operational suitability data (osd) flight crew...operational suitability data – flight crew...

HBC Document Reference# BE300-1900ALLOSDFC-01

Signature MARCUS S.VANDERPOOL, Pilot and Maintenance Training, Textron Aviation

Operational Suitability Data (OSD) Flight Crew

Hawker Beechcraft BE300/1900

Models 300, 300LW, B300/B300C, B300 (FF serial with ProLine21) and 1900, 1900C, 1900D

Initial Issue

17 November 2015

Operational Suitability Data – Flight Crew BE300/1900

OSD FC BE300/1900 – Initial Issue of 63

Hawker Beechcraft BE300/1900

Operational Suitability Data (OSD) – Flight Crew

Revision Record Revision No. Content Date

OSD FC Initial Issue Initial evaluation of the BE300/1900 models 17 Nov 2015



Contents

Revision Record ............................................................................................................................. 2

Content ........................................................................................................................................... 3

Acronyms ........................................................................................................................................ 5

Preamble ....................................................................................................................................... 7

1. Introduction ................................................................................................................ 7

2. Operational Evaluation BE 300/1900 models) ............................................................. 7

Operational Suitability Data (OSD) – Flight Crew ............................................................................ 8

1. Aircraft Type Designation and Pilot Licence Endorsement .......................................... 8

2. Aircraft Specifics for the BE300/1900 models .............................................................. 8

2.1 Aircraft Approach Category ........................................................................... 10

2.2 Part-CAT, Subpart D – Instruments, Data, Equipment .................................. 10

2.3 Electronic Flight Bag (EFB) .......................................................................... 10

3. Operator Differences Requirements (ODR) ............................................................... 11

4. Master Differences Requirements (MDR) .................................................................. 12

4.1 MDR tables for the Models 300, 300LW, B300/B300C and

300 (FF serial with ProLine 21) .................................................................... 12

5. Specifications for Pilot Training ................................................................................. 13

5.1. BE300/1900 Initial Type Rating Training ......................................................... 13

5.1.1 Prerequisites ....................................................................................... 13

5.1.2 Training syllabus ................................................................................. 13

5.1.3 Training Areas of Special Emphasis (TASE) ....................................... 13

5.2. Familiarization / Differences Training ............................................................... 14

5.2.1 Familiarization / differences training from the BE 1900 models

(BE-1900 UA, BE-1900C UB/UC, and BE-1900D UE) to the

BE 300 models (300, 300LW, B300/B300C EFIS 85A, and

B300/B300C ProLine 21) .................................................................... 14

5.2.2 Familiarization / differences training between BE 300 models

(300 / 300LW / B300/B300C with EFIS 85A / B300/B300C

with ProLine 21) .................................................................................. 15

5.2.3 Familiarization / differences training between BE 1900 models

(BE-1900 UA, BE-1900C UB/UC, and BE-1900D UE) ........................ 16

5.2.4 Night Vision Goggle Operation (NVGO) .............................................. 17

6. Recurrent Training .................................................................................................... 17



7. Specification for Checking ........................................................................................ 17

7.1. Line Checks ................................................................................................... 18

8. Specifications for Recent Experience and Currency.................................................. 18

8.1. Recent Experience .......................................................................................... 18

8.2. Currency ......................................................................................................... 19

9. Line Flying Under Supervision (LIFUS) / Supervised Operating Experience (SOE)... 19

9.1 LIFUS / SOE following BE 300 Initial Type Rating Training ............................. 19

Appendix 1: Initial Type Rating Training for BE300/1900 ............................................................. 20

Appendix 2: ODR Tables for BE300/1900 models......................................................................... 21



Acronyms AFM .......................... Airplane Flight Manual

APU .......................... Auxiliary Power Unit

AT ............................. Auto throttle

CAS .......................... Crew Alerting System

CCD .......................... Cursor Control Device

CPD .......................... Common Procedures Document for conducting Operational Evaluation Boards, dated 10 June 2004

CPT .......................... Cockpit Procedures Trainer

CS-FCD ................... Certification Specifications for Operational Suitability Data (OSD) Flight Crew Data CS-FCD, Initial issue, 31 January 2014

CS-FSTD(A) ............ Certification Specifications for Aeroplane Flight Simulation Training Devices of 4 July 2012

Difference Level ....... a designated level of difference as defined in CS-FCD

EFIS.......................... Electronic Flight Instrument System

FFS ........................... Full Flight Simulator (Level C or D)

FMS .......................... Flight Management System

GPS .......................... Global Positioning System

GPWS ....................... Ground Proximity Warning System

HBC ......................... Hawker Beechcraft Company

IPT ............................ Integrated Procedure Trainer

LNAV ........................ Lateral Navigation

LPV ........................... Localizer Precision with Vertical guidance

LST .......................... License Skill Test

MFD .......................... Multi-Function Display

ND ............................ Navigation Display

ODR.......................... Operational Differences Requirements

OPC ......................... Operator Proficiency Check

OSD ......................... Operational Suitability Data

Part-FCL ................... Annex I to Commission Regulation (EU) No 1178/2011 of 3 November 2011 laying down technical requirements and administrative procedures related to civil aviation aircrew pursuant to Regulation (EC) No 216/2008 of the European Parliament and of the Council (as amended)

Part-ORO .................. Annex III to Commission Regulation (EU) No 965/2012 of 05 Oct 2012 laying down technical requirements and administrative procedures related to air operations pursuant to Regulation (EC) No 216/2008 of the European Parliament and of the Council (as amended)



Part-SPA ................... Annex V to Commission Regulation (EU) No 965/2012 of 05 Oct 2012 laying down technical requirements and administrative procedures related to air operations pursuant to Regulation (EC) No 216/2008 of the European Parliament and of the Council (as amended)

Route Sector ............ as defined in Part-FCL [“Route sector" means a flight comprising take-off, departure, cruise of not less than 15 minutes, arrival, approach and landing phases]

TCAS ........................ Traffic Alert and Collision Avoidance System

VNAV ........................ Vertical Navigation



Preamble 1. Introduction Where references are made to requirements and where extracts of reference texts are provided,

these are at the amendment state at the date of evaluation or publication of this document. Users

should take account of subsequent amendments to any references, in particular concerning

requirement for civil aviation aircrew and air operations.

Determinations made in this document are based on the evaluations of specific configurations of

aircraft models, equipped in a given configuration and in accordance with current regulations and

guidance.

Modifications and upgrades to the aircraft evaluated require additional OSD assessment for type

designation, training / checking / currency, operational credits, and other elements within the scope

of the OSD evaluations.

In accordance with Regulation (EU) No 748/2012 as amended by Commission Regulation (EU) No

69/2014 of 27 Jan 2014, the Operational Suitability Data contained in this document are identified

as follows:

[M] ............. mandatory Operational Suitability Data, bearing the status of rule (see GM No 3 to

21A.15(d))

[AMC] ......... non-mandatory Operational Suitability Data, bearing the status of Acceptable Means

of Compliance (see GM No 3 to 21A.15(d))

2. Operational Evaluation BE 300/1900 models The BE300/1900 models were evaluated in accordance with CS-FCD as certification basis, as well

as relevant requirements for pilot licensing and air operations which were applicable at the time of

the evaluation.

An operational evaluation of initial type rating training, familiarisation and differences training for

the BE300/1900 models was conducted by EASA as a catch-up evaluation. The evaluation

included an analysis of the corresponding FAA FSB reports for the BE-300 of 24 June 2015 and for

the BE-1900 of 17 Dec 2014, a review of an EASA approved syllabus for initial type rating of the

Beechcraft 300/1900 Series, dated 11 June 2014, provided by FlightSafety International, as well as

relevant Textron documentation.

The data contained in this document are agreed on the certification basis of CS-FCD, Initial Issue,

dated 31 Jan 2014 (elect to comply).



Operational Suitability Data (OSD) – Flight Crew 1. Aircraft Type Designation and Pilot License Endorsement [M]

With reference to Part-FCL, FCL.010 (‘type of aircraft’) and GM1 FCL.700, the BE300/1900 series

aircraft have been evaluated for aircraft categorisation and license endorsement.

The following BE300/1900 models are classified as high performance aeroplanes and within the

same type rating: Models 300, 300LW, B300/B300C and 300 (FF serial modified by installation of

Rockwell Collins ProLine 21 EFIS), as well as Models 1900, 1900C and 1900D.

The license endorsement is established as “BE300/1900”.

Manufacturer Aircraft

Model / Name License

Endorsement Variants Complex SP /

SP HPA / MP

OEB FC REPORT /

OSD FC available

Remarks

Hawker Beechcraft Corporation

1900 1900 C

BE300/1900 X X SP HPA X OSD FC BE300/1900, dated 17 Nov 2015

1900 D 300 300LW B300/B300C (except with ProLine 21)

B300/B300C (with ProLine 21) 300 (FF serial with ProLine 21)

2. Aircraft Specifics for the BE300/1900 models Model 300 The Model 300 aircraft is a complex, high performance, turboprop aircraft powered by 2 P&W

PT6A-60, 1050 shp engines. Rudder Boost is required to be installed and operative; if inoperative,

180lb. pressure may be required for single engine operation. Auto feather is required to be armed

and operative for takeoff, climb, approach and landing. The aircraft is certified for operations up to

35,000 feet but flight above 11,000 feet is prohibited without Yaw Damper operating. Maximum

take-off / landing weight is 14,000 pounds and maximum seating is 15, including crew.

Model 300LW The difference in the Model 300LW from the Model 300 is that the Model 300LW has a reduced

maximum takeoff / landing weight of 12,500 pounds. All systems, procedures and limitations

remain the same between the two models.

Model B300 / B300C The Model B300 is a follow-on version to the Model 300 with increased gross weight and

performance changes. The B300 has a 34 inch increase in cabin length, 14 inches ahead of the

wing and 20 inches aft of the wing. Wingspan is increased by approximately 3 feet plus winglets



adding 7 square feet of wing area. The B300 gross weight is increased to 15,000 pounds with 17

maximum occupants. The B300 is equipped with EFIS on the left side with optional EFIS for the

right side. The Model B300C is identical to the B300 except the addition of a large top hinged

Cargo Door in place of the bottom hinged passenger airstair door.

Model 300 (FF serial) – BE-300F The BE-300 and the BE-300F have identical flight characteristics. The Model 300 (FF serials) is a

Model 300 modified for use as a flight inspection aircraft and issued FF series serial numbers. The

modification consists primarily of an electronic testing equipment installation. The major difference

in type design is a large centre console, installed in the 300 (FF serials) variant that houses some

of this flight inspection equipment. The centre console restricts either pilot from reaching required

items on the opposite side of the cockpit. Because of this condition, the “Pedestal Equipment

Location” requires a minimum crew of two pilots for all operations. Model 300-F previously

equipped with Bendix King EFS-10 and modified by installation of Rockwell Collins ProLine 21

EFIS (FAA STC # SA01267WI-D, approved 27 July 2007) have a minimum crew requirement of

one pilot.

The Model 300-F equipped with Bendix King EFS-10 constitutes a separate type rating (with MP

operations), whereas the Model 300-F modified by installation of Rockwell Collins ProLine 21 EFIS

is within the same BE-300 type rating as a variant.

Model 1900, 1900C and 1900D

The systems between the Model 300 and the Model 1900 are basically the same regarding pilot

actions. The exceptions are the power steering on the Model 1900 and the propeller pitch lights

and rudder boost on the Model 300. Some flight characteristics of the Model 300 associated with

the shorter fuselage are not apparent in the Model 1900. However, most control and basic flight

characteristics of the two models are similar.

The FAA FSB recommended the Model 300 be included with the Model 1900 pilot type rating and

established a Pilot Type Rating "BE-300, BE-1900" for the Model 300 and 1900 on the FAA Pilot

Certificate Aircraft Type Rating List of 6 December 1984. After 6 Nov 1991 the FAA issued separate

type ratings for the BE300 and BE1900 models, while the JAA type rating endorsement remained

unchanged.



2.1 Aircraft Approach Category

With reference to Part-CAT, CAT.OP.MPA.320(b) the minimum straight-in approach category for

the BE300/1900 is as follows:

Aircraft Category

BE300/1900 B

2.2 Part-CAT, Subpart D – Instruments, Data, Equipment EU operators must show compliance with applicable elements of Annex IV to EU Regulation

956/2012 (Part-CAT, Subpart D), prior to beginning commercial transport operations.

2.3 Electronic Flight Bag (EFB) Electronic Checklists

(ProLine 21 Only)

A printed pilot checklist is always required for compliance with ORO.GEN.110. The Electronic Pilot

Checklist does not contain all required procedures due to inability to function in all non-normal flight

operation situations. The Electronic Pilot Checklist is acceptable for use for those Normal

Procedures it contains provided the aircraft operator ensures the Electronic Pilot Checklist

procedures remain current for the aircraft.

(ProLine FUSION)

A printed pilot checklist is always required for compliance with ORO.GEN.110. The Electronic

Checklist feature meets functional requirements and redundancy for Electronic Checklists, but no

Electronic Checklist content has been determined operationally suitable. Option for FSA-6000 on

all three AFD-3700 Displays is required for electronic dual redundancy. Viewing distance for PFD

and MFD charts is ~24 and ~28 inches, respectively. Use for chart zooming and touchscreen

panning is necessary to meet view ability for chart legibility.

Electronic Charts

(ProLine 21 Only)

Electronic Approach Charts (SIDS, STARS, Approach Charts & Airport Diagrams) are available

through the IFIS-5000 File Server Unit. Dual redundancy is not met due to single MFD Display, File

Server Unit, and Cursor Control Panel. Memory button selection on the Cursor Control Panel is

required to allow single pilot action to change between Navigation Display, Electronic Checklist



Display and Electronic Charts Display to mitigate single pilot workload using these functions. The

enhanced map overlays do not meet requirements for Enroute charts therefore another suitable

source of Enroute Chart information must be available at the pilot station.

(ProLine FUSION)


through the FSA-6000 File Server Application. Low Visibility Taxi Charts are also selectable (not

approved for Airport Moving Map Display per FAA AC 20-159). The option for FSA-6000 on all

three AFD-3700 Displays is required for electronic dual redundancy.

(G1000 Only)


through the GDU-1500 MFD SD Card. Dual redundancy is not met due to single MFD Display and

SD Card. Display does not meet criteria for full chart displayed equally viewable to paper being

replaced, however the zoom and pan feature allows a single pilot action to view the remainder of a

chart when set to a readable size. In addition, the chart display function has soft keys for Briefing,

Plan, Profile & Minimums chart sections to be selected with single pilot action.

3. Operator Differences Requirements (ODR) [M] The FAA approved ODR tables as reproduced at Appendix 2 are part of the operational

suitability data and constitute the basis for familiarisation and differences training.

[M] All familiarisation and differences training contained in this document must address the items

listed in the pertinent ODR tables.

ODR tables are HBC generic and therefore may not include items that are applicable to particular

operators.

[AMC] Operators using more than one variant must have approved ODR tables pertinent to their

fleet.



4. Master Differences Requirements (MDR) [M]

4.1 MDR tables for the Models 300, 300LW, B300/B300C and 300 (FF serial with ProLine 21). MDR tables for the above variants are shown below. Definitions of the various levels for Training /

Checking / Currency are those used in CS-FCD.

Master Differences Requirement (MDR) Table

FROM AIRCRAFT

TO A

IRC

RA

FT

Model 300 Model 300LW

Model B300/B300C except with ProLine 21

Model B300/B300C with ProLine

21

Model 300 (FF serial)

with ProLine 21

Model 300 A / A / A (1)(2)(3)(4)(5)(6)

B / A / B (1)(2)(3)(4)(5)

B / B / B (1)(2)(3)(4)(5) D / C / C D / D / D

Model 300LW B / A / B (1)(2)(3)(4)(5)

A / A / A (1)(2)(3)(4)(5)(6)

B / B / B (1)(2)(3)(4)(5) D / C / C D / D / D

Model B300/B300C except with ProLine 21

B / B / B (1)(2)(3)(4)

B / B / B (1)(2)(3)(4)

A / A / A (1)(2)(3)(4)(6) D / C / C D / D / D

Model B300/B300C with ProLine 21 D / C / C D / C / C D / C / C A / A / B

(3)(7)(8) B / B / C

(3)

Model 300 (FF serial) With ProLine 21 D / D / D D / D / D C / D / D C / C / C A / A / B

(3)

NOTES: (1) Primary Flight Instruments may include mechanical, electro-mechanical, Collins EFIS-74A &

EFIS 85 (3, 4 or 5 tube), Sperry EDZ 600/800 (3 or 5 tube), Bendix EFS-10 (3 or 4 tube).

Differences in primary flight instruments from mechanical and electro-mechanical (servo) to

EFIS or between EFIS systems installations is C/B/C. Differences in primary flight

instruments from EFIS to mechanical and electro-mechanical (servo) or between mechanical

and electro-mechanical (servo) is B/B/B.

(2) Installation of ProLine 21 on aircraft equipment listed in NOTE (1) is D/C/C.

(3) For Collins ProLine 21 equipped aircraft, the installation of IFIS-5000 FSU is C/B/C.

(4) Installation of Collins IDS-3000 ON EFIS 85 aircraft is D/C/C.

(5) Installation of Honeywell EPIC CDS/R on EDZ-600/800 aircraft is D/C/C.

(6) Installation of GARMIN G1000 is D/C/D.

(7) Installation of GARMIN G1000 is C/C/C for basic equipped or D/C/D if optional SVS & ESP.

(8) Installation of ProLine FUSION Embedded Display System (EDS) on ProLine 21 is C/C/C.

BE 1900 models is shown in separate table.



5. Specifications for Pilot Training

5.1 BE300/1900 Initial Type Rating Training 5.1.1 Prerequisites

These provisions apply for pilots who meet the minimum prerequisites in accordance with Part-

FCL.

[AMC] For pilots with no or limited experience in multi-engine turboprop aircraft, including various

avionics suites and navigation systems, additional modular training should be considered prior to

beginning practical training.

5.1.2 Training syllabus

[AMC] Full initial type rating training and initial type rating training with credit for commonality is

contained at Appendix 1.

[M] Reduced initial type rating training is based on commonality between the King Air 200 Series

(BE 200 / 200GT / 250) and the BE300/1900 series when both are equipped with ProLine 21. It is

applicable for experienced pilots who are current and qualified on the King Air 200 Series (BE 200 /

200GT / 250) equipped with ProLine 21 when transitioning to the BE300/1900 series.

5.1.3 Training Areas of Special Emphasis (TASE)

[M] The following training areas of special emphasis must be addressed during ground and flight

training for all BE300 models:

• Aircraft performance calculations and operational performance requirements; gross versus

net climb gradients for terminal are procedures and for obstacles;

• Navigation means with various installed equipment and navigation systems;

• Primary Flight Display (PFD) format and function for mechanical, electronic and PFD

displays;

• EFIS function and procedures, including Display Processor Unit (DPU) failures and EFIS

Reversionary Switching, as well as use of Composite Mode to conduct Precision and Non-

Precision Approaches, with and without Flight Director;

• High altitude operations.

[M] The following training areas of special emphasis must be addressed during ground and flight

training for BE300/1900 models, as applicable:

• Aircraft performance calculations and operational performance requirements (with an

emphasis on differences between variants, as applicable); gross versus net climb gradients

for terminal are procedures and for obstacles;



• Navigation means with various installed equipment and navigation systems;

• Primary Flight Display (PFD) format and function for mechanical, electronic and PFD

displays;

• EFIS function and procedures, including Display Processor Unit (DPU) failures and EFIS

Reversionary Switching, as well as use of Composite Mode to conduct Precision and Non-

Precision Approaches, with and without Flight Director (BE300 models and BE-1900D);

• High altitude operations;

• Reduced Power Takeoffs, including associated AFM criteria (BE-1900D);

• Flight characteristic for stall warning with ice accumulation – airframe buffet in lieu of

audible stall warning (BE1900 models).

5.2 Familiarization / Differences Training

5.2.1 Familiarization / differences training from the BE 1900 models (BE-1900, BE-1900C, and BE-1900D) to the BE 300 models (300, 300LW, B300/B300C EFIS 85A, and B300/B300C ProLine 21).

[M] Familiarisation training is valid only when integrated into BE 300 initial type rating training.

[M] The pilot must be qualified and current in the applicable BE 1900 variant.

[AMC] The following MDR table applies when transitioning from the BE 1900 models to the BE 300

models:

Familiarization Training / Checking / Currency

FROM AIRCRAFT

TO A

IRC

RA

FT

BE-1900 / BE-1900C BE-1900D

300, 300LW, B300/B300C EFIS 85A

D / C / C (1) (3)

B / B / B (1) (3) (4) (5)

B300/B300C ProLine 21 D / C / C (4) (5)

D / C / C (1) (2) (3) (4) (5)

Definitions of the levels for Training / Checking / Currency are those used in CS-FCD.

Familiarization / differences training should address the items shown in the above table, which

correspond to the following subjects:

(1) Aircraft General

(2) Electrical Power

(3) Avionics

(4) Fuel



(5) Performance / Weight & Balance

Time required for training is 2.0 hours for 2 subjects, 3.0 hours for 4 subjects and 4.0 hours for 5

subjects.

Level B checking should consist of a written examination.

5.2.2 Familiarization / differences training between BE 300 models (300 / 300LW / B300/B300C with EFIS 85A / B300/B300C with ProLine 21)

[M] The pilot must be qualified and current in the applicable BE 300 base model.

[AMC] The following applies when transitioning from a BE 300 base model to another BE 300

variant:


FROM AIRCRAFT

TO A

IRC

RA

FT

B300/B300C with EFIS 85A

B300/B300C with ProLine 21

B300/B300C with EFIS 85A - - - (2)

B300/B300C with ProLine 21 (1) - - -

300 / 300LW (3) (3)

Training should address the items shown in the above table, which correspond to the following

subjects:

(1) Avionics including ProLine 21 – Initial 8.0 hours / Recurrent 4.0 hours

(2) Avionics including EFIS 85A – Initial 6.0 hours / Recurrent 4.0 hours

(3) Differences B300/B300C to 300/300LW – 0.5 hours



5.2.3 Familiarization / differences training between BE 1900 models (BE-1900, BE-1900C, and BE-1900D)

[M] The pilot must be qualified and current in the applicable BE 1900 base model. Familiarisation

training may be integrated in BE 1900 initial type rating training.

[M] The following MDR table applies when transitioning between BE 1900 models:


FROM AIRCRAFT

TO A

IRC

RA

FT

BE-1900 (UA) BE-1900C (UB) BE-1900C (UC) BE-1900D (UE)

BE-1900 (UA) see note (a)

B / B / B (1) (3) (10) (11)

(13) see note (a)

B / B / B (1) (3) (10) (11)

(13) see note (a)

C / B / B (1) through (13)

BE-1900C (UB)

B / B / B (1) (3) (10) (11)

(13) see note (a)

see note (a)

B / B / B (1) (3) (10) (11)

(13) see note (a)

C / B / B (1) through (13)

BE-1900C (UC)

B / B / B (1) (3) (10) (11)

(13) see note (a)

B / B / B (1) (3) (10) (11)

(13) see note (a)

see note (a) C / B / B

(1) through (13)

BE-1900D (UE)

D / C / C (1) (3) (4) (9) (10)

(11) (13)

D / C / C (1) (3) (4) (9) (10)

(11) (13)

D / C / C (1) (3) (4) (9) (10)

(11) (13) see note (b)

Definitions of the levels for Training / Checking / Currency are those used in CS-FCD.

(a) Differences within the 1900 / 1900C variants are the fuel system and specific aircraft

equipage

(b) Differences within 1900D for specific equipage are B/B/B, for IDS-3000 installation D/D/C,

and for G950 installation are D/D/C.

[AMC] Familiarization/differences training should address the items shown in the above table,

which correspond to the following subjects:

(1) Aircraft General

(2) Electrical Power

(3) Fuel

(4) Propellers

(5) Powerplant

(6) Environmental

(7) Pressurization

(8) Oxygen



(9) Flaps

(10) Avionics

(11) Performance/Weight and Balance

(12) Ice/Rain Protection System

(13) Annunciator System

Time required for training is 2.0 hours for 5 subjects, 3.0 hours for 7 subjects and 4.0 hours for 13

subjects.

Level B checking should consist of an oral or written examination.

5.2.4 Night Vision Goggle Operation (NVGO)

[M] With reference to SPA.GEN.105 and SPA.GEN.120, the following training areas of special

emphasis must be addressed during aircraft NVG ground and flight training:

• Recovery from inadvertent IMC;

• 2 pilot operating procedures if required for type of NVG operation to mitigate workload or

NVG failures transitioning to un-aided operation;

• Landing illusions using NVGs;

• Operating aeroplanes around airports and/or obstructions with LED lighting not visible with

authorized NVGs.

6. Recurrent Training Recurrent training must be compliant with EU regulations for civil aviation aircrew and air

operations, as applicable, and include the identified Training Areas of Special Emphasis.

Operators must establish an approved recurrent training and checking programme which is

relevant to the aircraft variant flown and its intended operation.

[M] Difference levels between BE300/1900 variants for recurrent training are the same as for initial

training.

[M] Recurrent training must address the differences between the BE300/1900 variants flown as

identified in the relevant ODR tables.

7. Specification for Checking Checking must be performed in accordance with applicable EU regulations for civil aviation aircrew

and air operations.



Recurrent checking is addressed in Part-FCL and Part-ORO, specifically in ORO.FC.130,

ORO.FC.220, ORO.FC.230, AMC1 ORO.FC.230, GM1 ORO.FC.230, ORO.FC.240, and AMC1

ORO.FC.240

[M] Difference levels between BE300/1900 variants for recurrent checking are the same as for

initial checking.

[AMC] Recurrent checking should be alternated between BE300/1900 models flown.

[M] If recurrent checking is not alternated between BE300/1900 models flown, the differences as

identified in the relevant MDR/ODR tables between the BE300/1900 variants flown must be

addressed.

[M] All checking must include the elements of the relevant TASE on a rotational basis, as well as

the following items, as applicable:

• Takeoff Safety, Performance planning & decisions, contaminated runways;

• High altitude conditions and aerodynamics;

• RVSM, TCAS, TAWS and Windshear functions and procedures;

• Inflight and Ground Icing Awareness;

• CRM and CFIT procedures.

[AMC] The following items should be emphasised during checking, as applicable:

• Aircraft Performance calculation and aircraft handling to achieve performance;

• Demonstration of FMS navigation (departures, arrivals, approaches) proficiency;

• Selection and use of EFIS displays, raw data, flight director, and Reversion / Composite

modes, including DPU failure.

7.1 Line checks [M] A line check performed on any BE300/1900 variant is valid for all variants.

8. Specifications for Recent Experience and Currency

8.1 Recent Experience [M]

Recent experience requirements are contained in Part-FCL, FCL.060.

With reference to Part-ORO, ORO.FC.140(a), full credit is granted for recent experience

requirements between BE300/1900 variants.



8.2 Currency [M]

Where MDR tables specify Level B Currency, currency is maintained by operating the variant

aircraft within the previous 180 days. Level B currency may be re-established by a review of

Placards, Limitations and Operating Procedures prior to operating the variant.

Where MDR tables specify Level C Currency, currency is maintained by operating the variant

aircraft through a complete route sector including an instrument approach procedure within the

previous 90 days. Currency may be re-established by operating the variant with a qualified PIC for

at least one route sector, completing a Line Check, completing a Proficiency Check in the variant

aircraft or compliance with Part-FCL, FCL.060 recent flight experience requirements in the variant.

Where MDR tables specify Level D Currency, currency is maintained by operating the variant

aircraft through 3 complete route sectors within the previous 60 days. Currency may be re-

established by completing a Line Check, completion of a Proficiency Check in the variant or

compliance with Part-FCL, FCL.060 recent flight experience requirements in the variant.

9. Line Flying Under Supervision (LIFUS) / Supervised Operating Experience (SOE)

LIFUS should be performed in accordance with ORO.FC.220 and AMC1 ORO.FC.220(e).

Furthermore, GM1 ORO.FC.220(d) provides guidelines for operators to use when establishing their

individual requirements. Supervised Operating Experience (SOE) may be established in

accordance with Part-FCL, FCL.720.A (g) through the operational suitability evaluation.

9.1 LIFUS / SOE following BE 300 Initial Type Rating Training

[AMC] Pilots completing initial type rating training for the BE 300 should perform a minimum of 10

route sectors of LIFUS, followed by a 2 route sector line check or an equivalent amount of SOE.

[AMC] Where there is a change of operating conditions or route structure this should be taken into

account and may need additional route sectors to cover these elements.



Appendix 1 [AMC] Initial Type Rating Training for BE300/1900

TRAINING SYLLABI TIME SCALE

Full Initial Training Initial Training with credit for commonality

Ground School Hours of training

Aeroplane Systems 37.0* 10.5 General Operational Subjects (Includes Load and Balance, Performance, Flight Planning, AFM/POH, Windshear Training and CRM)

6.0 4.5

Systems Integration (completed as part of Ground School) 4.0* 0.0

Practical Training (in the Flight Simulator) 12.0 (SP) 14.0 (MP)(1)

6.0 (SP) 12.0 (MP)

Flight Crew Training (Flight Simulator) Single Pilot Operations • Pilot Flying (PF) Multi-Pilot Operations • Pilot Flying (PF) • Pilot Monitoring (PM)

12.0

12.0 2.0

6.0

6.0 6.0

* additional training may be required subject to previous experience on similar aircraft

systems and/or avionics.

(1) includes a minimum of 12.0 hours of PF and at of 2.0 hours of PM.

Briefing times are not included and normally consist of 1.0 hour (briefing) and 0.5 hour (debriefing)

for each flight simulator training session.

Full Initial Training: Theoretical training, including knowledge exam should be distributed over a period of 6 training

days.

Practical training, including skill test should be distributed over a period of 7 days.

Initial Training with credit for commonality: Theoretical training, including knowledge exam should be distributed over a period of 3 training

days.

Practical training, including skill test should be distributed over a period of 4 days.



Appendix 2 [M] ODR Tables for BE300/1900 models

1. Model 300 to Model 300(FF Serials) Definitions used in the ODR Tables:

X .......... Pilot’s Operating Handbook and or Flight Manual Supplement

CPT .... Cockpit Procedure Training

SI ........ Self Instruction

AI ........ Aided Instruction

DIFFERENCE AIRCRAFT: 300(FF Serials) BASE AIRCRAFT: Model 300

COMPLIANCE METHOD

TRAINING CHKG/CURR

SYSTEM REMARKS FLT CHAR

PROC CHNG

LVL A

LVL B

LVL C

LVL D

CHK CURR

21 Air Conditioning

Auto Pressure Controller located at rear of Center Pedestal

No Minor SI A B

21 Auxiliary Air Conditioner

Initially installed then later removed. No Minor AI B B

22 Autopilot/Yaw Damper

Yaw Damper-King vs Collins. Both operate identically.

No No SI A A

23 Communication

Addition audio panel and communication equipment.

No No AI B B

24 Electrical Power

Load Shedding No Yes AI B C

25. Flight Inspection Panel System

Mission specific equipment installed. No Yes AI B B

26 Fire Protection

Location of Portable Fire Extinguishers. No No SI A A

34 Navigation

Bendix King EFS-10 Electronic Flight Instruments System (EFIS) – Symbol Generators. FMS operation. Flight Inspection Control Display Unit.

No Yes CPT D D



DIFFERENCE AIRCRAFT: 300(FF Serials) BASE AIRCRAFT: Model 300

COMPLIANCE METHOD

TRAINING CHKG/CURR

DESIGN REMARKS FLT CHAR

PROC CHNG

LVL A

LVL B

LVL C

LVL D

CHK CURR

Inst Panel Layout Dual EFS-10 EFIS and Multi-function Displays. Caution/Warning Panel and Flight Director mode controllers relocated to glareshield. Standby Attitude Indicator required for Dual EFS-10 system.

No Minor AI A B

Flight Deck Pressurization controller relocated to rear of center console.

No Minor AI A B

MANUEVER REMARKS FLT CHAR

PROC CHNG

LVL A

LVL B

LVL C

LVL D

CHK CURR

No Change



2. Models 300, 300LW (SFAR 41C) to Models B300/B300C (commuter category) Definitions used in the ODR Tables:

X .......... Flight Manual / Pilot’s Operating Handbook and / or FM Supplement

AI ......... Aided Instruction

CBT .... Computer Based Training

ICBT ... Interactive Computer Based Training

FTD ..... Flight Training Device (FTD Level I or II)

FFS ...... Full Flight Simulator (Level A, B, C, D)

SAMPLE DIFFERENCES TABLE DIFFERENCE AIRCRAFT: B300, B300C (commuter category) BASE AIRCRAFT: 300, 300LW (SFAR 41C)

COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

General Airplane Configuration

Commuter Category certification basis 34 inches longer cabin, 14 fwd, 20 aft 3 feet wingspan by 18 inch wingtips Cockpit 14 inches fwd reference nacelles

NO NO AI B B

Weights

Increase to 15,000 pounds MGTW NO NO X A B

Limitations

VMO/MMO Overspeed Aural Warning Single Engine Reversing Prohibited NO YES AI B B

Placards and Markings

Numerous Annunciator Panel changes. NO YES AI B B

Servicing

Engines

Flight Deck

Instrument Panel Layout

Left side EFIS standard, Right side option. Auto Feather annunciators relocated NO YES X A B

Cabin

Flight Controls Flaps preset positions only NO YES AI B B

Aerodynamic Controls

Reduction in roll control forces 3 position Flaps, no intermediate

YES YES AI B B



SAMPLE DIFFERENCES TABLE

DIFFERENCE AIRCRAFT: B300, B300C (commuter category) BASE AIRCRAFT: 300, 300LW (SFAR 41C)

COMPLIANCE METHOD

TRAINING CHKG/CURR

MANEUVER REMARKS FLT CHAR

PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

Preflight

Engine Start

Taxi

Takeoff Improved Performance for Commuter Category Takeoff, Climb, Approach Climb Changes in propeller Ground Low Pitch Stop at 68 to 70% N1 prevents engine acceleration surges on takeoff.

NO YES AI B B

RTO Or V1 Fail

B300 meets Engine Failure performance requirements for Commuter Category NO YES AI B B

Climb Cruise Decent

Instrument Approaches

Landing Demonstrated Crosswind no 25 Kts NO NO X A B

Shutdown Hot Battery Buss Switch NO YES AI A B

Normal Procedures Changed Normal Procedures for design changes and Commuter Category NO YES AI B B

Abnormal Procedures

Changed and New Abnormal Procedures for design changes and Commuter Category. NO YES AI B B

Emergency Procedures

No Single Engine Reverse NO YES AI A B

In-Flight Maneuvers Roll Control forces reduced approx. 35% YES NO AI A B




DIFFERENCE AIRCRAFT: B300, B300C (commuter category) BASE AIRCRAFT: 300, 300LW (SFAR 41C)

COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

21 Air Conditioning

Cabin Pressure White Annunciator at 10,000 feet with Aural Tone. Cabin Altitude Red warning annunciator and Aural Tone at 12,000 feet.

NO YES AI B B

22 Auto-Flight

Control Wheel Disconnect button is 2 position for trim interrupt & AP Disconnect. Autofeather is Torque activated versus bleed air activated previous

NO YES AI B B

23 Communications

Various radio suite options (See MDR NOTES) NO YES

24 Electrical Power

Both AC Inverters ON full time Hot Battery Buss & Switch added, several power distribution changes

NO YES AI A B

25 Equipment / Furn.

26 Fire Protection

27 Flight Controls

Flap selection 3 position with no intermediate settings. NO YES AI A B

28 Fuel

Optional Extended Range Fuel tanks NO NO X A B

29 Hydraulic

30 Ice / Rain

2 Deice Boot green annunciators to monitor boot operation. NO YES X A B

31 Indicating/Record

Propeller Pitch Lights now White to preclude transient Master Cautions. Pitch Trim annunciator now caution Add Annunciators: AC Buss, Cabin Overpressure, Auto Feather OFF, Oxygen Not Armed, Rudder Boost OFF, Wing Deice, Tail Deice, 10,000 ft Cabin Altitude, Cabin Differential High, Aural Warning on Airspeed Overspeed.

NO YES AI B B

32 Landing Gear

33 Lights

Hot Battery Buss cockpit flood light NO YES AI A B

34 Navigation

Various Avionics Suites available as options and may be different from base airplane. (See MDR NOTES)

NO YES

35 Oxygen

Add Passenger Oxygen Light NO YES AI B B

36 Pneumatics

Brake Deice now ON for Takeoff & Landing Remove Rudder Boost from Bleed Air system. NO YES AI B B

37 Vacuum

49 APU

52 Doors

Cargo Door Model, Large cargo door hinged at top replaces narrow passenger door airstair hinged at bottom.

NO YES AI B B



SAMPLE DIFFERENCES TABLE DIFFERENCE AIRCRAFT: B300, B300C (commuter category) BASE AIRCRAFT: 300, 300LW (SFAR 41C)

COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

53 Fuselage

34 inches longer cabin, 14 in. fwd of wing, 20 in. aft of wing

NO NO X A A

54 Nacelles/Pylons

55 Horizontal & Vertical Stab.

56 Windows

57 Wings

3 feet wingspan increase by 18 inch wingtips NO NO X A A

61 Propellers

Low Pitch Stop resets from Ground Idle to Flight Idle at 68-70% N1 (or Kit # 130-9600) NO NO X A A

72 Engine (turbine)

73 Fuel Controls

74 Engine Ignitions

75 Engine Bleed Air

76 Engine Controls

77 Engine Indicating

78 Exhaust

79 Engine Oil

80 Engine Starting



3. Models 300, 300LW, B300/B300C Proline 2 EFIS-85 to Models 300, 300LW, B300/B300C Proline 21

Definitions used in the ODR Tables:


AI ......... Aided Instruction





SAMPLE DIFFERENCES TABLE DIFFERENCE AIRCRAFT: 300, 300LW, B300, B300C Proline 21 BASE AIRCRAFT: 300, 300LW, B300, B300C Proline 2 EFIS-85

COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR


Change from individual flight instruments to composite PFD format.

No Yes AI C C

Weights

Revised BOW No No X A B

Limitations

New Limitations for new equipment No No X B B


Changed Placards & Markings for avionics. AFM changed to new P/N No Yes X B B

Servicing

No Change

Engines

No Change

Flight Deck

Configuration and controls to accommodate Proline 21 system. No Yes AI C C


EFIS-85 EADI, EHSI, ALT, AS, VSI, TC replaced with Proline 21 PFD(2) & MFD(1) No Yes AI C C

Cabin

No Change

Flight Controls No Change


No Change




DIFFERENCE AIRCRAFT: 300, 300LW, B300, B300C Proline 21 BASE AIRCRAFT: 300, 300LW, B300, B300C Proline 2 EFIS-85

COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

Preflight PFD/MFD power distribution No Yes FTD B B

Engine Start Use of MFD Engine Display and PFD/MFD power distribution. No Yes FTD B B

Taxi Flight Instrument checks. No Yes FTD B C

Takeoff V-speed and Altitude Selection. Airspeed Indication on tape format. No Yes FTD B C

RTO Or V1 Fail

Airspeed Indication on tape format. Attitude indications on PFD format. Low Speed Awareness cues.

No Yes FFS B C

Climb Cruise Decent

PFD format for all flight instruments. Low Speed Awareness cues. Selection and use of Nav Sources Instrument scan skill in PFD format.

No Yes FTD B C


Nav Source Selection & display format. Instrument scan skill in PFD format. No Yes FFS C C

Landing V-speed and Altitude Selection. Airspeed Indication on tape format No Yes FTD B C

Normal Procedures Nav Source selection, Nav Display format, Autopilot & FD control. IFIS-5000 use procedures. TCAS & TAWS use procedures.

No Yes FFS C C

Abnormal Procedures

Abnormal procedures for Avionics / Flight Instruments of Proline 21 system No Yes FTD B B


Emergency procedures for Dual Generator Failure, AC Inverter Failures, Emergency Power Management, and Standby Flight Instruments

No Yes FTD C C

In-Flight Maneuvers Tape format & Low Speed Awareness for Steep Turns and Stalls. Instrument scan skill in PFD format.

No Yes FFS C C




DIFFERENCE AIRCRAFT: 300, 300LW, B300, B300C Proline 21 BASE AIRCRAFT: 300, 300LW, B300, B300C Proline 2 EFIS-85

COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

All System Chapters Chapters not listed on this table are unchanged by this modification.

22 Auto-Flight

FCP-65 Control, Mode Control Panel and respective annunciation panels in pedestal replaced by FGP-3000 on glare shield and mode annunciation on PFD. AP Mode Annunciation now on PFD.

No Yes AI B B

23 Communications

CTL-22 VHF Comm controls replaced with RTU-4200 on center instrument panel for primary control and CDU-3000 as secondary control. Audio Panel control moved from upper center instrument panel to outboard instrument panel.

No Yes AI B B

24 Electrical Power

AC Powered use equipment reduced. Avionics Buss items changed ESIS Standby Power.

No Yes AI B B


Install Integrated Avionics Processor System. Several Annunciations now on PFD

No No X A A

33 Lights

Display Dimming controls changed No No X A A

34 Navigation

Flight Instruments ADI, HSI, ALT, AS, VSI, TC “Basic T” replaced with Proline 21 PFD format. DME, RMI & Radio Altimeter integrated into PFD. (2) Attitude Heading Computers AHC-3000, (2) Flux Detector Units FDU-3000 and (2) External Concentrator Units ECU provide Attitude and Heading information to PFD (2) Air Data Computers ADC-85A provide PFD data for AS, ALT & VS. Airspeed data includes Overspeed Alerts and Low Speed Warnings on PFD. Altitude Selector and Alerter control moved to FGP. Altimeter Baro Selection on DCP and configurable for Ft/M & In/hPa. Standby Instruments Add GH-3100 (ESIS) Electronic Standby Instrument System provides ATT, ALT, AS, TS, HDG, Baro-set, NAV 1.

No Yes FTD C C

34 Navigation

EFIS Controls Added (2) DCP-3000 on instrument panel (1) FGP-3000 on glare shield (1) CDU-3000 on center pedestal Flight Display (FD) Bezel Buttons control display configuration. Reversion controls on lower center Inst. Panel CHP-86B Course Heading Panel replaced by Flight Guidance Panel FGP-3000 FGP-3000 includes Flight Director Mode Selection

No Yes FTD C C



SAMPLE DIFFERENCES TABLE DIFFERENCE AIRCRAFT: 300, 300LW, B300, B300C Proline 21 BASE AIRCRAFT: 300, 300LW, B300, B300C Proline 2 EFIS-85

COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

34 Navigation

FMS UNS-1K replaced by FMS-3000 controlled by CDU-3000. CTL-32 Nav Radio tuning replaced with RTU-4200 and CDU-3000 backup tuning.

No Yes FTD C C

34 Navigation

AFD-3010 MFD display replaces MFD-85. Weather Radar overlay selectable on MFD Radar control on FD Bezel and DCP.

No Yes AI B B

34 Navigation

TAWS/GPWS display on PFD and MFD with control on FD Bezel and DCP. Remote switch/annunciators on Inst. Panel for FLAP/OVRD, G/S INHIB, TERR INHIB and STEEP APPR.

No Yes AI B B

34 Navigation

TCAS I with Traffic Display selectable on PFD and MFD with Nav Display overlay. TCAS control on FD Bezel and DCP. TCAS Mode Selections On/Stby & Test/Alt on lower center Inst. Panel. Transponder control on RTU & CDU.

No Yes ICBT B B

45 Maintenance Computer

MDC-3100 series Maintenance Computer added. No No X A A

46 Information Systems

IFIS-5000 File Server Unit (FSU) option FSU provides Charts, Geo-Political and WX Data functions on MFD.

No Yes FTD B C

53 Fuselage

New Exterior Antenna for Wx Data options. No No X A B

61 Propellers

Propeller Syncro-Scope moved to MFD EIS AFX green annunciation on EIS near Trq/ITT instrument.

No No X A B


Separate Analog Engine Instruments replaced Engine Display. (Normal on MFD, Reversion on PFD) Exceedences are annunciated in Red. Abnormal indications are annunciated in Amber. Primary for power Torque and ITT combined round dial gauge & digital display, Propeller RPM is round dial gauge & digital display: N1 is round dial gauge & digital display. Fuel Flow, Oil Pressure & Oil Temp are digital only. Engine Fire Indication added to Engine Display inside TRQ/ITT indicator. EIS Reversion to PFD if MFD fails

No Yes FTD C C

80 Engine Starting

Engine Instruments on MFD EIS for start No No FTD C C



4. Models 300, 300LW, B300/B300C [MDR NOTE (1) equipment only] to Models 300, 300LW, B300/B300C with G1000

Definitions used in the ODR Tables:

X .......... Pilot’s Operating Handbook and / or FM Supplement




CPT .... Cockpit Procedure Trainer


DIFFERENCES TABLE DIFFERENCE AIRCRAFT: 300/300LW/B300/B300C with G1000 BASE AIRCRAFT: 300/300LW/B300/B300C (MDR NOTE (1) equipment only)

COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

General Airplane Configuration No Change

Weights Reduces Basic Operating Weight NO NO X A B

Airworthiness Limitations

New aircraft Limitations (See Airplane Flight Manual Supplement) NO YES X A A


New aircraft Placarding (See Airplane Flight Manual Supplement) NO NO X A A

Servicing

AFMS Section 8, new service & handling (ref. G1000/GFC 700 System Maint. Manual) NO YES X B B

Engines No Change

Flight Deck

Remove Collins EFIS-85B, FCP-65 Mode Control Panel, Mode Control Annun. Panel, AP Control, AP Annun. Panel Install Garmin G1000

NO YES FFS C D


• Separate AS, EADI/EHSI, ALT, VSI to dual PFD Format

• RMI removed • Engine Gauges replaced to MFD • Replaced standby ADI with mechanical

standby AI, altimeter and airspeed ind. • Prop sync switch moved to instrument panel • Standby instrument power switch moved to

instrument panel • GMC 710 autopilot controller beneath

glareshield in center instrument panel • GMA-1347 audio panels outboard of PFD • GCU-477 MFD control in center pedestal

NO YES FFS C D

Cabin No Change

Flight Controls Electric Trim has added speed schedule. YES NO X A A


Garmin Electronic Stability & Protection (ESP) Garmin Under Speed Protection (USP) and Overspeed Protection Systems added (option)

YES YES FFS D B




DIFFERENCE AIRCRAFT: 300/300LW/B300/B300C with G1000 BASE AIRCRAFT: 300/300LW/B300/B300C (MDR NOTE (1) equipment only)

COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

Preflight Avionics Preflight NO YES X B B

Engine Start Engine Gauges changed to electronic display on the MFD NO NO X B B

Taxi Taxi and Runup Checklist Procedures - See Airplane Flight Manual Supplement NO YES X B B

Takeoff PFD replaces separate Basic T inst. Engine Power Instruments moved to MFD. Speed displayed on tape with Low Speed Awareness. Altitude displayed on tape with RAD ALT interface collocated.

NO NO FFS C D

RTO Or V1 Fail

No Change

Climb Cruise Decent

No Change

In-Flight Maneuvers Steep Turns, Slow Flight, Approach to Stall affected by PFD display changes for Low Speed Awareness cues. SVS function and use. ESP & USP function and use

NO NO FFS C D


All new PFD, MFD, FMS, Autopilot WAAS procedures, LNAV & LPV approaches USP function and use

NO YES FFS C D

Landing PFD Primary Flight Inst. with Vref on speed tape. RAD Alt & Mins on Altitude tape. NO YES FFS B B

Shutdown No Change

Normal Procedures See Airplane Flight Manual Supplement for review of all Normal Procedures NO YES FTD C D

Abnormal Procedures

See Airplane Flight Manual Supplement for new or changed Abnormal Procedures NO YES FTD C D


See Airplane Flight Manual Supplement for new or changed Emergency Procedures NO YES FTD C D




DIFFERENCE AIRCRAFT: 300/300LW/B300/B300C with G1000 BASE AIRCRAFT: 300/300LW/B300/B300C (MDR NOTE (1) equipment only)

COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

21 Air Conditioning No Change

22 Auto-Flight

Collins APS-65 autopilot & FCP-65 mode control replaced by Garmin GFC 700 autopilot with GMC 710 mode control. Alt. Alerter integrated on PFD using DCU. Remote Mode Annun. Panel removed for GFC-700 Mode Annun. now integrated on PFD. RED Autopilot Disconnect on yoke now single stage switch for Trim, YD, RB, AP Rudder Boost using AP servo for Vmcg per Exemption 5599 (B300, B300C only)

YES YES FTD C C

22 Auto-Flight

Garmin ESP System software, default to ON Garmin USP System software AP coupled Go-Around only with ESP installed

YES YES FFS C D

23 Communications

Dual Garmin GIA 63W Communication Transceivers are installed. Replaced Audio Control Panel with dual Garmin GMA 1347 audio panels outboard of each PFD. Emer. Freq. push button add on Center Pedestal

NO YES X B B

24 Electrical Power

Individual Circuits & Circuit Breakers change with new EL Panel labels and locations. (No circuit breaker source color code provide) Power Distribution for new systems (AFMS Sec.7) Standby battery powered items changed AC Inverters and associated switches removed by G1000 installation

NO YES X B B


Several New Avionics Racks behind instrument panel and in forward avionics bay NO NO X A A

26 Fire Protection No Change

27 Flight Controls

Electric Trim Circuit Breaker Switch removed. Trim interrupt (Yoke Trim Button) new function Electric Pitch Trim speed schedule added.

YES YES X B A

28 Fuel No Change

29 Hydraulic No Change

30 Ice / Rain No Change


Replaced A/P TRIM FAIL, INVERTER, AP DISC, AP TRIM FAIL and ELEC TRIM OFF lamp assemblies with blank annunciators Removed Autofeather (AFX) annunciators and relocated to MFD. Remove AFX indicators for B300/B300C models only Add Rudder Boost Off Ann. for Model 300

NO YES X B B

32 Landing Gear No Change



SAMPLE DIFFERENCES TABLE DIFFERENCE AIRCRAFT: 300/300LW/B300/B300C with G1000 BASE AIRCRAFT: 300/300LW/B300/B300C (MDR NOTE (1) equipment only)

COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

33 Lights

Pilot and Copilot dimming control added to the overhead panel for EFIS display system brightness control.

NO NO X A A

34 Navigation

Install dual Garmin GIA 63W GPS/VHF Navigation receivers Turn Coordinator removed, pointer on PFD provides slip/skid indication GRS-77 AHRS source for Attitude data GDC-7400 ADC for Air Data. Collins TDR-94 tuning & Ident moves to PFDs. Added Standby AS & Alt. on RH Pitot System Overspeed Test removed(if installed), now part of GIA built-in-test. GWX-68 WX radar installed GCU-477 controls Nav Display on MFD. GTS-TAS/TCAS or TCAS II system. GDU contains TAWS A or B

NO YES FTD B B

34 Navigation

SVS selectable on PFD Display & transition. Formats differ for attitude scale, Reference Zero vs. Zero Pitch Line depiction and Flight Path Marker.

NO YES FFS C C

35 Oxygen No Change

36 Pneumatics No Change

37 Vacuum No Change

38 Waste / Water No Change


No Change


Optional datalink equipment available that provides XM data (GDL-59) or (GFDS)Garmin Flight Data Service International service (GDL-69). Also provided are the abilities to send and receive telephone calls and SMS text messaging

NO YES X A A


EFB , Electronic Charts, Airport Diagrams Selectable display format using GDU-1500. SAFETAXI not AMMD AC20-159 compliant.

NO YES FTD B B

49 APU No Change

52 Doors No Change

53 Fuselage Added (2) GPS antennae NO NO X A A

54 Nacelles/Pylons No Change


No Change

61 Propellers

Prop Syncroscope on MFD engine display. G1000 STC includes 4-Blade propeller airplanes only

NO NO X A A



SAMPLE DIFFERENCES TABLE DIFFERENCE AIRCRAFT: 300/300LW/B300/B300C with G1000 BASE AIRCRAFT: 300/300LW/B300/B300C (MDR NOTE (1) equipment only)

COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

72 Engine (turbine) No Change

73 Fuel Controls No Change

74 Engine Ignitions No Change

75 Engine Bleed Air No Change

76 Engine Controls No Change


Analog Engine Indicators replaced by engine indications on G1000 MFD AFX Indicators on MFD engine display

NO YES FTD C B

78 Exhaust No Change

79 Engine Oil No Change

80 Engine Starting

Analog Engine Indicators replaced by digital engine indications on G1000 Muti-Function Display (MFD) – ITT gauge changes scale during start sequence

NO YES FTD C B



5. Models B300/B300C with Proline 21 to Models B300/B300C with G1000 Definitions used in the ODR Tables:







DIFFERENCES TABLE DIFFERENCE AIRCRAFT: B300 / B300C with G1000 BASE AIRCRAFT: B300 / B300C with Proline 21

COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

General Airplane Configuration No Change

Weights Reduced Basic Operating Weight NO NO X A B

Limitations

New aircraft Limitations (See Airplane Flight Manual Supplement) NO YES X A A


New aircraft Placarding (See Airplane Flight Manual Supplement) NO NO X A A

Servicing

AFMS Section 8, new service & handling (ref. G1000/GFC 700 System Maint. Manual) NO YES X B B

Engines No Change

Flight Deck

Replace Collins ProLine 21 with G1000 Collins CDU & CCD replaced with GDU-477 NO YES FTD C C


• Collins dual PFD and single MFD changed to G1000 dual PFD single MFD.

• Collins Flight Guidance Panel removed and replaced with GMC 710 controller

• Removed Display Control Panels • Replaced standby ESIS with mechanical

standby AI, Altimeter and Airspeed • Standby instrument power switch moved to

instrument panel • Replaced audio panels outboard of PFD • Removed source select panel on lower

instrument panel.

NO YES FTD C C

Cabin No Change

Flight Controls Electric Trim has added speed schedule. YES NO X A A


Garmin Electronic Stability & Protection (ESP) Garmin Under Speed Proctection (USP) and Overspeed Protection Systems added (option)

YES YES FFS D C



DIFFERENCES TABLE

DIFFERENCE AIRCRAFT: B300 / B300C with G1000 BASE AIRCRAFT: B300 / B300C with Proline 21

COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

Preflight Avionics Preflight NO YES X B B

Engine Start Engine Gauges electronically displayed on the MFD. Format differs from ProLine 21. NO NO X B B

Taxi Taxi and Runup Checklist Procedures - See Airplane Flight Manual Supplement NO YES X B B

Takeoff Garmin PFD differs from Collins PFD format Garmin Speed Awareness cues. NO NO FTD B C

RTO Or V1 Fail

No Change

Climb Cruise Decent

No Change

In-Flight Maneuvers SVS function and use. ESP & USP function and use NO NO FFS C D


New PFD, MFD, FMS, Autopilot WAAS procedures, LNAV & LPV approaches NO YES FTD C D

Landing PFD Primary Flight Inst. with Vref on speed tape. RAD Alt & Mins on Altitude tape. NO NO X B B

Shutdown No Change

Normal Procedures See Airplane Flight Manual Supplement for review of all Normal Procedures NO YES FTD C C

Abnormal Procedures

See Airplane Flight Manual Supplement for new or changed Abnormal Procedures NO YES FTD C C


See Airplane Flight Manual Supplement for new or changed Emergency Procedures NO YES FTD C C



DIFFERENCES TABLE

DIFFERENCE AIRCRAFT: B300 / B300C with G1000 BASE AIRCRAFT: B300 / B300C with Proline 21

COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

21 Air Conditioning No Change

22 Auto-Flight

Collins autopilot replaced by Garmin GFC 700 autopilot with GMC 710 mode controller. RED Autopilot Disconnect on yoke now single stage switch for Trim, YD, RB, AP Rudder Boost using AP servo for Vmcg per Exemption 5599

YES YES FTD C C

22 Auto-Flight

Garmin ESP System software, default to ON Garmin USP System software AP coupled Go-Around only with ESP installed

YES YES FFS C D

23 Communications

Dual Garmin GIA 63W Communication Transceivers are installed Replaced Audio Control Panels with dual Garmin GMA 1347 audio panels outboard of each PFD. Emer. Freq. push button add on Center Pedestal RTU removed, GCU-477 provides function

NO YES X B B

24 Electrical Power

Individual Circuits & Circuit Breakers change with new labels and locations. (No circuit breaker source color code provide) Power Distribution for new systems (AFMS Sec.7) Standby battery powered items changed

NO YES X B B


Several New Avionics Racks behind instrument panel and in forward avionics bay NO NO X A A

26 Fire Protection No Change

27 Flight Controls Electric Pitch Trim speed schedule added YES NO X B A

28 Fuel No Change

29 Hydraulic No Change

30 Ice / Rain No Change

31 Indicating/Record Autofeather (AFX) annunciators removed. NO NO X B A

32 Landing Gear No Change

33 Lights

Pilot and Copilot dimming control added to the overhead panel for EFIS display system brightness control.

NO NO X A A

34 Navigation

Install dual Garmin GIA 63W GPS/VHF Navigation receivers GRS-77 AHRS source for Attitude data GDC-7400 ADC for Air Data. Transponder tuning & Ident moves to PFDs. GWX-68 WX radar installed GCU-477 controls Nav Display on MFD. GTS-TAS/TCAS or TCAS II system.

NO YES FTD B B




COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

GDU contains TAWS A or B ADF not integrated, ADF-60 on center pedestal. ESIS replaced with mechanical standby AI, Altimeter and Airspeed Indicator.

34 Navigation

SVS selectable on PFD Display & transition time. Formats differ for attitude scale, Reference Zero vs. Zero Pitch Line depiction and Flight Path Marker.

NO YES FFS C C

35 Oxygen No Change

36 Pneumatics No Change

37 Vacuum No Change

38 Waste / Water No Change


No Change


Optional datalink equipment available that provides XM data (GDL-59) or (GFDS) Garmin Flight Data Service International service (GDL-69). Also provided are the abilities to send and receive telephone calls and SMS text messaging

NO YES X A A


EFB , Electronic Charts, Airport Diagrams Selectable display format using GDU-1500 MFD. SAFETAXI not AMMD AC20-159 compliant.

NO YES FTD B B

49 APU No Change

52 Doors No Change

53 Fuselage Added (2) GPS antennae NO NO X A A

54 Nacelles/Pylons No Change


No Change

56 Windows No Change

57 Wings No Change

61 Propellers

G1000 STC includes 4-Blade propeller airplanes only NO NO X A A

71 Powerplant No Change

72 Engine (turbine) No Change

73 Fuel Controls No Change




COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

74 Engine Ignitions No Change

75 Engine Bleed Air No Change

76 Engine Controls No Change


Engine Indicators displayed on G1000 Multi-Function Display (MFD) in different format NO NO X B B

78 Exhaust No Change

79 Engine Oil No Change

80 Engine Starting

Engine indications on G1000 ITT gauge changes scale during start sequence NO NO X B B



6. Model BE-300 (Proline 21) to Model BE-300 (Proline Fusion) Definitions used in the ODR Tables:







Note: see Rockwell Collins, Pro Line Fusion Operator Differences, # RCA-9302

DIFFERENCES TABLE DIFFERENCE AIRCRAFT: BE-300 (Proline Fusion) BASE AIRCRAFT: BE-300 (Proline 21)

COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR


No Change

Weights

BOW reduced 12.3 lbs. by Proline Fusion NO NO X A A


No Change


No Change

Servicing

No Change

Engines

No Change

Flight Deck

Remove CDU replace with CCP & MKP NO YES FTD C C


Proline 21 AFD-3010 PFD/MFD displays replaced with Fusion AFD-3700 Touch Screen with FDSA-6500 Flight Display System Application. Minor PFD changes in presentation of EADI, EHSI, AS, Alt. Changes to MFD format to full, half, quarter display. Warning and Caution Annunciator Panels replaced with CAS Messaging

NO YES FTD C C

Cabin

No Change



No Change



DIFFERENCES TABLE

DIFFERENCE AIRCRAFT: BE-300 (Proline Fusion) BASE AIRCRAFT: BE-300 (Proline 21)

COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

Engine Start No Change

Preflight Reversionary Switches, Alternate Static, AFD-3700 Display Setup, ESIS, Radio Tuning, Ground Com/Ops, Flight Planning, Speed Bugs

NO NO FTD C B

Taxi No Change

Takeoff No Change

RTO Or V1 Fail

No Change

Climb Cruise Decent

No Change

In-Flight Maneuvers No Change


Instrument Approach Selection, Display Setup NO NO FTD B B

Landing No Change

Normal Procedures CAS Messages, NO NO AI A A

Abnormal Procedures

CAS Messages, Automatic Reversions, Miscompare, Display Tuning Fail, EIS Fail NO YES FTD B B


CAS Messages, Automatic Reversions NO NO AI A B



DIFFERENCES TABLE

DIFFERENCE AIRCRAFT: BE-300 (Proline Fusion) BASE AIRCRAFT: BE-300 (Proline 21)

COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

22 Auto-Flight

No Change, same Autopilot and Flight Control Panel as Proline 21.

23 Communications

RTU replaced by FUSION MKP Quick Tune Tool Bar, CCP Radio Tuning Knobs, Radio Tuning Window or Graphical Tuning Ground Comm/Ops.

NO NO AI A B

24 Electrical Power

Battery 3 positions switch for Ground Ops. NO NO AI A B


Warning & Caution Annunciator Panels replace by 17 Emergency, 65 Abnormal, 56 Advisory, 11 Status CAS Messages, plus 4 EIS Indications, CAS Message Inhibits

NO YES AI B B

33 Lights

Display back lighting & control NO NO X A A

34 Navigation

FMS CDUs removed, Navigation Tuning & Setup by 1-Multifunction Keypad Panel (MKP). 2-Cursor Control Panel CCP-3500 and Multifunction Windows on AFD-3700

NO YES FTD C C

34 Navigation

Alternate Static Selection moved to Reversionary Panel. Altimeter Baro Setting by Baro 2-SKP Wx Radar Control on PFD Menu & Radar Tilt by 2-Single Knob Panel SKP-3500. TCAS II Control on Radio Tuning Window ATC Transponder on Radio Tune Window DBU-4100/5000 remove, Data entry on Bezel of AFS-3700s

NO NO AI B B

34 Navigation

Electronic Standby Instrument System GH-3100 replaced by DU42 on Glareshield

NO NO AI B B

34 Navigation

SVS selectable on PFD Display Format appearance differs for attitude scale, Reference Zero vs. Zero Pitch

NO NO FTD B B


Each AFS-3700 has own maintenance function available only on ground. NO NO X A A


FSA-6000 File Server Application must be active on all 3 AFD-3700. PFD viewing distance of ~ 24 in. and MFD viewing distance of ~ 28 in. necessitate zooming and panning to meet minimum readable font size at that distance. XM and Universal Wx are simultaneously available but not simultaneous display.

NO YES FTD C B

No other system changes associated with Proline Fusion installation



7. Model BE-1900/1900C to Model BE-1900D Definitions used in the ODR Tables:

X .......... Pilot’s Operating Handbook and / or Flight Manual Supplement




FTD .... Flight Training Device (FTD Level I or II)



DIFFERENCE AIRCRAFT: BE-1900D

BASE AIRCRAFT: BE-1900/1900C

COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR


1900/1900C Part 23 & SFAR 41 1900D Part 23 Commuter Category Yes Yes X A B

Weights

Weights vary slightly by model and modification status, including GW increase No No X A B


Numerous changes in system design to address Rotor Burst criteria. Changed Fatigue

Life.

No No X A B


Different Placards listed in AFM/POH No No X A B

Servicing

Similar

Engines

1900/1900C has PT6A-65B 1900D has PT6A-67D

Yes Yes X B B

Flight Deck

Wide center pedestal, Revise Overhead Panel, Various Instrument Panel Changes No No X A B


1900D has Collins EFIS-84 No Yes FFS C C

Cabin

New interior design but same max. pax. configuration. No No X A B

Flight Controls 1900D adds Aileron Rudder interconnect and Rudder Boost option.

1900/1900C has Power Steering option

Yes Yes X B B


1900/1900C have 4 position Flaps 1900D has 3 position Flaps Yes Yes FFS C C






COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

Preflight Various Exterior, Interior and Cockpit changes No Yes X B B

Engine Start Start procedures and characteristics No Yes X B B

Taxi Early 1900/1900C had Power Steering Yes Yes X B B

Takeoff 1900/1900C Takeoff Distance is to 50 ft. with no Accelerate Stop consideration.

1900D Takeoff Distance is to 35 ft. and considers factors listed in AFM

1900D has Reduced Power Takeoff

Yes Yes FFS C C

RTO Or

V1 Fail

1900D has Accelerate/Stop Performance and Takeoff Flight Path gradient required. Yes Yes X B B

Climb Cruise Decent

1900D Performance includes Takeoff Flight Path requirements. Yes Yes X B B


EFIS-84 navigation information display Yes Yes FFS C C

Landing Use of Vref for landing and Balked Landing Yes Yes X B B

Normal Procedures

Preflight, Takeoff, Landing, Go-Around Yes Yes FFS C C

Abnormal Procedures

EFIS-84 Reversion/Composite/FD No Yes FFS C C


Aircraft Performance Profile and various Emergency Procedures No Yes X B B

In-Flight Maneuvers

Similar






COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

21 Air Conditioning

Increased Max Differential Pressure and changes to Bleed Air, Environmental Air and Pressurization

components. No No X B B

22 Auto-Flight

1900D optional APS-65 Autopilot 1900C optional SPZ-2000 or SPI-4000 No Yes X B B

23 Communications

Upgraded Collins Comm Radios & CVR No No X A A

24 Electrical Power

Dual AC Buss System No Yes X B B


New Interior No No X A A

26 Fire Protection

Changes in Firewall and Aft Nacelle No No X A A

27 Flight Controls

Add Aileron Rudder interconnect and Rudder Boost option. Dual Pushrod Trim Tabs, Optional Electric Trim

without AP

Yes Yes X B B

28 Fuel

1900 fuel system has bladder fuel cells, 1900C fuel system changes to wet wings,

1900D has changes to fuel venting to accommodate wing tip extension.

No No X A A

29 Hydraulic

Similar

30 Ice / Rain

Additional Deice Boot coverage, Deice Annunciators & Pitot Heat Annunciator System. No Yes X B B


Upgrade FDR standard, Revised Annunciator Panel, No No X A A

32 Landing Gear

Revise Gear Position Indicators (various) No No X A A

33 Lights

Add Dual Position Lights, New EL Panel Lighting No Yes X B B

34 Navigation

Upgraded Collins Nav Radios and EFIS-84 Displays, Standby Attitude Indicator Yes Yes FFS C C

35 Oxygen

New Crew Mask Container and Mask Mic. No Yes FTD B B

36 Pneumatics

Changes in Bleed Air Pressure and Vacuum readings No Yes X A A

37 Vacuum

Vacuum Flight Instruments removed on Right Side No Yes X B B

38 Waste / Water

NA

45 Maintenance

Computer

NA


NA

49 APU

NA

52 Doors

Larger Airstair, Cargo and Emer Exit Doors No No X A A






COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

53 Fuselage

Oval Cabin Shape for Standup Cabin No No X A A

54 Nacelles/Pylons

Changed Nacelle Firewall and Aft Nacelle No No X A A

55 Horizontal & Vertical

Stab.

Twin Ventral Fins and larger Tailets Yes No X B B

56 Windows

Taller cabin windows and New cockpit sun visor. No No X A A

57 Wings

Wing tip extensions and winglets, vortex generators on outboard flaps No No X A A

61 Propellers

Composite blade construction with nickel leading edge. No No X A A

71 Powerplant

New engine truss and New Autofeather annunciations No Yes X B B

72 Engine (turbine)

PT6A-67D engines (PT6A-65B 1900/1900C) No Yes X B B

73 Fuel Controls

PT6A-67D has Duplex Fuel nozzles No No X A B

74 Engine Ignitions

Similar

75 Engine Bleed Air

Similar

76 Engine Controls

Similar


Similar

78 Exhaust

Larger constant area Exhaust Stacks and Heat Dissipation Concerns. No No X A A

79 Engine Oil

Similar

80 Engine Starting

Similar



8. Model BE-1900D to Model BE-1900/1900C Definitions used in the ODR Tables:








DIFFERENCE AIRCRAFT: BE-1900/1900C

BASE AIRCRAFT: BE-1900D

COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR


1900/1900C Part 23 & SFAR 41 1900D Part 23 Commuter Category Yes Yes X A B

Weights

Weights vary slightly by model and modification status, including GW increase No No X A B


Numerous changes in system design. Changed Fatigue Life.

No No X A B


Different Placards listed in AFM/POH No No X A B

Servicing

Similar

Engines

1900/1900C has PT6A-65B 1900D has PT6A-67D

Yes Yes X B B

Flight Deck

Narrow center pedestal, Revise Overhead Panel, Various Instrument Panel Changes No No X A B


1900C has mechanical Flight Instruments No Yes FTD B B

Cabin

New interior design but same max. pax. configuration. No No X A B

Flight Controls 1900C has no Rudder Boost. 1900/1900C has Power Steering option

Yes Yes X B B


1900/1900C have 4 position Flaps 1900D has 3 position Flaps Yes Yes X A B






COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

Preflight Various Exterior, Interior and Cockpit changes No Yes X B B

Engine Start Start procedures and characteristics No Yes X B B

Taxi Early 1900/1900C had Power Steering Yes Yes X B B

Takeoff 1900/1900C Takeoff Distance is to 50 ft. with no Accelerate Stop consideration.

1900D Takeoff Distance is to 35 ft. and considers factors listed in AFM

Yes Yes B B B

RTO Or

V1 Fail

1900C has no Accelerate/Stop Performance and Takeoff Flight Path gradient required. Yes Yes X B B

Climb Cruise Decent

No Takeoff Flight Path requirements. Yes Yes X B B


Mechanical navigation information display Yes Yes FTD B B

Landing No Vref for landing No Yes X B B

Normal Procedures

Preflight, Takeoff, Landing, Go-Around Yes Yes X B B

Abnormal Procedures

Similar No No X A A


Aircraft Performance Profile and various Emergency Procedures No Yes X B B

In-Flight Maneuvers

Similar






COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

21 Air Conditioning

Decreased Max Differential Pressure and changes to Bleed Air, Environmental Air and Pressurization

components. No No X B B

22 Auto-Flight

1900D optional APS-65 Autopilot 1900C optional SPZ-2000 or SPI-4000 No Yes X B B

23 Communications

Different Collins Comm Radios & CVR No No X A A

24 Electrical Power

Single AC Buss System No Yes X B B


Different Interior No No X A A

26 Fire Protection

Changes in Firewall and Aft Nacelle No No X A A

27 Flight Controls

No Rudder Boost option. 4 Flap Settings Yes Yes X B B

28 Fuel

1900 fuel system has bladder fuel cells, 1900C fuel system changes to wet wings,

changes to fuel venting for wing tip difference. No No X A A

29 Hydraulic

Similar

30 Ice / Rain

Different Deice Boot coverage, Deice Annunciators & Pitot Heat Annunciator System. No Yes X B B


Different FDR standard and Annunciator Panel, No No X A A

32 Landing Gear

Gear Position Indicators (various) No No X A A

33 Lights

Different cockpit lighting No Yes X A A

34 Navigation

Different Collins Nav Radios and Mechanical Displays, No Standby Attitude Indicator Yes Yes FTD B B

35 Oxygen

Crew Mask Container and Mask Mic. No Yes FTD B B

36 Pneumatics

Changes in Bleed Air Pressure and Vacuum readings No Yes X A A

37 Vacuum

Vacuum Flight Instruments on Right Side No Yes X B B

38 Waste / Water

NA

45 Maintenance Com

NA


NA

49 APU

NA

52 Doors

Smaller Airstair, Cargo and Emer Exit Doors No No X A A

53 Fuselage

Round Cabin Shape no standup height No No X A A






COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

54 Nacelles/Pylons

Changed Nacelle Firewall and Aft Nacelle No No X A A


Stab.

Single Ventral Fins and smaller Tailets Yes No X A A

56 Windows

Smaller cabin windows and cockpit sun visor. No No X A A

57 Wings

Smaller Wing Tips, no winglets No No X A A

61 Propellers

Metal Propeller Blades. No No X A A

71 Powerplant

Different engine truss and Autofeather annunciations No Yes X B B

72 Engine (turbine)

PT6A-65B 1900/1900C No Yes X B B

73 Fuel Controls

No Duplex Fuel nozzles No No X A B

74 Engine Ignitions

Similar

75 Engine Bleed Air

Similar

76 Engine Controls

Similar


Similar

78 Exhaust

Smaller Exhaust Stacks No No X A A

79 Engine Oil

Similar

80 Engine Starting

Similar



9. Model 1900D EFIS-84 to Model 1900D G950 Definitions used in the ODR Tables:





FBS .... Fixed Base Simulator (FTD Level II)




DIFFERENCE AIRCRAFT: 1900D G950

BASE AIRCRAFT: 1900D EFIS-84

COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR


Garmin G950 integrated flight deck PFD/MFD replaces existing EFIS 84 EADI’s & EHSI’s along with

all analog flight & engine instruments. Systems indicators located in the lower panels are retained,

including flaps & fuel quantity indicators.

NO YES FTD B C

Weights

Revised W&B / Equipment List NO NO X A A

Limitations

Limitations related to the avionics/Flt Inst KOEL change to G950 system

Limits for Class A TAWS, TCAS-1, GPS WAAS, RNP-4 & LPV

NO YES AI B B

Placards and Markings New Placard Formats replace existing placards. NO NO X A A

Servicing

No Change

Engines

No Change

Flight Deck

Replace EFIS-84, Mechanical Flt/Eng Inst., FDC-65, Alt Alerter & Proline 2 Radios with G950 System.

XM WX Data (optional) GSR-56 Iridium Satcom (optional)

Excludes FCS-65 Autopilot interface

NO YES FTD C C

Cabin

No Change


Aerodynamic Controls No Change


G950 PFD/MFD format replaces all Primary Flight Inst, & Engine Inst.

G950 PFD includes SVS GDU reversion controlled by GMA-1347 Display

Backup button. Lower Inst. Panel switches unchanged

Change from dual Collins EFIS 84, Mechanical Flt/Eng

indicators, Collins FDC-65 Flight Director, Collins Proline 2 radios to Garmin G950 Integrated flight

NO YES FTD C C






COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

deck system. • Changed from EADI/EHSI EFIS

84 & Mechanical Primary Flight Inst. to dual PFD (GDU-1040)

• RMI Removed, Bearing on PFD • Engine Instruments now displayed on MFD

(GDU-1500) • Replaced mechanical Standby Attitude Indicator with 3 in one standby display (MD302)

• Prop synch moved to MFD • FDC-65 Flight Director

Controllers replaced with GMC-710 FDC top center instrument panel

• MFD controller (GCU-477) on left forward center pedestal

• Proline 2 audio replaced by 2 (GMA-1347) audio panels outboard of PFD’s

• Yaw Damper self-test relocated to center pedestal switch with annunciation on PFD

• GWX-70 Weather Radar displayed on MFD • AFX displayed in engine instrument

grouping of the MFD. • Altitude Alerter moved to G950

PFD and FD using GMC-710. • System adds synthetic vision and

HITS displays (optional) • Garmin GPS400 replaced by

G950 system WAAS GPS • Garmin GDU-1500 integrated TAWS Class

A installed exclusively






COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

Preflight G950 Cockpit Preflight Procedures NO YES AI B B

Before Start Electrical Power Procedures, Busing, Standby Power & Displays.

Delete EFIS-84 checks NO YES AI B B

Engine Start Electronic Engine Gauges on MFD NO YES FTD B C

After Start & Taxi G950 System Checks NO YES FTD B B

Takeoff G950 PFD/MFD setup, V-speeds. PFD/MFD Inst reference for Takeoff NO YES FTD B C

RTO Or

V1 Fail

PFD airspeed & attitude reference MFD Engine indications NO NO FTD B C

Climb Cruise Decent

Flight Director Use, LSA Altitude Alerter Use

Navigation, Nav Source, FD NO YES FTD B C

In-Flight Maneuvers Maneuvers affected by PFD Flight Inst. (Steep Turns, Stall LSA, FD, Navigation) NO NO FFS D C


Flight Plan selection procedures Approach selection, activation, FD use

LNAV/VNAV & LPV approach procedures NO YES FFS D C

Landing PFD Inst. reference & setting V-speeds MFD Engine Inst. reference NO YES FTD B B

Shutdown G950 Display shutdown procedures NO YES FTD B B

Normal Procedures AFMS Procedures for G950 Display System, TCAS, TAWS NO YES FFS D C

Abnormal Procedures AFMS Procedures for G950 Display System, TCAS, TAWS NO YES FTD B B

Emergency Procedures AFMS Procedures for G950 Display System, TCAS, TAWS NO YES FTD C C






COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

21 Air Conditioning

No Change

22 Auto-Flight

FYD-65 Yaw Damper retained with YD Test moved to center console button.

ICU Converter added to interface with existing FYD-65.

FCS-65 not approved with this STC. CWS button on yoke

FCP-65 FD Controller replace with 1 GCU-710 top center instrument panel

NO YES AI B B

23 Communications

G950 Dual VHF (GIA-63W) replace Proline 2 radios,

tuned with DCP on GDU-1040s Abnormal Tuning Procedures added

GMA-1327 audio panels replace Proline 2 audio panels

Cohbam Model 240 provides PA system for GMA-1347 Audio Panels & cabin briefer.

NO YES FTD B C

24 Electrical Power

115VAC/400HZ remains but no G950 use

Changes to CB Panel AHRS/ADC/PFD/MFD/GEA power sources

Each PFD has own PS-835 Standby Battery & Standby Battery Switch.

RH AC Bus Transfer removed.

NO NO X A B

27 Flight Controls

Interface Control added for YD/RB function convert digital to analog signal. NO NO X A B


AFX Green Ann. on MFD b/w ITT & Torq Prop Syncphaser indicator on MFD.

YD Ann. on PFD PFD/MFD cooling fan functions added

G950 interfaces with L3 FDR & CVR New Annunciator Switches for Prop Sync & Emer

Freq along with Dimming Selection

NO NO AI B B

33 Lights

G950 Internal Display lighting Existing Cockpit Lighting control function NO NO AI B B

34 Navigation

PFD Display Format replace Basic T Dual G950 VHF Navs

Single ADF, DME & RAD ALT on G950 interface NO YES FFS D C

34 Navigation

Navigation Display & Flight Plan Dual GPS WAAS with GIA-63A, w/ RNP-4

LNAV/VNAV & LPV Approaches NO YES FFS D C

34 Navigation

G950 integrated ADC (GDC-7400) with Pitot/Static interface changes.

Baro-set & Alt. Alerter LSA on speed tape

Tape Altimeter & VS G950 integrated ADHRS (GRC-77)

NO YES FTD C C

34 Navigation

GTX-33 Transponder controlled by PFD DCP or GDU-477.

Collins DME-42 retained w/ G950 display Collins ADF-462 retained w/ bearing on PFDs

RAC-870 Converter installed to retain Collins ALT-55 RAD ALT on PFD

WX RDR (GWX-70) TCAS (GTS-855)

TAWS Class A integrated in G950 PFD/MFD.

NO YES AI B B


G950 EFB Functions IAP only, no Enroute Charts

Emergency Power Chart availability NO YES FTD

ICBT B C






COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

XM WX Data (GDL-69A)

53 Fuselage

Add GPS WAAS antennas, XM Antenna, and 2 OAT Probes NO NO X A B

61 Propellers

Propeller Synchrophase Indication on MFD Propeller Synchrophase Switch now PB

AFX Green Ann. on MFD NO NO X A B


The engine instruments were independent analog instruments and are now indications included in the Garmin G950 using 2 GEA-71 engine/airframe

data concentrators with Signal Conditioners.

Eng. Inst. Primary display is in the MFD with reversionary displays in the PFD’s.

Engine displays include: Prop RPM X 2 Torque X 2

Turbine speed X 2 Turbine Temperature X 2

Fuel Flow X 2 Engine oil pressure X 2

Engine oil Temperature X 2 The engine displays include alerting for operation

outside normal ranges.

AFX indication above each torque Indicator

Prop Sync indication is between RPM ind.

Engine indication for ITT rescales for starting and once the engine is started, displays normal scaling

NO YES FTD B C

80 Engine Starting

Engine starting is unchanged except where impacted by Engine Indicating and Electrical Power distribution

procedures.



10. Model 1900D with Proline 2 (EFIS-84) to Model 1900D with IDS-3000 Definitions used in the ODR Tables:







SAMPLE DIFFERENCES REQUIREMENTS TABLE

DIFFERENCE AIRCRAFT: 1900D with IDS-3000

BASE AIRCRAFT: 1900D with Proline 2 (EFIS-84)

COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR


No Change

Weights

Change in BOW and equipment list NO NO X A B


Limitations for IDS-3000 Engine Display Markings NO NO X B B


No Change

Servicing

No Change

Engines

No Change

Flight Deck

Center Pedestal extended aft to accommodate relocation of radio controls, CHP, Mode Select Panel

and MFD control NO YES AI A B


Install IDS-3000 PFD1, PFD2, and MFD. Removal EFIS-84 flight instruments. Remove analog engine indications.

Relocated following from Instrument Panel to Center Pedestal:

(1) #1&#2 FCP-65 Control Panel, (2)#1 & #2 VHF NAV/Com Transceiver Control Head,

(3) #1 & #2 ADF Control Head, (4) Transponder Control Head,

(5) TCAS Control Head. Add Audio Panel with Compass Control and PFD

dimming Add Reversionary Panel with MFD dimming, Gnd Comm Pwr, AP select, TCAS, DME Vol., intercom,

Rad Alt., Xpdr & Prop Sync. Add 2 Display Control Panels with Integrated

Altitude Alerter

NO MINOR AI FTD ICBT B B







COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

Preflight PFD/MFD power distribution. NO YES FTD B B

Engine Start Use of MFD Engine Display and PFD/MFD power distribution. NO YES FTD B B

Taxi Flight Instrument checks. NO YES FTD B C

Takeoff V-speed and Altitude Selection. Airspeed Indication on tape format. NO YES FTD B C

RTO Or

V1 Fail

Airspeed Indication on tape format. Attitude indications on PFD format.

Low Speed Awareness cues.

NO YES FTD B C

Climb Cruise Decent

PFD format for all flight instruments. Low Speed Awareness cues.

Selection and use of Nav Sources.

NO YES FTD B C


Nav Source Selection & display format. LNAV, LNAV/VNAV & LPV approaches NO YES FFS D C

Landing V-speed and Altitude Selection. Airspeed Indication on tape format. NO YES FTD B C

Normal Procedures

Nav Source selection, Nav Display format, Autopilot & FD control.

IFIS-5000 use procedures. TCAS & TAWS use procedures.

NO YES FFS C C

Abnormal Procedures

Abnormal procedures for Avionics / Flight Instruments of IDS-3000 system.

NO YES FTD B B


Emergency procedures for Dual Generator Failure, AC Inverter Failures, Emergency Power

Management, and Standby Flight Instruments.

NO YES FTD C C

In-Flight Maneuvers

Tape format & Low Speed Awareness for Steep Turns and Stalls.

NO YES FFS D C






COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

21 Air Conditioning

No Change

22 Auto-Flight

Original Collins APS-65 Autopilot is retained adding dual AHRS monitoring,

Autopilot Mode Annunciation and Disconnect Annunciation now on PFD.

AP/FD Flight Control Panel & Remote Mode Annunciator Panel moved from above EADI to forward

Center Pedestal. AP/FD couple arrow not functional for AP.

AP selector on Reversionary Panel. Dual FD installation

YD annunciation

NO YES AI B B

23 Communications

VHF Com, VHF Nav, ADF, XPDR & TCAS Control Heads relocated to pedestal

NO NO X A A

24 Electrical Power

Add Emergency Power sources control panel on top center instrument panel.

Add PS-835 Emergency Power Supplies for emergency power of PFD1 & MFD

Normal PFD1 and MFD power #2 avionics buss, Normal PFD 2 power Rht. Gen Buss.

Standby Horizon Power & lighting remains. Circuit Breaker Panel changes & additions.

115 V AC no longer utilized by aircraft. 26 V AC remains for FD, AP, Radar Stab.

NO YES AI B B


No Change

26 Fire Protection

Engine Fire Indication added to Engine Display inside TRQ/ITT indicator. NO NO X A A

27 Flight Controls

No Change

28 Fuel

No Change

29 Hydraulic

No Change

30 Ice / Rain

Low Speed Awareness for Icing conditions requires use of REFS Vt selected to 160 kts. No Low Speed

Awareness automated adjustment for icing conditions included.

NO YES AI B B

31

Indicating/Record

No Changes to main Annunciator Panels

Remote Annunciators changed, removed or relocated: • AFX green remote annunciation is now on MFD

Engine Display inside TRQ/ITT/ • Autopilot Disconnect and Mode annunciation is

now on PFD. • GPWS/EGPWS annunciators relocated above

PFD1&PFD2 on Remote Ann. Panel • TCAS annunciation now on PFD/MFD

• FDR status annunciation moved to remote annunciator panel above PFD1.

NO YES AI B B






COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

• FD/AP/YD mode Remote Annunciator Panel moved to center pedestal with FCP-65 relocation.

Flight Control Annunciations are duplicated on PFD1 & PFD2.

• Reversion annunciation is on PFD.

32 Landing Gear

Protrusion of Parking Brake Knob through the Center Pedestal Cover creates potential for inadvertent

release of Parking Brake.

NO NO AI B B

33 Lights

Cockpit lighting control changes to multiple dimming controls. PFD dimming on Audio Panel, MFD dimming

on Reversion Panel. Minor changes in EL Panel format & labels

NO YES X B B

34 Flight Instruments

EADI/EHSI CRT EFIS displays replaced by 8x10” LCD PFD EFIS displays.

Separate EADI & EHSI replaced with composite PFD format.

NORM or FREE Heading slave mode control relocated to Audio Panel.

Analog Flight Instruments replaced with composite PFD format.

Separate mechanical pneumatic Airspeed, Altimeter & Vertical Speed replaced with composite PFD format.

RMI removed, bearing selections displayed on composite PFD format.

New EFIS format / control / selections • 2 Display Control Panels (DCP) for PFD

• 1 Course Heading Panel (CHP), • 2 Digital Interface Units (DIU),

• 1 Cursor Control Panels (CCP) for MFD

NO YES FTD C C


Add Dual Garmin GPS400W required. (GPS1 & GPS2) Navigation Display available on lower composite PFD

format and on MFD. Add LNAV, LNAV/VNAV & LPV Approach capability. No

Baro-VNAV.

NO YES FTD C C


Install Dual ADC-85 Air Data Computers. Add Low Speed Awareness to speed tape.

Altitude Baro Set is provided on DCP. Altitude Alerter/Pre-selector Controller is provided on

DCP.

NO YES FTD A B


Collins TCAS-4000 (TCAS II) display is selectable to PFD and MFD.

WX Radar only selectable to MFD. Honeywell Mk 6 TAWS (TAWS B only) Class B only

because no Terrain Display.

NO YES FTD A B

35 Oxygen

No Change

36 Pneumatics

No Change

37 Vacuum

No Change

38 Waste / Water

No Change






COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

45 Maintenance

Computer

No Change


IFIS-5000 installed for Electronic Charts and/or Graphical Weather.

IFIS-5000 is not linked to Flight Plan. Chart selection is workload intensive using rotary knob

on CCP. Own-Ship-Position is available on IFIS-5000 provided

graphics.

NO YES FTD ICBT B C

49 APU

NA

52 Doors

No Change

53 Fuselage

Add 2 exterior antennas for GPS/XM. NO NO X A B

54 Nacelles/Pylons

No Change


Stab.

No Change

56 Windows

No Change

57 Wings

No Change

61 Propellers

Propeller Synchronization switch is relocated to Reversionary Panel.

Propeller Syncrophaser is indicated on Engine Display. AFX green annunciation added to Engine Display

replacing remote annunciators.

NO NO X A B

72 Engine (turbine)

No Change

73 Fuel Controls

No Change

74 Engine Ignitions

No Change

75 Engine Bleed Air

No Change

76 Engine Controls

No Change


Separate Analog Engine Instruments replaced Engine Display. (Normal on MFD, Reversion on PFD)

Exceedences are annunciated in Red. Abnormal indications are annunciated in Amber.

Primary for power Torque and ITT combined round dial gauge & digital display,

Propeller RPM is round dial gauge & digital display: N1 is round dial gauge & digital display.

Fuel Flow, Oil Pressure & Oil Temp are digital only. AC powered Torque Indicators are replaced with self

generating torque sending units. Placement and function of DCUs & EDUs (2 each)

NO YES FTD B C






COMPLIANCE METHOD

TRAINING CHKG/CURR


PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

80 Engine Starting

Engine Instruments on EIS of MFD NO NO AI B B

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