mmel ce-510 - t c · web view(flc, alt, vnv, vs) i. i -10 c 4 3 i -20 b 4 0 may be inoperative...

U.S. Department of TransportationFederal Aviation AdministrationWashington, D.C.

Master Minimum Equipment List (MMEL)

Revision: 1Date: 04/04/2013

Cessna-510

For PART 91 and PART 135 ONLY

Thomas M. KieffaberChair, Flight Operations Evaluation Board

Federal Aviation Administration Kansas City Aircraft Evaluation Group

901 Locust Street, Department of Transportation BuildingKansas City, MO 64106

Telephone: (816) 329-3233FAX: (816) 329-3241

This Page Intentionally Left Blank

U.S. DEPARTMENT OF TRANSPORTATIONMASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATIONAIRCRAFT:

CESSNA 510REVISION NO. 1DATE: 04/04/2013

PAGE NO.I

TABLE OF CONTENTS / CONTROL PAGESYSTEM PAGES REVISION DATE

-- Cover Page - 1 04/04/2013-- Table of Contents / Control Page I 1 04/04/2013-- Highlights of Change II, III, IV, V 1 04/04/2013-- Definitions and Preamble VI 1 04/04/2013-- Guidelines for (M) & (O) Procedures

VII 1 04/04/2013

-- Section One VIII 1 04/04/201321 Air Conditioning 21-1 thru 21-3 1 04/04/201322 Auto Flight 22-1 1 04/04/201323 Communications 23-1 thru 23-4 1 04/04/201324 Electrical 24-1 1 04/04/201325 Equipment/Furnishings 25-1 thru 25-5 1 04/04/201326 Fire Protection 26-1 1 04/04/201327 Flight Controls 27-1 1 04/04/201328 Fuel 28-1 1 04/04/201330 Ice & Rain Protection 30-1 thru 30-2 1 04/04/201331 Indicating/Recording Systems 31-1 thru 31-2 1 04/04/201332 Landing Gear 32-1 1 04/04/201333 Lights 33-1 thru 33-3 1 04/04/201334 Navigation 34-1 thru 34-7 1 04/04/201335 Oxygen 35-1 1 04/04/201338 Water/Waste 38-1 1 04/04/201345 Central Maintenance System 45-1 1 04/04/201346 Information Systems 46-1 1 04/04/201352 Doors 52-1 thru 52-3 1 04/04/201373 Engine Fuel and Control 73-1 1 04/04/201376 Engine Controls 76-1 1 04/04/2013-- Section Two INT-1 thru INT-3 1 04/04/2013-- CAS Relief 2-1 thru 2-5 1 04/04/2013




PAGE NO.II

HIGHLIGHTS OF CHANGE

NOTE: This revision incorporates a revised numbering format. Definitions and preamble replaced with a requirement to include definitions and preamble in operators MEL.

ATA 21 Moved Cabin Altitude Warning System relief to Chapter 31.-20-01 Added relief for Cockpit Air Outlet.-20-02 Added relief for Cabin Air Outlet.-21-01 Revised remarks and exceptions.-21-02 Revised remarks and exceptions.-21-03 Revised remarks and exceptions.-21-04 Revised title, number required for dispatch, and remarks and exceptions.-30-01 Added relief for Cabin Pressurization System.-31-01 Revised title and remarks and exceptions. -32-01 Revised title and remarks and exceptions. -32-02 Revised title and remarks and exceptions. -33-01 Revised title and remarks and exceptions. -33-02 Revised remarks and exceptions.-33-03 Revised title and remarks and exceptions.-33-04 Added relief for Cabin Dump Function.-50-01 Revised title and remarks and exceptions. -60-01 Revised title and remarks and exceptions.ATA 22 Moved Electric Elevator Trim relief to Chapter 27.-00-01 Revised remarks and exceptions.-10-01 Revised remarks and exceptions.-10-02 Added relief for Go-Around Button.-10-03 Revised title and remarks and exceptions.-10-04 Added relief for Autopilot/Flight Director Sync (CWS Button).ATA 23 Moved Emergency Locator Transmitter (ELT) relief to Chapter 25.-00-01 Added relief for Flight Phone System.-10-01 Added relief for High Frequency (HF) Communications System.-12-01 Revised remarks and exceptions.-20-01 Moved Datalink relief from Chapter 34.-30-01 Added relief for Auxiliary Audio Input System.-30-02 Added relief for XM Radio Wireless Remote System.-40-01 Added relief for Passenger Address (PA) System-50-01 Standardized relief for Flight Deck Headsets Earphone/Headphones and Boom

Microphones with PL-58.-50-02 Added relief for Hand Microphone.-50-03 Added relief for Hand Microphone Jack.-50-04 Added relief for Hand Microphone Holder.-50-05 Revised title and remarks and exceptions. Added relief for individual buttons.-50-06 Added relief for Cockpit Speaker.-60-01 Separated Static Wick relief into zones. -70-01 Added relief for Cockpit Voice RecorderATA 24 Removed relief for Standby Instrument Battery.-31-01 Added relief for Battery Temperature Indication.-40-01 Added relief for External Power System.-60-01 Added relief for Cockpit 12V Outlet.




PAGE NO.III

HIGHLIGHTS OF CHANGE-60-02 Added relief for Interior Disconnect.ATA 25 Removed relief for Passenger Convenience expired on 31 Dec 2007.-00-01 Added relief for Document Holder.-10-01 Added relief for Flight Crew Seat-10-02 Revised title and remarks and exceptions. -10-03 Added relief for Cockpit Assist Handle.-10-04 Deleted remarks and exceptions.-10-05 Added relief for Emergency Gear Handle Cover.-20-01 Revised remarks and exceptions. Added relief for individual items.-20-02 Added relief for Folding Cabin Seat.-20-03 Added relief for Cabin Curtain.-20-04 Added relief for Non-Essential Equipment & Furnishings (NEF)-30-01 Added relief for Cabin Storage Compartment. -30-02 Added relief for Storage Compartment Key Lock.-40-01 Added relief for Ashtray.-60-01 Separated Emergency Medical Equipment by type. -61-01 Added relief for Life Preserver.-62-01 Moved Emergency Located Transmitter (ELT) relief from Chapter 23.-64-01 Added relief for Life Raft.ATA 26-22-01 Revised number required for dispatch and remarks and exceptions.ATA 27-31-01 Moved Electric Elevator Trim relief from Chapter 22.-60-01 Revised remarks and exceptions. -60-02 Added relief for Speed Brake Position.-60-03 Added relief for Speed Brake Switch.-70-01 Added relief for Aileron/Elevator Control Lock.-70-02 Added relief for Rudder Lock.ATA 28-10-01 Added relief for Over-wing Refueling Cap Lock.-41-01 Added relief for Fuel Low Level Indicating System.ATA 30-10-01 Revised title and remarks and exceptions.-10-02 Revised title and remarks and exceptions.-20-01 Revised title and remarks and exceptions.-30-01 Revised title, number installed, number required for dispatch and remarks and

exceptions.-30-02 Revised title, number installed, number required for dispatch, and remarks and

exceptions.-30-03 Added relief for Stall Warning Vane Heater.-40-01 Revised title and remarks and exceptions.-40-02 Added relief for Windshield Rain Repellant.-70-01 Added relief for Air Conditioner FWD Evaporator Drain Heater.ATA 31-20-01 Revised remarks and exceptions.-30-01 Added relief for Flight Data Recorder (FDR) System.-30-02 Added relief for Quick Access Recorder.




PAGE NO.IV

HIGHLIGHTS OF CHANGE-40-01 Added relief for Electronic Checklist.-40-02 Added relief for Fuel Totalizer-50-01 Separated relief for Master Caution/Warning to annunciator and function.-50-02 Added relief for Cabin Altitude Warning SystemATA 32-41-01 Revised remarks and exceptions. Added note.-41-02 Added relief for Tire Spin Down System.ATA 33-10-01 Revised title and remarks and exceptions.-10-02 Revised remarks and exceptions.-10-03 Revised remarks and exceptions.-10-04 Added relief for Cockpit Map Light.-10-05 Added relief for G1000 Display Dimmer.-20-01 Revised title, repair category, number installed, number required for dispatch and

remarks and exceptions.-20-02 Revised title, repair category, number installed, number required for dispatch and

remarks and exceptions.-30-01 Revised title. Added relief for Door Proximity Switch.-30-02 Added relief for Door Proximity Switch.-40-01 Revised title, repair category and remarks and exceptions.-40-02 Revised title and remarks and exceptions.-40-03 Revised title and remarks and exceptions.-40-04 Revised title and remarks and exceptions.-40-05 Revised title.-50-01 Added relief for Cockpit Flashlight and Holder Assembly. ATA 34 Moved Datalink relief to Chapter 23. -23-01 Revised remarks and exceptions.-25-01 Added relief for MFD Remote Mounted Control Panel.-25-02 Added relief for Mode Control Panel.-25-03 Added relief for Synthetic Vision.-25-04 Added relief for Moving Map Display.-25-05 Added relief for certain Primary Flight Display (PFD) buttons/functions.-31-01 Separated from Navigation Equipment. Revised remarks and exceptions.-31-02 Separated from Navigation Equipment. Revised remarks and exceptions.-32-01 Added relief for Glideslope.-34-01 Revised number required for dispatch and remarks and exceptions.-42-01 Revised number required for dispatch and remarks and exceptions.-43-01 Revised remarks and exceptions.-44-01 Added relief for Radar Altimeter System.-44-02 Separated into individual functions. -45-01 Added relief for Traffic Alert and Collision Avoidance System (TCAS).-45-02 Added relief for Traffic Information System (TIS).-45-03 Added relief for Traffic Collision Avoidance Device (TCAD).-51-01 Revised remarks and exceptions. -52-01 Revised remarks and exceptions. Added -04 per PL-076, Revision 05.-52-02 Added relief for ADS-B per PL-105, Revision 01. -55-01 Revised remarks and exceptions.




PAGE NO.V

HIGHLIGHTS OF CHANGE-57-01 Revised title and remarks and exceptions.-60-01 Revised title, repair category, and remarks and exceptions.-60-02 Added relief for Data Loader (SD Card Slot).ATA 35-00-01 Added relief for Oxygen Tank Fill Port.-00-02 Added relief for Plastic Blowout Disc/Green Label.-20-01 Revised remarks and exceptions. Separated relief for Cabin Mask and Drop Out Panel.-30-01 Added relief for Protective Breathing Equipment. -30-02 Added relief for Portable Oxygen Bottles.ATA 38-30-01 Revised remarks and exceptions.ATA 45-00-01 Added relief for Citation Diagnostics and Maintenance System (CDMS).ATA 46-00-01 Added relief for Electronic Flight Bag (EFB) System.ATA 52-10-01 Grouped items under Cabin Door. Revised remarks and exceptions. Added relief for

Gust Lock, Pull Chain, Step Assembly and Step Support Cable. -20-01 Added relief for Escape Hatch Pin.-30-01 Grouped items under Baggage Doors. Revised remarks and exceptions. Added relief

for Nose Door Gas Spring, Aft Door Gas Spring and Aft Door Seal. -70-01 Grouped items under Cabin Door Monitoring System. Revised remarks and exceptions. ATA 73 Moved Engine Synchronizer System relief to Chapter 76.-31-01 Revised remarks and exceptions.ATA 76-01-01 Moved Engine Synchronizer System relief from Chapter 73.

Section Two

Added relief for CAS messages.




PAGE NO.VI

DEFINITIONS AND PREAMBLE

DEFINITIONS

The required definitions listed are listed in Appendix B of MMEL Policy Letter 25. Additional definitions may be included in an operators MEL as desired. Revision of PL-025 does not require revision to the operator’s MEL.

PREAMBLE

The applicable preamble must be inserted in the operator’s MEL from current FAA Policy Letter PL-34 or Policy Letter PL-36.




PAGE NO.VII

GUIDELINES FOR (M) & (O) PROCEDURES

The FOEB has identified a need for certain procedures to provide an adequate level of safety while providing relief for some items. These procedures must be established by the operator and may be based on the aircraft manufacturer’s recommended procedures, Supplemental Type Certificate modifier’s recommended procedures, or equivalent operator procedures. When recommended procedures are published the operator should comply with these procedures. If recommended procedures are not published, the following guidelines delineate the aspects to be considered by the operator in the development of required procedures.

Cessna has developed recommended (M) maintenance and (O) operational procedures for the Cessna 510 Master Minimum Equipment List (P/N 510COMP-01-00, or later revision). Operator’s MEL procedures should be based on the Cessna procedures.




PAGE NO.VIII

SECTION ONE

LRU ORIENTED MMEL RELIEF




PAGE NO.21-1

SYSTEM, SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH4. REMARKS AND EXCEPTIONS

21 AIR CONDITIONING

-20-01 Cockpit Air Outlet C 2 0 I-20-02 Cabin Air Outlet C - 1 I-21-01 Fresh Air Fan C 1 0 May be inoperative provided

pressurization system is operative. I-21-02 Cabin Fan C 1 0 May be inoperative provided:

a) Cockpit fan is operative, andb) CABIN FAN remains OFF.

III

-21-03 Cockpit Fan C 1 0 May be inoperative provided:a) Cabin fan is operative,b) Cabin and cockpit temperature

control system is operative,c) All glareshield fans are operative,

andd) COCKPIT FAN remains OFF.

IIIIIII

-21-04 Glareshield Fan C 3 1 May be inoperative provided:a) Cockpit fan is operative and

selected ON, and b) Air conditioning system is

operative and selected ON.

II

-30-01 Cabin Pressurization System(Unpressurized)

C 1 0 (O) May be inoperative provided:a) PRESS CTRL is selected to

STANDBY,b) CABIN DUMP is selected ON,c) Aircraft is operated at 14,100 feet

cabin altitude or below, andd) Flight crew oxygen system is

operative and used as required by 14 CFR.

IIIIIIIII

NOTE: PRESS CTRL amber message will appear. CABIN ALTITUDE red message may appear at 9,800 +/- 200 feet cabin altitude.

IIII

-31-01 Pressurization Controller Auto Schedule Mode (NORM)(Unpressurized)

C 1 0 May be inoperative provided cabin pressurization system is considered inoperative.

IIII

-32-01 Cabin Differential Pressure (EICAS Indication)

-01 (Unpressurized) C 1 0 May be inoperative provided cabin pressurization system is considered inoperative.

III




PAGE NO.21-2




21 AIR CONDITIONING

-02 (Pressurized) C 1 0 (O) May be inoperative provided:a) Cabin altitude and rate (EICAS

Indication) are operative, b) Pressurization controller auto

schedule mode is operative, andc) A chart is provided and used to

convert cabin and aircraft altitude to differential pressure.

III

I

-32-02 Cabin Altitude (EICAS Indication)

-01 (Unpressurized) C 1 0 May be inoperative provided cabin pressurization system is considered inoperative.

III

-02 (Pressurized) C 1 0 (O) May be inoperative provided:a) Cabin differential pressure (EICAS

Indication) is operative,b) Pressurization controller auto

schedule mode is operative, andc) A chart is provided and used to

convert aircraft altitude and differential pressure to cabin altitude.

IIIIIIIII

-33-01 Cabin Outflow Valve(Unpressurized)

C 2 0 (M) May be inoperative provided:a) Affected cabin outflow valve is

removed, andb) Cabin pressurization system is

considered inoperative.

IIII

-33-02 Flow Control Valve C 2 1 (O) One may be inoperative provided:a) Pressurization controller auto

schedule mode is operative,b) Cabin pressurization air source is

selected to operative source, andc) Aircraft is operated at FL 250 or

below.

IIII




PAGE NO.21-3




21 AIR CONDITIONING

-33-03 Pressure Regulating Shutoff Valve(Failed Closed)

C 2 1 (O) One may be inoperative provided:a) Affected pressure regulated

shutoff valve is verified closed,b) Pressurization controller auto

schedule mode is operative,c) Cabin pressurization air source is

selected to operative source, andd) Aircraft is operated at FL 250 or

below.

IIIII

-33-04 Cabin Dump Function(Unpressurized)

C 1 0 (M) May be inoperative provided:a) One cabin outflow valve is

removed, andb) Cabin pressurization system is

considered inoperative.

IIIII

-50-01 Air Conditioning System C 1 0 (M) May be inoperative provided:a) Air conditioning system is

deactivated,b) Cabin and cockpit temperature

control system is operative, c) All glareshield fans are operative,

andd) Aircraft is restricted to

temperature limitation in accordance with AFM.

I

IIIIII

-60-01 Cabin and Cockpit Temperature Control System

C 2 1 May be inoperative provided:a) Crew determines that cockpit and

cabin temperature are satisfactory, and

b) DUCT O’HEAT amber message is monitored.

I

II




PAGE NO.22-1




22 AUTO FLIGHT

-00-01 Autopilot B 1 0 (M) May be inoperative provided:a) Autopilot is deactivated,b) Aircraft is not operated single

pilot, c) Enroute operations do not require

its use,d) Approach minimums do not

require its use, ande) Aircraft is not operated RVSM.

IIIIIIIII

-10-01 Yaw Damper C 1 0 (M) May be inoperative provided:a) Yaw damper is deactivated, b) Autopilot is considered

inoperative, andc) Aircraft is operated at FL 300 or

below.

IIIIII

-10-02 Go-Around Button-01 C 2 1 I-02 C 2 0 May be inoperative provided:

a) Flight director is not used for takeoff or during go-around, and

b) Autopilot is disconnected for go-around.

IIIII

NOTE: FMS missed approach procedure must be activated manually.

II

-10-03 Autopilot/Trim Disconnect (Red Yoke AP TRIM DISC Button)(Fails to disconnect) I

-01 C 2 1 Right side may be inoperative for single pilot operations.

II

-02 C 2 0 May be inoperative provided electric elevator trim is considered inoperative.

II

-10-04 Autopilot/Flight Director Sync(CWS Button)

C 2 0 III




PAGE NO.23-1




23 COMMUNICATIONS

-00-01***

Flight Phone System D - 0 II

-01 Handset D - 0 May be inoperative provided procedures do not require its use.

II

-02 Antenna system D - 0 May be inoperative provided procedures do not require its use.

II

-10-01***

High Frequency (HF) Communications System

D - - Any in excess of those required by 14 CFR may be inoperative.

II

-01 Wire Antenna C - 0 (M) May be inoperative provided:a) Horizontal and vertical stabilizers

are inspected for damage,b) Any remaining portion of wire

antenna is removed, andc) High Frequency (HF)

communication system is considered inoperative.

IIIIIIII

-12-01 Communication Systems (VHF)

C - - May be inoperative provided:a) Affected system is not on

emergency bus,b) System is not required by 14 CFR,

andc) Procedures do not require its use.

IIIIII

-20-01 Datalink (Including Satellite Radio and Weather)

II

-01 D - 0 May be inoperative provided procedures do not require its use.

II

NOTE: Any function(s) that operate normally may be used.

II

-02 C - 0 (O) May be inoperative provided alternate procedures are established and used.

II

-30-01***

Auxiliary Audio Input System

C 1 0 II

-30-02***

XM Radio Wireless Remote System

C 1 0 II

-40-01***

Passenger Address (PA) System (Aircraft with cabin headset jacks only)

-01 B - 0 (O) May be inoperative provided alternate normal, abnormal, and emergency procedures, and/or operating restrictions are established and used.

IIII




PAGE NO.23-2




23 COMMUNICATIONS

-02 D - 0 May be inoperative provided system is not required by 14 CFR.

II

-50-01 Flight Deck Headset Earphone/Headphone and Boom Microphone

III

-01 HeadsetBoom Microphone

-10 A - 0 May be inoperative provided:a) Hand microphone is installed and

operates normally,b) Repairs are made within three

flight days, andc) Aircraft is not operated single

pilot.

IIIIIII

-20 D - - Any in excess of those required by 14 CFR may be inoperative.

II

-02 Headset Earphones/Headphone

-10 C - 1 May be inoperative provided associated cockpit speaker operates normally.

II

-20 D - - Any in excess of those required by 14 CFR may be inoperative.

II

-03***

Active Noise Canceling/Reduction Function

D - 0 May be inoperative provided normal audio function of headset is operative.

III

-04 Headset Audio System C - - May be inoperative provided associated cockpit speaker is operative and used.

II

-50-02 Hand Microphone C 1 0 May be inoperative provided an operative headset boom microphone(s) is available.

II

-50-03 Hand Microphone Jack C 1 0 May be inoperative provided an operative headset boom microphone(s) is available.

II

-50-04 Hand Microphone Holder C 1 0 (O) May be inoperative provided hand Microphone is secured by alternate means.

III

-50-05 Audio Control Panel

-01 INTR COM Button D 2 0 May be inoperative for single pilot operations.

II

-02 PLAY Button D 2 0 I




PAGE NO.23-3




23 COMMUNICATIONS

-03 COM1, COM2, COM3 MIC Annunciator

C 6 0 May be inoperative provided crew refers to PFD frequency boxes for active transmit frequency (shown in green).

III

-04 MKR/MUTE Button C 2 0 May be inoperative provided:a) Approach procedures do not

require its use, andb) System is not required by 14 CFR.

IIII

-05 HI SENS Button (Marker Beacon Hi Sensitivity)

C 2 0 May be inoperative provided approach procedures do not require its use.

II

-06 DME Button C 2 0 May be inoperative provided procedures do not require its use.

II

-07 NAV1, NAV2 Button C 4 0 May be inoperative provided procedures do not require its use.

II

-50-06 Cockpit Speaker C 2 1 One may be inoperative provided: a) Affected speaker is not required

for procedures, andb) A headset is used for associated

inoperative speaker including during emergency procedures.

IIIIII

-60-01 Static Wick I-01 Aileron

(Each side)C 2 1 One may be damaged or missing

provided outermost wick is installed and not damaged.

III

-02 Wing Tip Assembly(Each side)

- 1 1 ||

-03 Elevator(Each side)

C 3 1 Two may be damaged or missing provided outermost wick is installed and not damaged.

I||

-04 Vertical Stabilizer - 1 1 |-05 Rudder C 2 1 One may be damaged or missing

provided uppermost wick is installed and not damaged.

I||

-06 Stinger - 1 1 |-70-01

***Cockpit Voice Recorder I

I-01 With Flight Data Recorder

InstalledA - 0 May be inoperative provided:

a) Flight data recorder operates normally, and

b) Repairs are made within three flight days.

IIIII




PAGE NO.23-4




23 COMMUNICATIONS

-02 For an Operator other than a Holder of an Air Carrier or Commercial Operator Certificate

A - 0 May be inoperative provided repairs are made in accordance with 14 CFR.

IIII

-03 Independent Power Source C - 0 I




PAGE NO.24-1




24 ELECTRICAL POWER

-31-01***

Battery Temperature Indication (Aircraft equipped with Lead-Acid Battery)

C 1 0 III

-37-01 DC Generator Current Display (AMPS)(EICAS Indication)

B 2 1 One may be inoperative provided GEN OFF L-R amber message is monitored.

II|

-40-01 External Power System C 1 0 I-60-01 Cockpit 12V Outlet

-01 C - 0 (O) May be inoperative provided alternate procedures are established and used.

II


II

-60-02 Interior Disconnect-01 C 1 0 (M) (O) May be inoperative provided:

a) Interior power system is deactivated,

b) Passengers are briefed on disabled cabin electrical systems, and

c) Cabin interior lighting, cockpit/cabin 12V outlets, and cabin audio are considered inoperative.

IIIIIIIII

-02 C 1 0 (M) May be inoperative provided:a) Interior power system is

deactivated, b) Passengers are not carried, andc) Cabin interior lighting,

cockpit/cabin 12V outlets, and cabin audio are considered inoperative.

IIIIIIII




PAGE NO.25-1




25 EQUIPMENT/FURNISHINGS

-00-01 Document Holder(Airworthiness Certificate, Registration, Etc.)

D 1 0 (O) May be missing or inoperative provided an alternate means of securing and displaying required documents is used.

IIII

-10-01 Flight Crew Seat(per seat)

II

-01 Armrest-10 C 1 0 May be inoperative provided affected

armrest is stowed in retracted position.II

-20 C 1 0 (M) May be inoperative provided affected armrest is removed.

II

-02***

Lumbar Support C 1 0 II

-03 Recline/Tilt Function C 1 0 (O) May be inoperative provided:a) Affected seat is failed in a position

that permits normal visibility,b) Full flight control movement is

available, andc) Crewmember can reach all

necessary controls and equipment while restrained.

IIIIIIII

-04***

Restraint Buckle Protective Padding

C - 0 II

-05 Vertical Adjustment C 1 0 (O) May be inoperative provided:a) Affected seat is failed in a position

that permits normal visibility,b) Full flight control movement is

available, andc) Crewmember can reach all

necessary controls and equipment while restrained.

IIIIIIII

-06 Copilot Seat Belt/Shoulder Harness

C 1 0 May be inoperative provided seat remains unoccupied.

II

-10-02 Cockpit Sun Visor System and/or Attachment Mechanism

C 2 0 May be missing or inoperative provided pilot’s field of vision is not obstructed.

III

-10-03 Cockpit Assist Handle D 1 0 I-10-04 Yoke Mounted Chart Holder C 2 0 I-10-05 Emergency Gear Handle

CoverC 1 0 May be missing or inoperative provided

cover is removed. II




PAGE NO.25-2





-20-01 Passenger Seat C - - May be inoperative provided:a) Seat does not block an

emergency exit,b) Seat does not restrict any cabin

occupant access to main aircraft aisle,

c) Affected seat(s) are blocked and placarded “DO NOT OCCUPY”, and

d) A seat with an inoperative seat belt or shoulder harness is considered inoperative.

I

II

III

NOTE: Affected seat(s) may include seats near inoperative seat(s).

-01 Armrest D - - (M) May be inoperative or missing and seat occupied provided:

a) Armrest does not block an emergency exit,

b) Armrest does not restrict any passenger from access to aisle, and

c) If armrest is missing, reclining seat is secured in full upright position.

IIIIIIIIII

-02 Headrest-10 C - - May be inoperative and seat occupied

provided headrest is failed in placarded taxi, takeoff and landing position.

III

-20 D - - May be missing or inoperative in other than placarded taxi, takeoff, and landing position provided affected seat is considered inoperative.

IIII

-03 Recline Mechanism-10 C - - May be inoperative and seat occupied

provided seat back is immovable in the full upright position.

I

-20 D - - (M) May be inoperative and seat occupied provided seat is secured in full upright position.

III

(Continued)




PAGE NO.25-3





-20-01 Passenger Seat(Continued)

-04 Seat Belt/Shoulder Harness D - - May be inoperative provided affected seat is blocked and placarded "DO NOT OCCUPY".

III

-05 Seat Belt/Shoulder Harness Keeper

D - - II

-06 Lumbar Support D - - I-20-02

***Folding Cabin Seat C 1 0 May be inoperative provided:

a) Seat does not block an emergency exit,

b) Seat does not restrict any cabin occupant access to main aircraft aisle,

c) Affected seat(s) are blocked and placarded “DO NOT OCCUPY”, and

d) A seat with an inoperative seat belt or shoulder harness is considered inoperative.

IIIIIIIIIIII

NOTE: Affected seat(s) may include seats near inoperative seat(s).

II

-20-03 Cabin Curtain C 2 0 May be missing or inoperative provided curtain remains secured open.

II

-20-04 Non-Essential Equipment & Furnishings (NEF)

- - 0 May be inoperative, damaged or missing provided that the item(s) is deferred in accordance with the NEF deferral program. The NEF program, procedures and processes are outlined in the operator’s (insert name) Manual. (M) and (O) procedures, if required, must be available to the flight crew and included in the operator’s appropriate document.

NOTE: Exterior lavatory door ash trays are not NEF items.

IIIIIIIIIIII

-30-01 Cabin Storage Compartment




PAGE NO.25-4





-01 C - - (M) May be inoperative provided:a) Compartment does not contain

any aircraft system protection devices,

b) Any emergency equipment located in affected compartment is considered inoperative,

c) Affected compartment is not used for storage of any item except for those permanently affixed,

d) Procedures are established and used to secure compartment closed, and

e) Affected compartment is prominently placarded “DO NOT USE”.

IIIIIIIIIIIIIIII

-02 C - - (M) (O) May be inoperative provided:a) Affected door is removed,b) Affected compartment is not used

for storage of any item, except those permanently affixed,

c) Cabin occupants are briefed that affected compartment may not be used,

d) Affected compartment is prominently placarded “DO NOT USE”, and

e) Any permanently affixed emergency equipment located in affected compartment is available for use.

IIIIIIIIIIIIIII

-03 Shelving D - - May be inoperative provided any permanently affixed emergency equipment located on affected shelving is relocated and available for use.

IIII

-30-02***

Storage CompartmentKey Lock

D - 0 May be inoperative in unlocked position. II

-40-01***

Ashtray A - 1 May be inoperative or missing provided it is replaced within three calendar days.

II

50-01 Cargo Restraint System C - - May be inoperative or missing provided cargo compartment remains empty.




PAGE NO.25-5





-60-01***

Emergency Medical Equipment

II

-01 Automatic External Defibrillator and/or Associated Equipment

D - 0 III

-02 Emergency Medical Kit (EMK) and/or Associated Equipment

D - 0 I

-03 First Aid Kit (FAK) and/or Associated Equipment

D - - Any in excess of those required by 14 CFR may be incomplete, missing, or inoperative.

III

-61-01***

Life Preservers(Crew And Passenger)

D - 0 Any in excess of those required by 14 CFR may be inoperative or missing.

II

-62-01***

Emergency Locator Transmitter(ELT)

I

-01 Survival Type ELT D - - Any in excess of those required by 14 CFR may be inoperative or missing.

II

-02 Fixed ELT-10 A - 0 (M) May be inoperative provided:

a) System is deactivated, andb) Repairs are made within 90 days.

III

-20 A - 0 May be missing provided repairs are made within 90 days.

II

-30 D - - (M) Any in excess of those required by 14 CFR may be inoperative provided system is deactivated.

III

-40 D - - Any in excess of those required by 14 CFR may be missing.

II

-64-01***

Life Raft D - - Any in excess of those required by 14 CFR may be inoperative or missing.

II




PAGE NO.26-1




26 FIRE PROTECTION

-22-01 Portable Fire Extinguisher D - 1 (O) Any in excess of those required by 14 CFR may be inoperative or missing provided:

a) Inoperative portable fire extinguisher is tagged inoperative, removed from installed location and stored out of sight so it cannot be mistaken for a functional unit,

b) Required distribution is maintained, and

c) At least one operable portable fire extinguisher must be located in cockpit.

II

III




PAGE NO.27-1




27 FLIGHT CONTROLS

31-01 Electric Elevator Trim C 1 0 (M) May be inoperative provided: a) Electric trim system is

deactivated, b) Manual trim is operative and

unaffected, andc) Autopilot is considered

inoperative. II

-60-01 Speed Brake Actuation System(Failed in retracted position)

B 1 0 (M) (O) May be inoperative provided:a) Speed brakes are deactivate,b) Steep approaches are not

performed, andc) Operations are limited to VMO of

240 KIAS.

I

I

-60-02 Speed Brake Position B 1 0 May be inoperative provided speed brake actuation system is considered inoperative.

III

-60-03 Speed Brake Switch C 2 1 I-70-01 Aileron/Elevator Control

Lock(Failed Unlocked)

C 1 0 (O) May be inoperative in unlocked position provided full flight control is available.

III

-70-02 Rudder Lock(Failed Unlocked)

C 1 0 (O) May be inoperative in unlocked position provided full flight control is available.

III




PAGE NO.28-1




28 FUEL

-10-01 Over-wing Refueling Cap Lock

D 2 0 May be inoperative in unlocked position. II

-41-01 Fuel Low Level Indicating System

A 2 1 (O) One may be inoperative provided:a) Procedures for monitoring fuel

quantity are established and used, and

b) Repairs are made within three flight days.

IIIIII




PAGE NO.30-1




30 ICE AND RAIN PROTECTION

-10-01 Wing De-Ice Boot System(Failure to inflate)

C 1 0 (M) May be inoperative provided:a) All de-ice boots must be visually

verified to be deflated and held down when service air system is active, and

b) Aircraft is not operated in known, forecast, or AFM-defined icing conditions.

IIIIIIII

-10-02 Tail De-Ice Boot System(Failure to inflate)

C 1 0 (M) May be inoperative provided:a) All de-ice boots must be visually

verified to be deflated and held down when service air system is active, and


IIIIIIII

-20-01 Engine Anti-Ice System I-01 Failed On

(Flow)C 2 1 One may be inoperative provided:

a) Both ENGINE ANTI-ICE switches are selected ON,

b) Takeoff and landing performance calculations for anti-ice on are used, and

c) Aircraft are restricted to temperature limitation in accordance with AFM.

IIIIIIIII

-02 Failed Off(No Flow)

C 2 0 (M) May be inoperative provided:a) Affected engine anti-Ice is

secured for no flow, andb) Aircraft is not operated in known,

forecast, or AFM-defined icing conditions.

IIIIII

-30-01 Copilot Pitot Heater System B 1 0 May be inoperative provided:a) Aircraft is not operated in

Instrument Meteorological Conditions (IMC), and


IIIIIII




PAGE NO.30-2




30 ICE AND RAIN PROTECTION

-30-02 Copilot Static Port Heater B 2 1 One may be inoperative provided:a) Aircraft is not operated in

Instrument Meteorological Conditions (IMC),

b) Aircraft is not operated in known, forecast, or AFM-defined icing conditions, and

c) Aircraft is not operated RVSM.

IIIIIII

-30-03 Stall Warning Vane Heater C 1 0 May be inoperative provided aircraft is not operated in known, forecast, or AFM-defined icing conditions.

III

-40-01 Windshield Anti-Ice System C 2 0 (O) May be inoperative provided:a) Aircraft is not operated in known,

forecast, or AFM-defined icing conditions, and

b) Crew has a means to clear windshield of moisture.

IIII

-40-02 Windshield Rain Repellant C 1 0 May be missing provided aircraft is not operated in precipitation within five nautical miles of airport used for takeoff or intended landing.

IIII

-70-01 Air Conditioner Forward Evaporator Drain Heater

C 1 0 May be inoperative provided air conditioning system is considered inoperative.

III




PAGE NO.31-1




31 INDICATING/RECORDING SYSTEMS

-20-01 Flight Hour Meter C 1 0 (O) May be inoperative provided flight time is tracked by alternate means.

II

-30-01***

Flight Data Recorder (FDR) System

-01 (For a Holder of an Air Carrier or Commercial Operator Certificate)

A - 0 May be inoperative provided:a) Cockpit Voice Recorder (CVR)

operates normally,b) Airplane is not dispatched from a

designated airport as listed in operator’s MEL unless:

1. FDR failure occurs after dispatch but prior to takeoff, or

2. FDR repair was attempted but was not successful.

c) In those cases where repair is attempted but not successful, aircraft may be dispatched on a flight or series of flights until next designated airport where repair must be accomplished prior to dispatch, and

d) Repairs are made within three flight days.

IIIIIIIIIIIIIIIIIII

-10 FDR Recording Parameters Required by 14 CFR

A - - Up to three (3) recording parameters may be inoperative provided:

a) Cockpit Voice Recorder (CVR) operates normally, and

b) Repairs are made within 20 calendar days.

IIIIII

-20 FDR Recording Parameters Not Required by 14 CFR

A - - May be inoperative provided repairs are made prior to completion of next scheduled inspection/check of system.

III

-02 (For an Operator other than a Holder of an Air Carrier or Commercial Operator Certificate)

A - 0 May be inoperative provided repairs are made in accordance with applicable 14 CFR.

IIII

-30-02***

Quick Access Recorder C 1 0 II

-40-01***

Electronic Checklist D 1 0 May be inoperative provided equivalent checklist is used.

II




PAGE NO.31-2




31 INDICATING/RECORDING SYSTEMS

-40-02 Fuel Totalizer C 1 0 May be inoperative provided: a) Fuel quantity indicating system is

operative, andb) MFD map range rings and weight

planning functions are considered inoperative.

IIIIII

-50-01 Master Warning System I-01 Master Warning Reset

AnnunciatorB 2 1 Pilot side must be operative for single

pilot operations.II

-02 Master Warning Cancel/Reset Function

C 2 1 Pilot side must be operative for single pilot operations.

II

-03 Master Caution Reset Annunciator


II

-04 Master Caution Cancel/Reset Function


II

-50-02 Cabin Altitude Warning System

C 1 0 May be inoperative provided:a) Cabin altitude warning is not

displayed, andb) Aircraft is operated at 9,500 feet

MSL or below.

IIIII




PAGE NO.32-1




32 LANDING GEAR

-41-01 Antiskid System C 1 0 (O) May be inoperative provided:a) Aircraft is operated in accordance

with AFM DISPATCH WITH ANTISKID SYSTEM INOPERATIVE abnormal procedure, and

b) Steep approaches are not conducted.

IIIIIIII

NOTE: ANTISKID FAIL amber message will appear.

II

-41-02 Tire Spin Down System C 1 0 (O) May be inoperative provided aircraft is operated in accordance with AFM NO TIRE SPINDOWN white CAS message procedure is followed.

IIII




PAGE NO.33-1




33 LIGHTS

-10-01 Cockpit and Instrument Lighting System(Excluding Internally Lighted Annunciators and Buttons, Standby Flight Instrument Lighting, and STDBY ALT/AS Placard Lighting)

C - - Individual lights may be inoperative provided remaining lights are:

a) Sufficient to clearly illuminate all required instruments, controls, and other devices for which it is provided,

b) Positioned so that direct rays are shielded from crew members eyes,

c) Lighting configuration and intensity is acceptable to crew, and

d) Cockpit flood light is operative.

IIIIIII

I-10-02 Cockpit Flood Light C 1 0 May be inoperative provided aircraft is not

operated at night.II

-10-03 Windshield Ice Detection Light

-01 C 2 0 May be inoperative provided aircraft is not operated at night.

II

-02 C 2 1 Right side may be inoperative for single pilot operations.

II

-03 C 2 1 (O) One may be inoperative for two pilot operations provided alternate procedures are established and used.

III

-10-04 Cockpit Map Light-01 C 2 1 One may be inoperative provided cockpit

flood light is operative. II

-02 C 2 0 May be inoperative provided cockpit flood light is operative and a flashlight is available to crew.

III

-10-05 G1000 Display Dimmer (DISPLAYS knob)

C 1 0 (O) May be inoperative providing display brightness is adjusted through G1000 menu in manual mode.

III

-20-01 Lighted Passenger Information Sign(Excluding Cabin Exit Signs)




PAGE NO.33-2




33 LIGHTS

-01 C - 0 (O) May be inoperative provided:a) Alternate procedures are

established and used to alert cabin occupants when PAX SAFETY/SEAT BELT is selected, and

b) Scheduled operations are not conducted.

IIIIIIII

-02 C - 0 May be inoperative provided no cabin occupants are carried.

II

-20-02 Cabin Interior Lighting System (Excluding Emergency Lighting)

C - - (O) Individual lights may be inoperative provided cabin emergency lighting is verified operative.

III

-30-01 Aft Baggage Light C 1 0 I

-01 Door Proximity Switch C 1 0 (O) May be inoperative providing crew makes sure light is selected OFF using toggle switch.

III

-30-02 Nose Baggage Compartment Light

C 1 0

-01 Door Proximity Switch-10 C 2 0 (O) May be inoperative providing crew

makes sure light is selected OFF using rocker switch on light.

III

-20 C 2 1 I-40-01 Anti-Collision Light System

(Wing Strobes) (ANTI COLL)

A 1 0 May be inoperative provided:a) All position (NAV) lights are

operative,b) Ground recognition (BEACON)

light is operative, andc) Repairs are made within three

flight days.

III

-40-02 Position Light System(NAV)

C 1 0 May be inoperative provided system is not required by 14 CFR.

II

-40-03 Wing Inspection Light (WING INSP)

C 1 0 May be inoperative provided: a) Aircraft is not operated at night,

andb) Ground deicing procedures do not

require its use.

IIIII




PAGE NO.33-3




33 LIGHTS

-40-04 Landing/Taxi/Recognition Light (LANDING - RECOG TAXI)

C 2 0 Any in excess of those required by 14 CFR may be inoperative.

III

-40-05 Ground Recognition Light (BEACON)

C 1 0 May be inoperative provided anti-collision light system is operative. I

-50-01***

Cockpit Flashlight and Holder Assembly

II

-01 Flashlight D - - Any in excess of those required by 14 CFR may be inoperative or missing.

II

-02 Holder Assembly C - - May be inoperative provided associated flashlight is stowed by alternate means.

II




PAGE NO.34-1




34 NAVIGATION

-23-01 Non-Stabilized Magnetic Compass

-01 B 1 0 (O) May be inoperative provided:a) Both AHRS heading information

sources are operative,b) Aircraft is operated with dual

independent navigation capability, c) Flight is conducted under positive

radar control by ATC during en route portion of flight, and

d) MFD nav range ring is selected ON and reference to magnetic north.

-02 B 1 0 May be inoperative provided:a) Both AHRS heading information

sources are operative, andb) Aircraft is not operated at night or

in IFR conditions.II

-25-01 MFD Remote Mounted Control Panel

B 1 0 (O) May be inoperative provided:a) Weather radar is considered

inoperative,b) Datalink is considered inoperative, c) Electronic chart is considered

inoperative,d) Procedures do not require use of

MFD,e) Aircraft is operated in Visual

Meteorological Conditions (VMC), f) Aircraft is not operated at night,g) PFD Inset maps are used, andh) Alternate procedures are

established and used.NOTE: MFD navigation is disabled.

-01 Individual buttons(CRSR, ,D>, MENU, FPL, PROC, BACK, SPC, CLR, SEL, <, >, A-Z, 1-0, +/-, and period)(Except ENT, Range/PUSH PAN, and FMS Knobs/PUSH CRSR)

C - 0 NOTE: Corresponding buttons/knobs on PFD must be operative for relief, if applicable.

IIIIIIII

25-02 Mode Control Panel I




PAGE NO.34-2




34 NAVIGATION

-01 Yaw Damper Button(YD)

C 1 0 NOTE 1: Yaw damper may be engaged by engaging autopilot.

II

NOTE 2: Yaw damper may be disengaged by pushing AP TRIM DISC button.

III

-02 Course Knob Push Direct Function(CRS1 or CRS2 PUSH DIR)

C 2 0 III

-03 Bank Button(BANK)

C 1 0 II

-04 HDG Knob PUSH SYNC Function

C 1 0 II

-05 Vertical Mode Button(FLC, ALT, VNV, VS)

II

-10 C 4 3 I-20 B 4 0 May be inoperative provided:

a) Flight director is considered inoperative, and

b) Autopilot is considered inoperative.

IIIII

-06 Speed Button (SPD) C 1 0 I-07 Lateral Mode Buttons (NAV,

HDG, APR, BC) B 4 0 May be inoperative provided:

a) Flight director is considered inoperative, and

b) Autopilot is considered inoperative.

IIIII

-08 Annunciator LEDs and XFR Arrows

D 13 0 NOTE: PFDs are primary source for armed and active mode indications.

II

-09 XFR Button B 1 0 May be inoperative provided:a) FD Indicator Arrow is pointing to

LH side if operated single pilot, orb) Pilot flying must be seated in side

FD Indicator Arrow is pointing to if operated dual pilot.

IIIIII

-25-03***

Synthetic Vision C 1 0 May be inoperative provided procedures do not require its use.

II

-25-04 Moving Map Display C 3 0 May be inoperative provided procedures do not require its use.

II

-25-05 Primary Flight Display (PFD) I-01 Copilot’s BARO Knob and

PUSH STD FunctionC 1 0 May be inoperative for single pilot

operations. II




PAGE NO.34-3




34 NAVIGATION

-02 RANGE/PAN Knob/Joystick C 2 0 May be inoperative provided procedures do not require its use.

II

-03 D>, FPL, PROC Button C 6 0 May be inoperative provided corresponding button(s) on MFD remote mounted control panel are operative.

III

-04 Copilot’s Comm Swap Button (Hold for EMERG)

C 1 0 May be inoperative for single pilot operations.

II

-31-01 Navigation System (VHF)-01 VOR C - - May be inoperative provided:

a) Affected system is not on the emergency bus,

b) Procedures do not require its use, and

c) System is not required by 14 CFR.-02 Localizer C - - May be inoperative provided:


b) Procedures do not require its use,c) System is not required by 14 CFR,

andd) Associated glideslope is

considered inoperative.-03 Glideslope C - - May be inoperative provided:


b) Approach procedures do not require its use, and

c) System is not required by 14 CFR.

IIIIII

-34-01 Marker Beacon Receiver System

C 1 0 May be inoperative provided:a) Approach procedures do not

require its use, andb) System is not required by 14 CFR. I

-42-01 Weather Radar System C 1 0 May be inoperative provided system is not required by 14 CFR.

II




PAGE NO.34-4




34 NAVIGATION

-43-01 Altitude Alerting System A 1 0 (O) May be inoperative provided:a) Altitude pre-select function is

operative,b) Aircraft is not operated RVSM,c) Aircraft does not depart from a

designated airport (as listed in operator’s MEL) where repair or replacement can be made,

d) Autopilot with altitude hold and capture operates normally, and

e) Repairs are made within three flight days.

IIIIIII

I

-44-01***

Radar Altimeter System A 1 0 May be inoperative provided:a) Approach minimums or operating

procedures do not require its use,b) TCAS II, if installed, is considered

inoperative, andc) Repairs are made within two flight

days.

IIIIIII

-44-02 Terrain Awareness And Warning System (TAWS) – Class B

II

-01 C 1 0 May be inoperative provided system is not required by 14 CFR.

II

-02 C 1 0 (O) May be inoperative provided alternate procedures are established and used. NOTE: Any mode that operates normally

may be used. -03 Forward Looking Terrain

Avoidance ModeB 1 0 I

I-04 Premature Descent Alert

ModeB 1 0 I

I-05 Advisory Callouts I

-10 B - 0 (O) May be inoperative provided alternate procedures are established and used.

II

-20 C - 0 (O) May be inoperative provided:a) Advisory callout not required by

14 CFR, andb) Alternate procedures are

established and used.

IIIII

(Continued)




PAGE NO.34-5




34 NAVIGATION

-44-02 Terrain Awareness And Warning System (TAWS) – Class B(Continued)

-06 Excessive Descent Rate Mode

A 1 0 (O) May be inoperative provided:a) Alternate procedures are

established and used, andb) Repairs are made within two flight

days.

IIIII

-07 Negative Climb Rate or Altitude Loss After Takeoff Mode

A 1 0 (O) May be inoperative provided:c) Alternate procedures are

established and used, andd) Repairs are made within two flight

days.

IIIII

-45-01 Traffic Alert and Collision Avoidance System (TCAS)

II

-01***

TCAS II II

-10 Combined Traffic Alert (TA) and Resolution Advisory (RA) Dual Display System

C - 1 May be inoperative on the pilot not flying side provided:

a) TA and RA visual display is operative on the pilot flying side, and

b) TA and RA audio function is operative on pilot flying side.

IIIIIII

-20 Audio Function B - 0 May be inoperative provided procedures do not require use of TCAS II.

II

-30 Airspace Selection Function C - 0 I-02***

Traffic Alert System (TAS) C - 0 May be inoperative provided en route or approach procedures do not require use of TAS.

III

-45-02 Traffic Information System (TIS)

C 1 0 II

-45-03***

Traffic Collision Avoidance Device (TCAD)

C 1 0 II

-51-01 Distance Measuring Equipment System (DME)


II

-52-01 ATC Transponders and Automatic Altitude Reporting System




PAGE NO.34-6




34 NAVIGATION

-01 D - 1 Any in excess of those required by 14 CFR may be inoperative.

II

-02 B 2 0 May be inoperative provided:a) Operations do not require its use, b) Prior to flight, approval is obtained

from ATC facilities having jurisdiction over planned route of flight,

c) Aircraft is not operated RVSM, and

d) Traffic Alert and Collision Avoidance System (TCAS II) is considered inoperative.

I

IIII

-03 Elementary and Enhanced Downlink Aircraft Reportable Parameters Not Required By 14 CFR

A 2 0 May be inoperative provided:a) Operations do not require its use,

andb) Repairs are made prior to

completion of next scheduled inspection/check of system.

IIIIII

-04***

ADS-B Squitter Transmissions

A - 0 May be inoperative provided:a) Operations do not require its use,

andb) Repairs are made prior to

completion of next scheduled inspection/check of system.

IIIIII

-52-02 Automatic Dependent Surveillance-Broadcast (ADS-B) System

D - 0 May be inoperative provided system is not required by 14 CFR.

III

NOTE: If ADS-B is installed in lieu of or as a replacement for 14 CFR required equipment, repair category in operator’s MEL will be the same as that of 14 CFR required equipment.

IIIIII

-01 Cockpit Display and Traffic Information (CDTI)

D - 0 NOTE: CDTI display of data from other aircraft systems may be used.

II

(Continued)-52-02 Automatic Dependent

Surveillance-Broadcast (ADS-B) System(Continued)




PAGE NO.34-7




34 NAVIGATION

-02 CDTI Control Panel D - 0 May be inoperative provided:a) Flight ID can be set, andb) Screen display is acceptable to

flight crew.

IIII

-03 Data Link Transmitter D - 0 NOTE: In some aircraft, data link transmission is an integral part of the transponder and relief is provided in that section.

IIII

-04 Data Link Receiver D - 0 I-05 ADS-B Application D - 0 I

-55-01***

Automatic Direction Finding System (ADF)


II

-57-01 Navigation Equipment (GPS, FMS)

C - - Any in excess of those required by 14 CFR may be inoperative.

II

-60-01 Flight Management System(FMS) Navigation Database

A - - May be expired provided aircraft is operated in accordance with applicable AFM limitations.

III

-60-02 Data Loader (SD Card Slot) C - - NOTE: Certain card slots are used for real-time data access. If inoperative, the associated features are considered inoperative.

IIIII




PAGE NO.35-1




35 OXYGEN

-00-01 Oxygen Tank Fill Port C 1 0 (M) May be inoperative provided bottle is filled using alternate means when service is required.

III

-00-02 Plastic Blowout Disc/Green Label

C 1 0 (O) May be missing or damaged provided oxygen pressure is verified prior to each flight.

III

-20-01 Passenger Oxygen System C 1 0 May be inoperative provided:a) No cabin occupants are carried,

andb) Crew oxygen system is operative.

I

I-01 Cabin Mask C 5 0 Individual oxygen masks or dispensers

may be inoperative or missing provided associated seats are placarded “DO NOT OCCUPY”.

IIII

-02 Drop Out Panel C 5 0 (M) Individual panels may be out of normal position provided:

a) Oxygen masks and drop out panel are removed, and

b) Associated seats are placarded “DO NOT OCCUPY”.

IIIIII

-30-01***

Protective Breathing Equipment (PBE)

D - - Any in excess of those required by CFR may be inoperative or removed provided location placarding is removed or obscured.

IIII

-30-02***

Portable Oxygen Bottles C - - Any in excess of those required by 14 CFR may be inoperative provided:

a) Required distribution of serviceable bottles is maintained throughout the aircraft, and

b) Bottles not properly serviced are replaced, serviced or removed at next available maintenance facility.

IIIIIIIII




PAGE NO.38-1




38 WATER/WASTE

-30-01 Lavatory C 1 0 (O) Individual components may be inoperative provided:

a) Cabin occupants are briefed prior to each flight that toilet is inoperative and unusable, and

b) Lavatory is placarded "DO NOT USE TOILET".

IIIIIII




PAGE NO.45-1




45 CENTRAL MAINTENANCE SYSTEM (CMS)

-00-01 Citation Diagnostics and Maintenance System (CDMS)

C 1 0 May be inoperative provided procedures do not require its use.

III




PAGE NO.46-1




46 INFORMATION SYSTEMS

-00-01***

Electronic Flight Bag (EFB) System

II

-01 Class 3 EFB I-10 D - 0 May be inoperative provided procedures

do not require its use.II

-20 C - - (O) May be inoperative provided alternate procedures are established and used.

II

NOTE: Any function, program or document which operates normally may be used.

III

-02 Data Connectivity(Class 2)

II

-10 D - - May be inoperative provided procedures do not require its use.

II


II

-03 Power Connection(Class 1 & 2)

II


II


II

-04 Mounting Device(Class 2)

-10 D - 0 (M) May be inoperative provided:a) Associated EFB and hardware is

secured by an alternate means or removed from aircraft, and

b) Procedures do not require its use.

IIIII

-20 C - 0 (M) (O) May be inoperative provided:a) Associated EFB and hardware is

secured by an alternate means or removed from aircraft, and

b) Alternate procedures are established and used.

IIIIII




PAGE NO.52-1




52 DOORS

-10-01 Cabin Door I-01 Seal

(Unpressurized)C 1 0 May be inoperative or unserviceable

provided:a) Seal does not interfere with door

operation, andb) Cabin pressurization system is

considered inoperative.II

-02 Key Lock D 1 0 May be inoperative in unlocked position. I-03 Gust Lock B 1 0 (O) May be inoperative provided a

procedure is developed and used to prevent unrestricted movement of cabin door.

IIII

-04 Pull Chain C 1 0 May be inoperative provided damage or missing chain does not interfere with door operation.

III

-05 Step Assembly C 1 0 (M) (O) May be inoperative provided:a) Step support cables are removed, b) Step assembly is removed, and c) Alternate procedures for

entering/exiting aircraft are established and used.

IIIIII

-06 Step Support Cable C 2 0 (M) (O) May be inoperative provided:a) Step support cables are removed, b) Step assembly is removed, and c) Alternate procedures for

entering/exiting aircraft are established and used.

IIIIII

-20-01 Escape Hatch Pin C 1 0 May be missing or inoperative with hatch in unlocked position.

II

-30-01 Baggage Door I-01 Aft Door Key Lock C 1 0 May be inoperative in unlocked position

provided door is verified closed and latched prior to flight.

III

-02 Nose Door Key Lock-10 C 2 0 May be inoperative in unlocked position

provided door is verified closed and latched prior to flight.

III




PAGE NO.52-2




52 DOORS

-20 C 2 1 (O) One may be inoperative in locked position provided:

a) Other side door key lock is not failed in locked position,

b) Alternate procedures are established and used to perform required preflight actions, and

c) All latches are verified secured.

IIIIII

-03 Nose Door Gas Spring C 2 0 (O) May be inoperative or missing provided precautions are taken when opening door(s).

III

-04 Aft Door Gas Spring C 1 0 (O) May be inoperative or missing provided precautions are taken when opening door.

III

-05 Aft Door Seal C 1 0 (O) May be inoperative provided baggage compartment is verified empty prior to each flight.

III

-70-01 Door Monitoring System I-01 Cabin Door C 1 0 (O) May be inoperative provided:

a) Door is verified closed and handle latched,

b) 8 door pin indicators are visible in sight glass locations, and

c) Interior door handle is secure.-02 Aft Door C 1 0 (O) May be inoperative provided door is

verified secure and locked.-03 Nose Door C 2 0 (O) May be inoperative provided door is

verified secure and locked.




PAGE NO.73-1




73 ENGINE FUEL AND CONTROL

-31-01 Fuel Flow Indicating System B 2 1 (O) One may be inoperative provided a) Both fuel quantity indication

systems are operative, andb) Navigation map fuel range rings

and weight planning functions are considered inoperative.

III




PAGE NO.76-1




76 ENGINE CONTROLS

-01-01 Engine Synchronizer System(Failed Off)

C 1 0

I

SECTION TWO

CAS MESSAGE ORIENTED MMEL RELIEF

INTRODUCTION

Two section MMELs are authorized by FAA PL 119. Section Two of two-section MMELs may grant relief for failure indications presented as CAS messages on Engine Indicating and Crew Alerting Systems (EICAS), or Electronic Centralized Aircraft Monitoring (ECAM), rather than the traditional relief (Section One) for failed equipment. New technology self-diagnostic tests eliminate the need for failure isolation procedures by maintenance personnel for many CAS messages. By using (O) procedures, the crew can complete selected system/component deactivation/re-configuration from the cockpit for which the crew has been trained.

Section Two will only contain CAS message relief if the crew can act on the item. CAS message relief must ensure safe operation of aircraft. Flight Operations Evaluation Boards (FOEB) will use the normal FOEB processes for determining which CAS messages go into each section.

TWO-SECTION MMEL GUIDANCE:

Modern technology CAS MMELs shall be divided into two sections.

A. Section One. Items which either require maintenance actions (this may include some CAS messages), or caution/advisory information. Section One will continue to use the existing Line Replaceable Units (LRU)-oriented MMEL format and should address the following type of equipment failures:

1. Failures which are not annunciated to crew; and

2. Failures which are annunciated, but the failure indication by itself is not considered sufficient to determine the aircraft airworthiness status.

B. Section Two. Includes only items where flight members may act on CAS messages. MMEL items where CAS messages can be used to determine the aircraft airworthiness should be formatted as follows:

1. It should have only two columns:

a. Column one should list the failure indications (messages) for which relief is given (if desired, the messages may be listed in alphabetical order with no ATA break down).

b. Column two should include the corresponding MMEL limitations and/or procedures. The format of this column should be in line with the format requirements of the “Remarks or Exceptions” column of the conventional “LRU oriented” MMEL.Note: In many cases, CAS messages will not require maintenance to perform fault analysis. Relief provisos for these CAS items are expected to be more restrictive in content and repair interval, as compared to Section One relief provisos.

2. Section Two CAS message relief items require flight crews to accomplish one or more steps to deactivate/re-configure the affected system prior to flight. The “(O)” indicates the need for these tasks. Tasks include, but are not necessarily limited to the following duties:

a. Procedures accomplished using cockpit (or cabin) system controls.

b. Deactivation of affected systems (by pulling system breaker or use of remote electronic system isolation);

c. Visual confirmation of remote gauge indications, or valve positions as provided by integral external indicators; and

d. Visual inspection behind panels (internal or external).

1) These panels must be accessible without tools via quick-release latches and must clearly indicate their unlocked or unsafe state (red/green safe window; flush fit latches - candidates to be verified at FOEB).

2) The visual inspection of compartments accessed by the panels is within the normal crew duty requirements for which they have been trained; and

3) The crew may use an external ladder for visual inspection behind panels as long as this procedure is within the normal crew duty requirements for which they have been trained. Special equipment such as maintenance stands and hydraulic lifts may not be used by the crew to perform visual inspections.

C. The following statement will be included on page 1 of Section Two in all two-section MMELs:

1. Section Two of the MMEL will list only Crew Alerting system (CAS) messages meeting the following requirements:

a. Equipment failure indications(s) that can be used to determine the airworthiness status of the airplane;

b. Messages that the crew can act upon from the cockpit with simple troubleshooting procedures without the assistance of a mechanic, and for which the crew has been trained.

c. Messages using the new self-diagnostic technology (virtual) actions for which the crew has been trained.

2. CAS message relief items not meeting these requirements will be listed in Section One of the MMEL




PAGE NO.2-1

PFD Messages / Flags Dispatch Consideration

AFCS flag on PFD Aircraft may be dispatched provided autopilot system is considered inoperative.

TAWS FAIL Aircraft may be dispatched provided Terrain Awareness and Warning System (TAWS) is considered inoperative.

*** TCAS FAIL(With TCAS II Installed)

Aircraft may be dispatched provided traffic alert and collision avoidance system is considered inoperative.




PAGE NO.2-2

MFD Messages / Flags Dispatch Consideration

RDR FAIL message on radar page

Aircraft may be dispatched provided weather radar system is considered inoperative.

RDR FAULT message on radar page


STAB INOP message on radar page





PAGE NO.2-3

White PFD Messages Dispatch Consideration

***COM2 SERVICE COM3 SERVICE

Aircraft may be dispatched provided VHF Communication system is considered inoperative.

G/S1 FAIL G/S1 SERVICEG/S2 FAILG/S2 SERVICE

Aircraft may be dispatched provided Glideslope is considered inoperative.

GCU CONFIG GCU FAIL

Aircraft may be dispatched provided MFD remote mounted control panel is considered inoperative.

GDL 69 FAIL Aircraft may be dispatched provided datalink is considered inoperative.

GPS NAV LOST GPS1 FAILGPS1 SERVICEGPS2 FAILGPS2 SERVICE

Aircraft may be dispatched provided GPS is considered inoperative.

GWX CONFIG GWX FAILGWX SERVICE

Aircraft may be dispatched provided Datalink satellite weather is considered inoperative.

NAV2 SERVICE Aircraft may be dispatched provided VHF navigation system is considered inoperative.

XPDR1 CONFIG XPDR1 CTRL FAILXPDR1 FAILXPDR1 SRVCXPDR2 CONFIGXPDR2 CTRL FAILXPDR2 FAILXPDR2 SRVC

Aircraft may be dispatched provided ATC transponder and automatic altitude reporting system is considered inoperative.




PAGE NO.2-4

Amber CAS Messages Dispatch Consideration

AFT DOOR Aircraft may be dispatched provided aft door monitoring system is considered inoperative.

ANTISKID FAIL Aircraft may be dispatched provided antiskid system is considered inoperative.

BATT TEMP FAIL Aircraft may be dispatched provided battery temperature indication is considered inoperative.

CABIN DOOR Aircraft may be dispatched provided cabin door monitoring system is considered inoperative.

CHECK DOORS Aircraft may be dispatched provided cabin door and nose door monitoring systems are considered inoperative.

ENG A/I COLD L-R Aircraft may be dispatched provided engine anti-ice system is considered inoperative.

NOSE DOOR L-R Aircraft may be dispatched provided nose door monitoring system is considered inoperative.

P/S HTR R (in air) Aircraft may be dispatched provided copilot static port or copilot pitot heater system is considered inoperative.

PRESS CTRL Aircraft may be dispatched provided pressurization controller auto schedule mode is considered inoperative.

STALL WARN HTR Aircraft may be dispatched provided stall warning vane heater is considered inoperative.

TAIL DE-ICE FAIL Aircraft may be dispatched provided tail de-ice boot system is considered inoperative.

W/S A/I FAIL L-R Aircraft may be dispatched provided windshield anti-ice system is considered inoperative.

WING DE-ICE FAIL Aircraft may be dispatched provided wing de-ice boot system is considered inoperative.




PAGE NO.2-5

White CAS Messages Dispatch Consideration

*** CVR FAIL Aircraft may be dispatched provided cockpit voice recorder is considered inoperative.

*** FDR FAIL Aircraft may be dispatched provided flight data recorder is considered inoperative.

FUEL LO INOP L-R Aircraft may be dispatched provided fuel low indicating system is considered inoperative.

NO TIRE SPINDOWN Aircraft may be dispatched provided tire spin down system is considered inoperative.

P/S HTR R (on ground, with PITOT STATIC selected)

Aircraft may be dispatched provided copilot static port or copilot pitot heater system is considered inoperative.

mmel ce-510 - t c · web view(flc, alt, vnv, vs) i. i -10 c 4 3 i -20 b 4 0 may be inoperative...

Documents