Operational Suitability Data (OSD) Flight Crew - Cessna · Models BE-200/B200, BE-C90A/B ... Operational Suitability Data (OSD) – Flight Crew ... EASA approved syllabus for initial

HBC Document Reference BE90-200ALLOSDFC-01

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

OSD FC BE90/200 – Initial Issue Page 2 of 22

Hawker Beechcraft BE90/200 Series

Operational Suitability Data (OSD) – Flight Crew

Revision Record Revision No. Content Date

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



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



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 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).



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".

Manufacturer Aircraft

Model / Name License

Endorsement Variants Complex SP /

SP HPA / MP

OEB FC REPORT /

OSD FC available

Remarks

Hawker Beechcraft Corporation

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 BE-C90GTi/C90GTx

BE90/99/100/200 X X SP HPA X OSD FC BE90/200, dated 19 Nov 2015

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



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.



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.



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

TO A

IRC

RA

FT

Model 200 (normal)

Model 200 (commuter)

Model 200 (restricted)

Model 200 (normal)

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

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

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

Model 200 (commuter)

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

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

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

Model 200 (restricted)

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

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

not evaluated (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.



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.



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

TO A

IRC

RA

FT

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)

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)





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


(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)


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.



[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;



• 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.



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.



Appendix 1

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

TRAINING SYLLABI TIME SCALE

Full Initial Training Initial Training with credit for commonality

Ground School Hours of training

Aeroplane Systems

BE-C90A/B/GT, C90/90-1, E90, F90/F90-1, 90/A90/B90 16.0*

8.0 BE-200PL21/B200GT/250, B200, C90GTi/C90GTx

25.0*

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

5.0 2.5

Systems Integration (completed as part of Ground School)

BE-C90A/B/GT, C90/90-1, E90, F90/F90-1, 90/A90/B90, B200

4.0*

0.0

BE-200PL21/B200GT/250, C90GTi/C90GTx

8.0*

Practical Training

(in a Flight Simulator)

BE-C90A/B/GT, C90/90-1, E90, F90/F90-1, BE90/A90/B90, B200

10.0 (SP) 12.0 (MP) (1)

8.0 (SP) 8.0 (MP)

BE-200PL21/B200GT/250, C90GTi/C90GTx

12.0 (SP) 14.0 (MP) (1)

8.0 (SP) 8.0 (MP)

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

2.0 (2)

10.0

10.0 2.0

8.0

8.0 0.0



* 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


Beechcraft 200 Initial Training: Theoretical training, including knowledge exam should be distributed over a period of 5 training


Beechcraft 200 with Proline 21 Initial Training: Theoretical training, including knowledge exam should be distributed over a period of 6 training


Initial Training with credit for commonality:

Theoretical training, including knowledge exam should be distributed over a period of 2 training




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 BASE AIRCRAFT: HBC Model 200 Normal Category

COMPLIANCE METHOD

TRAINING CHKG/CURR

DESIGN REMARKS FLT CHAR

PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

General Airplane Configuration

Change from Normal to Commuter Category Remain Single Pilot operation NO YES AI A B

Weights

MGTOW 13,420 lbs Ramp Weight 13,510lbs. Landing Weight 12,500 lbs, no change

NO YES AI A B

Limitations

See AFM Supplement Limit 9 or less Pax NO YES X A B

Placards and Markings

New illuminated exit signs New Escape Path Lighting NO YES AI A B

Servicing

Some Inspection Interval Changes No other changes NO NO X A B

Engines

Limited to PT6A-41, 42, 52, 61 Engines only NO NO AI A B

Flight Deck

Takeoff Trim Warning System Overspeed Warning System Stall Warning Ice Mode

NO YES FTD B C

Instrument Panel Layout

New Stall Speed Ice Mode schedule NO YES FTD B C

Cabin

Emergency Lighting System installed with own battery system NO YES FTD A B



ACCEPTABLE DIFFERENCES TABLE

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

COMPLIANCE METHOD

TRAINING CHKG/CURR

MANEUVER REMARKS FLT CHAR

PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

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 Before TO

Stall Warning Ice Mode annunciator check NO YES FTD B C

Takeoff Add V1, Vr Procedure, Rotate 6-7 degrees pitch initially YES YES FTD C C

RTO Or V1 Fail

V1, Vr, V2 speeds for WAT Limit Accel/Stop – Accel/Go required Approach Climb Gradient for Landing required for Takeoff

NO YES FFS D D

Climb Cruise Decent

DeIce Boot activation at first indication Stall Warning Ice Mode speed procedures Minimum speed in Icing not 145 kts

NO YES AI B C

Instrument Approaches

Approach Climb Gradient for landing 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 Procedures

Changes in AFMS NO YES FTD C C

Abnormal Procedures

Changes in AFMS NO YES FFS D D

Emergency Procedures

Emergency Speeds change Engine Failure Procedures Evacuation Procedures and Lighting Engine Fire Extinguisher Procedure Changes in AFMS

NO YES FFS D D

In-Flight Maneuvers

Flight in Icing Procedures NO YES AI B B



ACCEPTABLE DIFFERENCES TABLE

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

COMPLIANCE METHOD

TRAINING CHKG/CURR

SYSTEM REMARKS FLT CHAR

PROC CHNG

LVL A

LVL B

LVL C

LVL D CHK CURR

24 Electrical Power

Battery for Emergency Lighting System NO YES AI A B

25 Equipment / Furn.

Escape Path Lighting – electroluminescent Emergency Exit Lighting – electroluminescent

NO YES AI B B

26 Fire Protection

Engine Fire Extinguisher System required NO YES AI A B

30 Ice / Rain

Stall Warning Ice Mode speed schedule system NO YES AI B B

31 Indicating/Record

Takeoff Warning Trim system added Stall Warning system new Ice mode NO YES AI B B

32 Landing Gear

Approved for Standard and High Flotation landing gear All options for Brakes approved at new weight

NO NO AI A B

33 Lights

Emergency Lighting system added NO YES AI A B

34 Navigation

Overspeed Warning system added NO YES AI A B

52 Doors

9 or less Pax for only one Emergency Exit NO NO X A B

61 Propellers

Both 3 & 4 Blade Propellers approved NO NO X A B

72 Engine (turbine)

Limited to 850 shp engines only NO NO X A B

Documents

Operational Suitability Data (OSD) Flight Crew - Cessna · Models BE-200/B200, BE-C90A/B ... Operational Suitability Data (OSD) – Flight Crew ... EASA approved syllabus for initial