operational suitability data (osd) flight crew - cessna · models be-200/b200, be-c90a/b ......
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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
Operational Suitability Data – Flight Crew BE90/200
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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).
Operational Suitability Data – Flight Crew BE90/200
OSD FC BE90/200 – Initial Issue Page 7 of 22
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
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OSD FC BE90/200 – Initial Issue Page 8 of 22
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.
Operational Suitability Data – Flight Crew BE90/200
OSD FC BE90/200 – Initial Issue Page 9 of 22
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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OSD FC BE90/200 – Initial Issue Page 10 of 22
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.
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OSD FC BE90/200 – Initial Issue Page 11 of 22
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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OSD FC BE90/200 – Initial Issue Page 12 of 22
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)
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OSD FC BE90/200 – Initial Issue Page 13 of 22
Operational Suitability Data – Flight Crew BE90/200
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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.
Operational Suitability Data – Flight Crew BE90/200
OSD FC BE90/200 – Initial Issue Page 15 of 22
[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;
Operational Suitability Data – Flight Crew BE90/200
OSD FC BE90/200 – Initial Issue Page 16 of 22
• 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.
Operational Suitability Data – Flight Crew BE90/200
OSD FC BE90/200 – Initial Issue Page 17 of 22
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.
Operational Suitability Data – Flight Crew BE90/200
OSD FC BE90/200 – Initial Issue Page 18 of 22
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
Operational Suitability Data – Flight Crew BE90/200
OSD FC BE90/200 – Initial Issue Page 19 of 22
* 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.
Operational Suitability Data – Flight Crew BE90/200
OSD FC BE90/200 – Initial Issue Page 20 of 22
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
Operational Suitability Data – Flight Crew BE90/200
OSD FC BE90/200 – Initial Issue Page 21 of 22
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
Operational Suitability Data – Flight Crew BE90/200
OSD FC BE90/200 – Initial Issue Page 22 of 22
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