ E/ E Not Applicable


C-1

APPENDIX C – ODR TABLES


OPERATOR DIFFERENCE REQUIREMENTS (ODR) TABLES

EMB-505 TO EMB-500 DIFFERENCES - GENERAL

COMPLIANCE METHOD

Base Aircraft: EMB-500 Difference Aircraft: EMB-505

TRAINING Checking/Currency

DESIGN REMARKS FLT CHAR

PROC CHNG

Training Level

Device FLT CHK

CURR

DIMENSIONS Increased Dimensions Length = + 9 ft 3 in (2.82 m) Height = + 2 ft 5.8 in (0.75 m) Wing span = + 11 ft 9.7 in (3.61 m) EMB-500 Length = 42 ft 1 in (12.82 m) Height = 14 ft 3.2 in (4.35 m) Wing span = 40 ft 4.3 in (12.30 m) EMB-505 Length = 51 ft 4in (15.64 m) Height = 16 ft 9 in (5.10m) Wing span = 52 ft 2 in (15.91 m)

No No A POH/ AFM

A A

CABIN Maximum occupants: EMB-500 = up to 6 seats EMB-505 = up to 9 seats

No No A POH/ AFM

A A

CARGO COMPARTMENTS

Cargo capacity increased in 0.405 m.cu EMB-500= 1.705 m.cu (total) EMB-505= 2.11 m.cu (total)

No No A POH/ AFM

A A

LIMITATIONS Weight

Weight Limitations Increased.

505 MRW

+ 3430 kg

MTOW + 3400 kg MLW + 3220 kg MZFW + 2520 kg

No No A POH/ AFM

A A


500 505 MRW

4770 kg 8200 kg

MTOW

4750 kg 8150 kg

MLW 4430 kg 7650 kg MZFW 3803 kg 6350 kg

LIMITATONS Center of Gravity

Limits for conditions of cruise with flaps and gear ups. EMB-500 = 23.5% to 36.9% at MTOW 21.5% to 38.5% at MZFW EMB-505 = 19% to 32% at MTOW 22% to 39% at MZFW

No No A POH/ AFM

A A

LIMITATIONS Speeds

VA increased. Refer to specific model AFM for VMCA and VMCG values.

No No A POH/ AFM

A A

NOISE LEVELS In EPNdb

EMB-500 = 70.4 Flyover 81.4 Lateral 86.1 Approach EMB-505 = TBD

No No A POH/ AFM

A A

Table I: General differences between EMB-500 and EMB-505


EMB-505 to EMB-500 DIFFERENCES - SYSTEMS

COMPLIANCE METHOD



SYSTEM DIFFERENCES FLT CHAR

PROC CHNG

TrainingLevel

Device FLT CHK

CURR

21 AIR CONDITIONING

EMB-500 max alt = 41000 ft, max alt cab de 8000 ft, delta-p = 8,34 psid EMB-505 max alt = 45000 ft, max alt cab de 6640 ft, delta-p = 9,36 psid PRENS/AIR Conditioning Panel EMB-500 Switch name “BLEED” commands PRSOVs. EMB-505 Switch name “ECS” commands FCSOVs Ground Operation EMB-500 If switch “BLEED” is active, FCSOVs appears open in Synoptic. EMB-505 Has one cross-bleed valve, that allows one bleed works for two FCSOVs, and ECS switch controls FCSOVs directly. If temperature higher than 30ºC the ECS is automatically closed, this automatically logic is superseded by the ECS switch commands and open the FCSOV selected. Additional CAS Message: - ECS 1(2) OFF - ECS 1(2) VALVE FAIL

No Yes B SU A A

22 AUTO FLIGHT EMB-505 has additionally:

• Ventral Rudder Control

No Yes A POH/ AFM

A A

23 COMMUNICATIONS

EMB-505 FMS panel allows frequency selection of COMM and NAV, and configuration of XPDR.

No No A POH/ AFM

A A


24 ELECTRICAL POWER

EMB-500 EMB-505

Shed Bus -

One additional shed bus

Circuit Break Panel

-

One additional CB panel behind

pilot seat.

Generator 2x 325A

2x 400A, limited in

350A when on Ground

Battery 2x VLRA 27Ah

1x 34Ah

1x 36Ah (engine start)

No No A POH/ AFM

A A

26 FIRE PROTECTION

EMB-505 Engine Fire Test switch has different location and additional functions: Ice, Stall, Alarms. Baggage compartment smoke detection system is presented on EMB-505 with “BAG SMK”, “BAG SMK FAIL” e “BAG SMK FAULT” messages on CAS.

No Yes A POH/AFM

A A

27 FLIGHT CONTROLS

EMB-505 has additionally:

• Hydraulically operated spoilers;

• Rudder Booster System; • Ventral Fin and Ventral

Rudder; • Two additional flap panels • Pusher is hydraulic (EMB-500

is electrical)

Yes Yes C FFS/ ACFT

C B

28 FUEL Max usable quantity per wing-tank increased in 573.6 kg. Fuel LO LEVEL message trigger point increased in 50 kg. Pressurized refuelling system for EMB-505.

No Yes B SU A A


EMB-500 Max usable quantity per tank = 636,4 kg Unusable quantity per tank = 10 kg Fuel LO LEVEL message trigger = 90 kg Imbalance message trigger = 100 kgImbalance procedure – In case of massage the XFR should be open through a push button in the panel. The pilot should monitor the equalization. EMB-505 Max usable quantity per tank = 1210 kg Fuel LO LEVEL message trigger = 140 kg Imbalance message trigger = 140 kgImbalance procedure – In case of message pilot should identify which tank should be selected for consumption. This selection is made by a rotary switch in cockpit panel.

29 HYDRAULIC POWER

EMB-505 has Two engine driven pumps with one Shutoff Valve before each, while EMB-500 has one Motor Pump in Power pack concept, with just one Shutoff Valve. Hydraulic Pump Panel has different operation. EMB-505 has three additional CAS messages.

No Yes B SU A A

30 ICE AND RAIN PROTECTION

EMB-505 has, optionally, an Ice Detector. EMB-505 has thermal anti-ice system for wings and leading edges surfaces. (Horizontal Stabilizer)

No Yes B SU A A

32 LANDING GEAR

EMB-500 EMB-505

Extended - VLE - KIAS

275 250

VLO-extension 180 250

VLO-retraction 180 250

No Yes B SU B A


Landing Gear Free Fall Lever has different position and shape. Brake System Different pedal to brake pressure transfer function

EMB-500 EMB-505

Brake Assembly

Steel heat sink

Carbon heat sink

Emergency /

Parking Brake

Accumulator

Piston Type –

requires nitrogen recharge

Bellow Type – free of

maintenance

Shutoff Valve

Cycles every pedal

actuation

Open once,

after LG extension

33 LIGHTS EMB-505 has a Refuelling Panel Light. Lights Panel.

No No A POH/AFM

A A

34 NAVIGATION

EMB-505 has additionally radio altimeter and TCAS II. EMB-500 has MDA/DH alerting based only on the barometric altitude (referred the landing field elevation) whereas for EMB-505 the MDA/DH alerting may be based either on the barometric altitude or on the radar altimeter height. EMB-505 FMS panel allows frequency selection of COMM and NAV, and configuration of XPDR.

No Yes A POH/AFM

A A

35 OXYGEN The EMB-505 oxygen cylinder has a No No A POH/ A A


capacity additional of 27 cu.ft (optional). EMB-500 - 50 cu.ft. EMB-505 - 77 cu.ft.

AFM

36 PNEUMATIC

EMB-505 has one panel in the cockpit dedicated to the Pneumatic System. Through the panel the pilot has control over the PRSOV 1 and 2 as well as XBV. There is an AMS Controller which is responsible for controlling and monitoring the Pneumatic System, Wing and Horizontal Stabilizer Anti-Ice System, as well as providing open loop control for both FCSOVs. Besides BLEED 1(2) FAIL, BLEED 1(2) OFF and BLEED 1(2) LEAK, the pneumatic system also comprises the following CAS messages: - AMS CTRL FAIL - AMS CTRL FAULT - BLEED 1(2) OVERPRES - XBLEED FAIL - XBLEED SW OFF - EBAY LEAK - A-I WINGSTB LEAK Even though, BLEED 1(2) FAIL and BLEED 1(2) LEAK exist in the EMB-500, the EMB-505 pilot's procedures are different.

No Yes B SU A A

71 POWER PLANT EMB-500 - P&W 617F-E - Thrust: 1695 lbs - Dual Channel FADEC - Airframe mounted - High bypass ratio 2.7 - Low speed spool (Single stage direct drive low pressure compressor, single stage low pressure turbine) - High speed spool (Two stage high pressure compressor, Single stage high pressure turbine) N1 = 100% (MAX) N2 = 59% (MIN) ; 100.4 (MAX) ITT: START = 892°C (MAX)

Yes No A POH/AFM

B B


NORMAL T/O = 830°C (MAX) MAX. T/O = 845°C MAX. CONTINUOUS = 830°C EMB-505 - P&W 535-E - PW535E Thrust: 3360 lbs - High bypass ratio 3.0 - Low speed spool (Single stage fan, Single stage booster, Two stage low pressure turbine) - High speed spool (Three stage high pressure compressor, Single stage high pressure turbine) N1 = 100% (MAX) N2 = 55.1% (MIN) ; 100% (MAX) ITT: START = 740°C (MAX) NORMAL T/O = 700°C (MAX) MAX. T/O = 725°C MAX. CONTINUOUS = 680°C

79 ENGINE OIL

EMB-505 has additional CAS message (OIL IMP BYPASS), procedure

No No A POH/ AFM

A A

80 ENGINE START EMB-505 has Windmill Start. No Yes C FFS/ ACFT

C B

Table II: System differences between EMB-505 and EMB-500


EMB-505 MANEUVERS OPERATOR DIFERENCES REQUIREMENTS

COMPLIANCE METHOD DIFFERNCE ACFT: EMB-505 BASE ACFT: EMB-500 TRAINING

Checking/Currency

MANEUVER REMARKS FLT CHAR

PROC CHG

Training level Device FLT

CHECK CURREN

CY

-Different systems panels positions and systems operation

No Yes A POH/

AFM A A

Preparation

-Different external inspection No Yes A POH/ AFM

A A

Start Different engines, different limitations with similar procedures Yes No

A POH/ AFM

A A

Normal Take Off

Different T.O. angles due to different performance

Flap Pitch Angle

1 11 TBD 2 9 TBD

Yes No

E FFS/ ACFT

E E

Climb Different performance Yes No A POH/ AFM

A A

Cruise Different performance – ability to exceed vmo/ mmo in level flight Yes No

A POH/ AFM

A A

Approach Maneuverability at low speed Yes No E FFS/

ACFT E E

Non-Normal Maneuvers

– Different systems, more complex with different and additional procedures

Yes Yes

B SU B B


- Engine airstart with wind milling capability

No Yes

B SU B B

- Flight Controls - Ventral rudder - Rudder booster with one engine

Yes Yes

E FFS/ ACFT

E E

-Landing with one engine inoperative with different flap position

No Yes

E FFS/ ACFT

E e

- Engine fail, more pronounced rolling moment Yes No

E FFS/ ACFT

E e

Table III: Operational differences between EMB-505 and EMB-500 models


EMB-500 TO EMB-505 DIFFERENCES - GENERAL

COMPLIANCE METHOD



DESIGN REMARKS FLT CHAR

PROC CHNG

Training Level

Device FLT CHK

CURR

DIMENSIONS Decreased dimensions Length = - 9 ft 3 in (2.82 m) Height = - 2 ft 5.8 in (0.75 m) Wing span = - 11 ft 9.7 in (3.61 m) EMB-505 Length = 51 ft 4in (15.64 m) Height = 16 ft 9 in (5.10m) Wing span = 52 ft 2 in (15.91 m) EMB-500 Length = 42 ft 1 in (12.82 m) Height = 14 ft 3.2 in (4.35 m) Wing span = 40 ft 4.3 in (12.30 m)

No No A POH/ AFM

A A

CABIN Maximum occupants: EMB-505 = up to 9 seats EMB-500 = up to 6 seats

No No A POH/ AFM

A A

CARGO COMPARTMENTS

Cargo capacity decreased in 0.405 m.cu EMB-505= 2.11 m.cu (total) EMB-500= 1.705 m.cu (total)

No No A POH/ AFM

A A

LIMITATIONS Weight

Weight Limitations decreased.

500 MRW

- 3430 kg

MTOW - 3400 kg MLW - 3220 kg MZFW - 2547 kg

500 505

No No A POH/ AFM

A A


MRW

4770 kg 8200 kg

MTOW 4750 kg 8150 kg MLW 4430 kg 7650 kg MZFW 3803 kg 6350 kg

LIMITATONS Center of Gravity

Limits for conditions of cruise with flaps and gear ups. EMB-500 = 23.5% to 36.9% at MTOW 21.5% to 38.5% at MZFW EMB-505 = 19% to 32% at MTOW 22% to 39% at MZFW

No No A POH/ AFM

A A

LIMITATIONS Speeds

VA decreased. Refer to specific model AFM for VMCA and VMCG values.

No No A POH/ AFM

A A

NOISE LEVELS In EPNdb

EMB-500 = 70.4 Flyover 81.4 Lateral 86.1 Approach EMB-505 = TBD

No No A POH/ AFM

A A

Table IV: General differences between EMB-500 and EMB-505


EMB-500 to EMB-505 DIFFERENCES - SYSTEMS

COMPLIANCE METHOD



SYSTEM DIFFERENCES FLT CHAR

PROC CHNG

TrainingLevel

Device FLT CHK

CURR

21 AIR CONDITIONING

EMB-505 max alt = 45000 ft, max alt cab de 6640 ft, delta-p = 9,36 psid EMB-500 max alt = 41000 ft, max alt cab de 8000 ft, delta-p = 8,34 psid PRENS/AIR Conditioning Panel EMB-505 Switch name “ECS” commands FCSOVs EMB-500 Switch name “BLEED” commands PRSOVs. Ground Operation EMB-505 Has one cross-bleed valve, that allows one bleed works for two FCSOVs, and ECS switch controls FCSOVs directly. If temperature higher than 30ºC the ECS is automatically closed, this automatically logic is superseded by the ECS switch commands and open the FCSOV selected. EMB-500 If switch “BLEED” is active, FCSOVs appears open in Synoptic. Does not have CAS Message of: - ECS 1(2) OFF - ECS 1(2) VALVE FAIL

No Yes A POH/AFM

A A

22 AUTO FLIGHT EMB-500 does not have:

• Ventral Rudder Control

No Yes A POH/ AFM

A A

23 COMMUNICATIONS

EMB-500 FMS panel does not allow frequency selection of COM and NAV, and configuration of XPDR.

No No A POH/ AFM

A A


24 ELECTRICAL POWER

EMB-500 EMB-505

Shed Bus

One Shed bus

One additional shed bus

Circuit Break Panel

One CB panel

behind each

cockpit seat.

One additional CB panel behind

pilot seat.

Generator 2x 325A

2x 400A, limited in

350A when on ground

Battery 2x VLRA 27Ah

1x 34Ah

1x 36Ah (engine start)

No No A POH/ AFM

A A

26 FIRE PROTECTION

EMB-500 does not have Engine Fire Test switch. It has only a dedicated bottom for engine fire test. EMB-500 does not have Baggage compartment smoke detection system.

No Yes A POH/AFM

A A

27 FLIGHT CONTROLS

EMB-500 does not have:

• Hydraulically operated spoilers;

• Rudder Booster System; • Ventral Fin and Ventral

Rudder; and

EMB-505 has:

• Two additional flap panels • Pusher is hydraulic (EMB-500

is electrical)

Yes Yes B SU A A

28 FUEL Max usable quantity per wing-tank decreased in 573.6 kg. Fuel LO LEVEL message trigger point decreased in 50 kg. EMB-500 does not have Pressurized refuelling system.

No Yes B SU A A


EMB-505 Max usable quantity per tank = 1210 kg Fuel LO LEVEL message trigger = 140 kg Imbalance message trigger = 140 kgImbalance procedure – In case of message pilot should identify which tank should be selected for consumption. This selection is made by a rotary switch in cockpit panel. EMB-500 Max usable quantity per tank = 636,4 kg Unusable quantity per tank = 10 kg Fuel LO LEVEL message trigger = 90 kg Imbalance message trigger = 100 kgImbalance procedure – In case of massage the XFR should be open through a push button in the panel. The pilot should monitor the equalization.

29 HYDRAULIC POWER

EMB-500 has one Motor Pump in Power pack concept, with just one Shutoff Valve, while EMB-505 has Two engine driven pumps with one Shutoff Valve before each. Hydraulic Pump Panel has different operation.

No Yes B SU A A

30 ICE AND RAIN PROTECTION

EMB-500 does not have an Ice Detector. EMB-500 does not have thermal anti-ice system for wings and leading edges surfaces. (Horizontal Stabilizer)

No Yes B SU A A

32 LANDING GEAR

EMB-505 EMB-500

Extended - VLE - KIAS

250 275

VLO-extension 250 180

VLO-retraction 250 180

No Yes B SU A A


Landing Gear Free Fall Lever has different position and shape. Brake System Different pedal to brake pressure transfer function

EMB-505 EMB-500

Brake Assembly

Carbon heat sink

Steel heat sink

Emergency /

Parking Brake

Accumulator

Bellow Type – free of

maintenance

Piston Type –

requires nitrogen recharge

Shutoff Valve

Open once,

after LG extensio

n

Cycles every pedal

actuation

33 LIGHTS EMB-500 does not have a Refuelling Panel Light.

No No A POH/AFM

A A

34 NAVIGATION

EMB-500 does not have radio altimeter and TCAS II. EMB-500 has MDA/DH alerting based only on the barometric altitude (referred the landing field elevation). EMB-500 FMS panel does not allow frequency selection of COM and NAV, and configuration of XPDR.

No Yes A POH/AFM

A A

35 OXYGEN

EMB-500 oxygen cylinder has a capacity of 50 cu.ft only.

No No A POH/ AFM

A A

36 PNEUMATIC

EMB-500 does not have a panel in the cockpit dedicated to the Pneumatic System. Even though, BLEED 1(2) FAIL and BLEED 1(2) LEAK exist on both aircraft, the pilot's procedures are different.

No Yes B SU A A

71 POWER PLANT EMB-505 - P&W 535-E - PW535E Thrust: 3360 lbs - High bypass ratio 3.0

Yes No A POH/AFM

A A


- Low speed spool (Single stage fan, Single stage booster, Two stage low pressure turbine) - High speed spool (Three stage high pressure compressor, Single stage high pressure turbine) N1 = 100% (MAX) N2 = 55.1% (MIN) ; 100% (MAX) ITT: START = 740°C (MAX) NORMAL T/O = 700°C (MAX) MAX. T/O = 725°C MAX. CONTINUOUS = 680°C EMB-500 - P&W 617F-E - Thrust: 1695 lbs - High bypass ratio 2.7 - Low speed spool (Single stage direct drive low pressure compressor, single stage low pressure turbine) - High speed spool (Two stage high pressure compressor, Single stage high pressure turbine) N1 = 100% (MAX) N2 = 59% (MIN) ; 100.4 (MAX) ITT: START = 892°C (MAX) NORMAL T/O = 830°C (MAX) MAX. T/O = 845°C MAX. CONTINUOUS = 830°C

79 ENGINE OIL

EMB-500 does not have the CAS message (OIL IMP BYPASS). The pilot must inspect one mechanic pop-up on the engine.

No No A POH/ AFM

A A

80 ENGINE START EMB-500 does not have Windmill Start.

No Yes A POH/ AFM

A A

Table V: System differences between EMB-500 and EMB-505


EMB-500 MANEUVERS OPERATOR DIFERENCES REQUIREMENTS

COMPLIANCE METHOD DIFFERNCE ACFT: EMB-500 BASE ACFT: EMB-505 TRAINING

Checking/Currency

MANEUVER REMARKS FLT CHAR

PROC CHG

Training level Device FLT

CHECK CURREN

CY

-Different systems panels positions and systems operation No Yes A POH/

AFM A A

Preparation -Different external inspection No Yes A POH/

AFM A A

Start Different engines, different limitations with similar procedures Yes No

A POH/ AFM

A A

Normal Take Off

Different T.O. angles due to different performance

Flap Pitch Angle

1 11 TBD 2 9 TBD

Yes No

E FFS/ ACFT

E E

Climb Different performance Yes No E FFS/ ACFT

E E

Cruise Different performance Yes No A POH/

AFM A A

Approach Maneuverability at low speed Yes No E FFS/

ACFT E E

Non-Normal Maneuvers

– Different systems, more complex with different and additional procedures

Yes Yes

B SU B B


- Engine airstart with wind milling capability

No Yes

B SU B B

- Flight Controls - Ventral rudder - Rudder booster with one engine

Yes Yes

E FFS/ ACFT

E E

-Landing with one engine inoperative with different flap position

No Yes

E FFS/ ACFT

E E

- Engine fail, more pronounced rolling moment Yes No

E FFS/ ACFT

E E

Table III: Operational differences between EMB-505 and EMB-500 models


D-1

APPENDIX D – BOARD RECORD Original FSB- EMB-500 TIME AND LOCATION – The EMB-500 FSB convened on August 20, 2008, at CAE SimuFlite at Dallas Fort Worth, Texas Airport. This ground school was conducted as part of a Joint Operational Evaluation Board T-5 test evaluation with EASA and ANAC subject pilots acting as the students. This ground school consisted of five days of ground school and Integrated Procedures Training. The FAA members of the JOEB are considered the FAA Flight Standardization Board. The JOEB members critiqued the training materials consisting of Web Based Training, Pilot Operating handbooks, and Pilot Training Manuals. There were a considerable amount of comments made as the training material was understandably based upon previous material provided by Embraer. The FAA FSB then proceeded to Araraquarra, S.P. Brazil to evaluate and undergo aircraft flight training on August 29, 2008. BOARD COMPOSITION – All four FSB members held airline transport pilot certificates (ATP) with an airplane category and multiengine class rating, and one or more type ratings. They were experienced general aviation or air carrier inspectors, with an extensive background in airman evaluation and certification. FSB TRAINING – Ground training was scheduled and provided by CAE instructors that had been issued Letters of Authorization to conduct ground training and provided endorsements that the FSB and JOEB members had completed the ground training required by 14CFR 61.157 and 61.63. Integrated Procedures Training was conducted at CAE SimuFlite by these same instructors. No flight training credit was credited nor did CAE SimuFlite seek any flight training credit for this training. All flight training was conducted in the EMB-500 airplane by the Embraer instructor pilots that had been issued LOA’s to conduct the flight training and make endorsements in accordance with 14CFR61.157 and 14CFR 61.63. Training flights originated from Araraquarra Embraer Flight Test facility at SBGP. The FSB performed an evaluation of all PTS maneuvers required for an airman to receive an airman certificate with an EMB-500 type rating. The FSB completed approximately 54 hours of aircraft operations, including type rating practical tests, to determine if the EMB-500 was suitable for operations under Parts 91 and 135. Additionally, the FSB evaluated normal, abnormal, and emergency procedures, which are included in the airplane flight manual (AFM). FSB TESTS – Board members completed the type rating practical test in accordance with Airline Transport Pilot and Aircraft Type Rating Practical Test Standards for Airplane, dated July 2008, Document No. FAA-S-8081-5E. This method of evaluating a new aircraft type, entering service for the first time in the United States, is described and referred to in AC 120-53 as the T-5 Test. The T-5 Test is used for evaluating a new base aircraft when a new type rating designation will be required, and when a variant does not exist. EMB-505 FSB TIME AND LOCATION- The EMB-505 FSB convened November 16, 2009 at CAE SimuFlite in Dallas/Fort Worth Airport to begin a recurrent ground school. This consisted of an update of the status of the EMB-500 program and the EMB-500 aircraft flight maneuver package. Then the FSB moved to Alliance Fort Worth


D-2

(AFW) airport where an EMB-500 airplane, PP-XOG, was located. This airplane was a Brazilian registered experimental airplane and had been used to conduct training and checking for all applicants due to a qualified EMB-500 simulator not being available. Qualification at an interim Level C had been recently accomplished but due to the training back log, the FSB was conducted entirely in two airplanes, one EMB-500 and one EMB-505. BOARD COMPOSITION-Three members of the Board were members of the original EMB-500 FSB and were rated in the EMB-500. One member was not type rated in the EMB-500 but had extensive turbojet experience. FSB TRAINING-Each FSB member accomplished 2 two-hour training flights in PP-XOG and then accomplished a no jeopardy check ride to base line their performance in the EMB-500. Then FSB members were relocated to DFW and received 6 hours of ground training per Embraer’s proposed T5 test and Operator Difference Requirement Documents. FSB members felt that 6 hours of ground school was not enough and that 8 would be a minimum. Then FSB members relocated to AFW and were trained in selected maneuvers in PP-XVG, another Brazilian registered experimental EMB-505 airplane. This airplane had no interior, had flight test equipment, but was functionally equivalent to a conformed production airplane. Due to it not having an interior, it did not have a smoke detector. The ice protection system was not approved. Load 35 of the Prodigy avionics suite was installed. Both test airplanes, being Brazilian registered, were operated in accordance with the ANAC approved AFM and QRH in the case of PP-XOG and a draft AFM and QRH, in the case of PP-XVL. The significance of this fact is that the weights and measures were in kilograms and liters. Brazilian pilots issued LOA’s by the FSB Chairman, acted as PIC for all flights. A risk assessment of the proposed flight maneuvers and procedures were conducted by Embraer flight test pilots and flight test engineers in accordance with a risk assessment process approved by ANAC and accepted by the FAA. This was previously coordinated with FAA validation pilots prior to their FAA validation flights conducted the week before in the same airplane. FSB members were trained in the variant airplane, the EMB-505, in specific maneuvers. This consisted of Normal Preflight and Cockpit Preparation, Normal Takeoff, Climb to altitude for airwork consisting of steep turns, all stalls, a demonstration of the rudder boost system, and single engine maneuvering, followed by multiple approaches, both single engine and all engine operating to missed approaches and rejected landings at Waco, Texas with an approach and landing at Alliance Fort Worth.. FSB TESTS – After receiving the approximately 2 hours each in the EMB-505 Board members completed the type rating practical test in accordance with Airline Transport Pilot and Aircraft Type Rating Practical Test Standards for Airplane, dated July 2008, Document No. FAA-S-8081-5E. The Board performed an evaluation of all PTS maneuvers required for an airman to receive an airman certificate with an EMB-505 type rating. The FSB completed approximately 40 hours of aircraft operations, including type rating practical tests. Due to the evaluation of the Operator Differences Requirements submitted by Embraer prior to the convening of the FSB, it was determined by the FSB Chairman that a T5 test for a shortened transition course, in accordance with the procedures described in AC 120-53A was appropriate. Embraer’s ODR proposal included no Level E differences identified several flight maneuvers as Level C and that these maneuvers be trained in either a Full Flight Simulator or the aircraft. This is in fact the AC 120-53A definition of Level E differences. After flying both aircraft the Board set some maneuvers at Level E. Additionally, the Board made recommendations that the differences training be increased to at least two training flights in the EMB-505 or EMB-500, as appropriate to which aircraft the applicant is transitioning.