HBC BE90-200ALLOSDFC-01 Document Reference

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

Operational Suitability Data (OSD) Flight Crew

Hawker Beechcraft BE90/200 Series (90/99/100/200)

Models BE-200/B200, BE-C90A/B/GT, BE-C90/90-1, BE-E90, BE- F90/F90-1, BE-90/A90/B90, BE-200PL21/B200GT/250, and BE- C90GTi/C90GTx

19 November 2015

Operational Suitability Data – Flight Crew BE90/200

Hawker Beechcraft BE90/200 Series

Operational Suitability Data (OSD) – Flight Crew

Revision Record

Revision No. Content Date

OSD FC Initial evaluation of the BE90/200 series aircraft 19 Nov 2015 Initial Issue

OSD FC BE90/200 – Initial Issue Page 2 of 22 Operational Suitability Data – Flight Crew BE90/200

Contents

Revision Record ...... 2 Content ...... 3 Acronyms ...... 4 Preamble ...... 6 1. Introduction ...... 6 2. Operational Evaluation BE90/200 Series (90/99/100/200) ...... 6 Operational Suitability Data (OSD) – Flight Crew ...... 7 1. Aircraft Type Designation and Pilot Licence Endorsement ...... 7 2. Aircraft Specifics ...... 7 2.1 Aircraft Approach Category ...... 8 2.2 Part-CAT, Subpart D – Instruments, Data, Equipment ...... 8 2.3 Electronic Flight Bag (EFB) ...... 9 3. Operator Differences Requirements (ODR) ...... 9 4. Master Differences Requirements (MDR) ...... 10 4.1 MDR tables for the Model 200 normal, commuter and restricted categories ...... 10 4.2 MDR tables for the BE90/200 series variants C90GTi/GTx, C90A/B/GT, C90/90-1, E90, F90/F90-1, 90/A90/B90, 200/B200, B200PL21/B200GT, and 250 ...... 11 5. Specifications for Pilot Training ...... 11 5.1. BE90/200 Initial Type Rating Training ...... 11 5.2. BE90/200 Initial Type Rating Training with Credit for Commonality ...... 12 5.3 Familiarisation Training between BE90/200 Series variants ...... 12 5.4 Training Areas of Special Emphasis (TASE) ...... 13 6. Recurrent Training ...... 14 7. Specification for Checking ...... 14 7.1. Line Checks ...... 15 8. Specifications for Recent Experience and Currency...... 15 8.1. Recent Experience ...... 15 8.2. Currency ...... 15 9. Line Flying Under Supervision (LIFUS) / Supervised Operating Experience (SOE)... 16 9.1 LIFUS / SOE following BE90/200 Initial Type Rating Training ...... 16

Appendix 1: Initial Type Rating Training for BE90/200 Series ...... 17

Appendix 2: ODR Tables for Model 200 Normal Category to Model 200 Commuter Category ..... 19

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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)

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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

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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 BE90/200 Series (90/99/100/200)

The BE90/200 series aircraft 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 BE90/200 models was conducted by EASA as a catch-up evaluation. The evaluation included an analysis of the corresponding FAA FSB report for the BE-200 of 12 June 2013, a review of an EASA approved syllabus for initial type rating of the Beechcraft 90/200 Series (BE90/99/100/200) dated 03 March 2015, 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).

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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 BE90/200 series aircraft have been evaluated for aircraft categorisation and license endorsement. The following HBC models are classified as high performance aeroplanes and within the same type rating: Models BE-200/B200, BE-C90A/B/GT, BE-C90/90-1, BE-E90, BE-F90/F90-1, BE- 90/A90/B90, BE-200PL21/B200GT/250, and BE-C90GTi/C90GTx.

The license endorsement is established as "BE90/99/100/200".

SP / OEB FC Aircraft License REPORT / Manufacturer Variants Complex SP HPA / Remarks Model / Name Endorsement OSD FC MP available Hawker BE-200/B200 BE90/99/100/200 X X SP HPA X OSD FC BE90/200, Beechcraft BE-C90A/B/GT dated 19 Nov 2015 Corporation BE-C90/90-1 BE-E90 BE-F90/F90-1 BE-90/A90/B90 BE-200PL21/B200GT/250 BE-C90GTi/C90GTx

2. Aircraft Specifics

Model 200 Restricted Category Each Restricted Category airplane has different performance capabilities and limitations. These different configurations can have significant effect on performance. Model 200T and 200CT represents an example of significant performance detriment in Restricted Category Model 200s. Restricted Category Model 200 configurations can be very sluggish and sensitive to airspeed deterioration when flaps and gear are down with substantial power application necessary to maintain or correct airspeed. Restricted Category airplanes have significantly reduced performance on takeoff with an engine failure at increased gross weights. Some Restricted Category AFM Limitations restrict sink rate for landing touchdown because of increased gross weight.

Model 200 Commuter Category STC The Commuter Category STC Model 200 aircraft is a complex, high performance, turboprop aircraft powered by 2 P&W PT6A-41, -42, -52, -61 engines with 850 shp.

Commuter Category STC Model 200s differ from Normal Category Model 200s by maximum takeoff weight of 13,420 lbs but limited to 9 or less passengers, commuter category performance and requisite design changes to meet commuter category certification standards. Maximum landing weight is unchanged at 12,500 lbs. which establishes the maximum takeoff weight due to 25% of total fuel capacity for certification purposes. System changes include Takeoff Trim Warning, Over-Speed Warning, Engine Fire Extinguisher, Stall Warning Ice Mode, Emergency Cabin

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Lighting and Escape Path Markings to meet commuter category requirements. Various Flight Instrument Systems remain the same as certified in the Normal Category Model 200s but with Flight Hazard Assessment (FHA) to a more stringent design assurance level for Commuter Category.

The primary differences for the Commuter Category STC Model 200 from the Normal Category Model 200 are dictated by handling procedure changes resulting from commuter category performance requirements. The commuter category performance and procedures along with additional safety related equipment substantially improve the operating safety margins for the Commuter Category STC Model 200 airplanes.

The same pilot type rating between Restricted Category and Commuter Category is maintained because although Restricted Category airplanes vary widely in performance capabilities and limitations, in cases where Restricted Category airplanes are certified to ICAO Annex 8 the performance and handling will be nearly identical.

B200GT / King Air 250

The B200GT evolved from the B200 by the installation of new PT6A-52 engines. The PT6A-52 was derived by mating the turbine section of the 1,050-shp capable PT6A-60A found on the BE-300 with the existing B200 PT6A-42 gearbox. The result is an engine that holds its 850-shp flat rating to a much higher altitude, improving climb and cruise performance under almost all flight conditions. The King Air 250 is the designation of the B200GT with four STCs embodied: a Raisbeck Ram Air Recovery System, Boundary Layer Research (BLR) Winglets, a Hartzell Composite Propeller, and a BLR Ultimate Performance Package.

2.1 Aircraft Approach Category

With reference to Part-CAT, CAT.OP.MPA.320(b) the minimum straight-in approach category for the BE900/200 series aircraft is as follows:

Aircraft Category

BE90/200 Series 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.

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2.3 Electronic Flight Bag (EFB)

Electronic Checklists

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.

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.

G1000 Only: Electronic Approach Charts (SIDS, STARS, Approach Charts & Airport Diagrams) are available 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 softkeys 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.

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4. Master Differences Requirements (MDR) [M]

MDR tables for the above variants are shown below. Definitions of the various levels for Training / Checking / Currency are those used in CS-FCD.

4.1 MDR tables for the Model 200 normal, commuter and restricted categories

The following MDR table applies between the Model 200 normal, commuter and restricted categories:

Master Differences Requirement (MDR) Table

FROM AIRCRAFT

Model 200 Model 200 Model 200 (normal) (commuter) (restricted)

Model 200 B / A / B B / A / B B / C / B (normal) (1)(2)(3)(4)(5) (1)(2)(3)(4)(5) (1)(2)(3)(4)(5)

Model 200 D / D / D B / A / B D / D / D (commuter) (1)(2)(3)(4)(5) (1)(2)(3)(4)(5) (1)(2)(3)(4)(5)(6) TO AIRCRAFT

Model 200 D / D / D D / D / D not evaluated (restricted) (1)(2)(3)(4)(5) (1)(2)(3)(4)(5)(6) (1)(2)(3)(4)(5)(6)

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-2000 ON EFIS 85 aircraft is D/C/C. (5) Installation of GARMIN G1000 is D/C/D. (6) Restricted Category differences may be less than designated based on similarity of special purpose equipage. ICAO Annex 8 compliant Restricted Category differences may be less than designated for Normal Category based on similarity of special purpose equipage.

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4.2 MDR tables for the BE90/200 series variants C90GTi/GTx, C90A/B/GT, C90/90-1, E90, F90/F90-1, 90/A90/B90, 200/B200, B200PL21/B200GT, and 250 [M]

Difference levels between BE90/200 Series variants are defined as difference level B / B / B for training, checking and currency between the following variants: • C90GTi/GTx • C90A/B/GT • C90/90-1 • E90 • F90/F90-1 • 90/A90/B90 • 200/B200 • B200PL21/B200GT • 250

Level B checking consists of an oral or written examination.

Level B 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.

5. Specifications for Pilot Training

5.1 BE90/200 Initial Type Rating Training

5.1.1 Prerequisites

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

[AMC] Additional modular training should be considered for pilots with no or limited experience in multi-engine turboprop aircraft, including various avionics suites and navigation systems (e.g. EFIS, FMS, RVSM), prior to beginning practical training.

5.1.2 Training syllabus

[AMC] Full initial type rating training is contained at Appendix 1.

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5.2 BE90/200 Initial Type Rating Training with Credit for Commonality

[M] Reduced type rating training based on commonality is limited to initial type rating training for BE90/200 Series equipped aircraft with ProLine 21, and to pilots meeting the following prerequisites: • Current and qualified on BE300/1900 series aircraft equipped with ProLine 21 avionics; and • a minimum of 150 hours as PIC and/or Co-Pilot and three months flying experience in a BE300/1900 series aircraft with Proline 21; and • passed knowledge test on base aircraft prior to training on the BE90/200 series

5.2.2 Training syllabus

[AMC] Initial type rating training with credit for commonality is contained at Appendix 1.

5.3 Familiarisation Training between BE90/200 Series variants

[M] Familiarisation training is applicable between the BE-200/B200, BE-C90A/B/GT, BE-C90/90-1, BE-E90, BE-F90/F90-1, BE-90/A90/B90, BE-200PL21/B200GT/250, and BE-C90GTi/C90GTx aircraft.

5.3.1 Training Footprint [AMC]

Familiarisation training between BE90/200 Series variants should include the following subjects and hours of training:

FROM AIRCRAFT

200/B200 B200PL21/B200GT 250 C90A/B/GT C90GTi/GTx

C90GTi/GTx (4) (1) (1) (4) - - -

C90A/B/GT (1) (1) (1) - - - (1)

C90/90-1 (1) (1) (1) (1) (1)

E90 (1) (1) (1) (1) (1)

F90/F90-1 (1) (1) (1) (1) (1) TO AIRCRAFT 90/A90/B90 (1) (1) (1) (1) (1)

200/B200 - - - (1) (1) (1) (1)

B200PL21/B200GT (4) - - - (5) (4) (1)

250 (4) (5) - - - (4) (1)

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Familiarisation training should comprise the following number of hours and address the listed subject areas: (1) 1.0 hrs theoretical training, subjects 1 through 10 (2) 1.5 hrs theoretical training, subjects 1 through 10 (3) 1.5 hrs theoretical training, subjects 1, 2, 4 through 10 (4) 1.0 hrs theoretical training, subjects 1 through 10 (prior completion of ProLine 21 avionics course required) (5) 0.5 hrs theoretical training, subjects 1 through 10

Subject areas are as follows: 1 ...... Electrical 2 ...... Fuel 3 ...... Powerplant 4 ...... Avionics 5 ...... Pneumatics 6 ...... Air Conditioning 7 ...... Ice and Rain Protection 8 ...... Landing Gear and Brakes 9 ...... Flight Controls 10 ...... Aircraft Performance

5.4 Training Areas of Special Emphasis (TASE)

[M] The following training areas of special emphasis must be addressed during ground and flight training for all BE90/200 series models: • Aircraft performance calculations and operational performance requirements for normal, restricted and commuter categories; gross versus net climb gradients for terminal area procedures and for obstacles; • Navigation means with various installed equipment and navigation systems; use of the FCU and FMS, including mode selection, for the types of instrument approaches to be flown. Use of RNAV/GPS FCU navigation modes in lieu of or in conjunction with NDB, VOR, localizer, or back course localizer procedures; • 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.

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[M] Model 200 Restricted Category aircraft require specific training for special purpose configurations.

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 BE90/200 variants for recurrent training are the same as for initial training.

[M] Recurrent training must address the differences between the BE90/200 variants flown.

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 BE90/200 variants for recurrent checking are the same as for initial checking.

[AMC] Recurrent checking should be alternated between BE90/200 variants flown.

[M] If recurrent checking is not alternated between BE90/200 variants flown, the differences must be addressed in checking.

[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;

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• Selection and use of EFIS displays, raw data, flight director, and Reversion / Composite modes, including DPU failure; • Use of Autopilot and flight automation to support single pilot operation; • Knowledge of Normal, Commuter and Restricted Categories related to the BE90/200 variants.

7.1 Line checks

[M] A line check performed on any BE90/200 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 BE90/200 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 90 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.

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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 BE90/200 Series Initial Type Rating Training

[AMC] Pilots completing initial type rating training for the BE90/200 series 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.

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Appendix 1

[AMC] Initial Type Rating Training for BE90/200 Series

TRAINING SYLLABI TIME SCALE Initial Training Full Initial Training with credit for commonality Ground School Hours of training

BE-C90A/B/GT, C90/90-1, E90, 16.0* F90/F90-1, 90/A90/B90 Aeroplane Systems 8.0 BE-200PL21/B200GT/250, B200, 25.0* C90GTi/C90GTx

General Operational Subjects (Includes Load and Balance, Performance, Flight 5.0 2.5 Planning, AFM/POH, Windshear Training and CRM)

BE-C90A/B/GT, C90/90-1, E90, 4.0* F90/F90-1, 90/A90/B90, B200 Systems Integration (completed as part of 0.0 Ground School) BE-200PL21/B200GT/250, 8.0* C90GTi/C90GTx

Practical Training

BE-C90A/B/GT, C90/90-1, E90, 10.0 (SP) 8.0 (SP) F90/F90-1, BE90/A90/B90, (1) B200 12.0 (MP) 8.0 (MP) (in a Flight Simulator) BE-200PL21/B200GT/250, 12.0 (SP) 8.0 (SP) C90GTi/C90GTx 14.0 (MP) (1) 8.0 (MP)

Flight Crew Training (Flight Simulator)

System Integration 2.0 (2)

Single Pilot Operations • Pilot Flying (PF) 10.0 8.0

Multi-Pilot Operations • Pilot Flying (PF) 10.0 8.0 • Pilot Monitoring (PM) 2.0 0.0

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* additional training may be required subject to previous experience on similar aircraft systems and/or avionics.

(1) includes a minimum of 2.0 hours of PM

(2) for BE-200PL21/B200GT/250, C90GTi/C90GTx aircraft only

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:

Beechcraft C90B Initial Training: 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 6 days.

Beechcraft C90GTi 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.

Beechcraft 200 Initial Training: Theoretical training, including knowledge exam should be distributed over a period of 5 training days. Practical training, including skill test should be distributed over a period of 6 days.

Beechcraft 200 with Proline 21 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 2 training days. Practical training, including skill test should be distributed over a period of 5 days.

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Appendix 2

[M] ODR Tables for Model 200 Normal Category to Model 200 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 (Level I or II) FBS ..... Fixed Base Simulator (Level II) FFS ..... Full Flight Simulator (Level A, B, C, D)

ACCEPTABLE DIFFERENCES TABLE

DIFFERENCE AIRCRAFT: HBC Model 200 Commuter Category COMPLIANCE METHOD BASE AIRCRAFT: HBC Model 200 Normal Category

TRAINING CHKG/CURR

FLT PROC LVL LVL LVL LVL DESIGN REMARKS CHK CURR CHAR CHNG A B C D General Airplane Change from Normal to Commuter Category Configuration Remain Single Pilot operation NO YES AI A B MGTOW 13,420 lbs Weights Ramp Weight 13,510lbs. NO YES AI A B Landing Weight 12,500 lbs, no change See AFM Supplement Limitations Limit 9 or less Pax NO YES X A B Placards and New illuminated exit signs Markings New Escape Path Lighting NO YES AI A B Some Inspection Interval Changes Servicing No other changes NO NO X A B Limited to PT6A-41, 42, 52, 61 Engines only Engines NO NO AI A B Takeoff Trim Warning System Flight Deck Overspeed Warning System NO YES FTD B C Stall Warning Ice Mode Instrument Panel New Stall Speed Ice Mode schedule Layout NO YES FTD B C Emergency Lighting System installed with Cabin own battery system NO YES FTD A B

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ACCEPTABLE DIFFERENCES TABLE

DIFFERENCE AIRCRAFT: HBC Model 200 Commuter Category COMPLIANCE METHOD BASE AIRCRAFT: HBC Model 200 Normal Category

TRAINING CHKG/CURR

FLT PROC LVL LVL LVL LVL MANEUVER REMARKS CHK CURR CHAR CHNG A B C D Preflight First Flight Check – Emergency Lighting System NO YES AI A B Engine Start Each Flight Check – Takeoff Trim Warning NO YES FTD B C

Taxi Stall Warning Ice Mode annunciator check Before TO NO YES FTD B C Takeoff Add V1, Vr Procedure, Rotate 6-7 degrees pitch initially YES YES FTD C C RTO V1, Vr, V2 speeds for WAT Limit Or Accel/Stop – Accel/Go required NO YES FFS D D V1 Fail Approach Climb Gradient for Landing required for Takeoff Climb DeIce Boot activation at first indication Cruise Stall Warning Ice Mode speed procedures NO YES AI B C Decent Minimum speed in Icing not 145 kts Instrument Approach Climb Gradient for landing Approaches Balked Climb Gradient for landing YES YES FFS D D Landing Vref speed used for landing Approach configuration for landing NO YES FFS D D Shutdown Emergency Cabin Lighting System switch NO YES AI B B

Normal Changes in AFMS Procedures NO YES FTD C C Abnormal Changes in AFMS Procedures NO YES FFS D D Emergency Emergency Speeds change Procedures Engine Failure Procedures Evacuation Procedures and Lighting NO YES FFS D D Engine Fire Extinguisher Procedure Changes in AFMS In-Flight Flight in Icing Procedures Maneuvers NO YES AI B B

OSD FC BE90/200 – Initial Issue Page 21 of 22 Operational Suitability Data – Flight Crew BE90/200

ACCEPTABLE DIFFERENCES TABLE

DIFFERENCE AIRCRAFT: HBC Model 200 Commuter Category COMPLIANCE METHOD

BASE AIRCRAFT: HBC Model 200 Normal Category

TRAINING CHKG/CURR

FLT PROC LVL LVL LVL LVL SYSTEM REMARKS CHK CURR CHAR CHNG A B C D 24 Battery for Emergency Lighting System Electrical Power NO YES AI A B 25 Escape Path Lighting – electroluminescent Equipment / Furn. Emergency Exit Lighting – NO YES AI B B electroluminescent

26 Engine Fire Extinguisher System required Fire Protection NO YES AI A B 30 Stall Warning Ice Mode speed schedule Ice / Rain system NO YES AI B B 31 Takeoff Warning Trim system added Indicating/Record Stall Warning system new Ice mode NO YES AI B B

32 Approved for Standard and High Flotation Landing Gear landing gear NO NO AI A B All options for Brakes approved at new weight 33 Emergency Lighting system added Lights NO YES AI A B 34 Overspeed Warning system added Navigation NO YES AI A B 52 9 or less Pax for only one Emergency Exit Doors NO NO X A B 61 Both 3 & 4 Blade Propellers approved Propellers NO NO X A B 72 Limited to 850 shp engines only Engine (turbine) NO NO X A B

OSD FC BE90/200 – Initial Issue Page 22 of 22