FAA · Type Certificate Data Sheet
TCDS A24CE
Beechcraft Corporation
Models covered (41)
- A200
- 200
- 1900D
- 300
- B300
- 300LW
- B200C
- A200C
- 200T
- 1900C
- 200C
- A200CT
- B300C
- B200CT
- 200CT
- B200T
- B200
- 1900
- A200CT (RC-12Q)
- A200 (C-12C)
- B200C (UC-12F)
- A200CT (C-12F)
- A200CT (FWC-12D)
- A200CT (RC-12H)
- A100-1 (U-21J)
- A200CT (RC-12G)
- A200 (C-12A)
- B200C (C-12R)
- B200C (UC-12M)
- B200C (C-12F)
- A200CT (C-12D)
- 1900C (C-12J)
- A200C (UC-12B)
- A200CT (RC-12P)
- A200CT (RC-12D)
- A200CT (RC-12K)
- B300C (UC-12W)
- B200GT
- B200CGT
- B300C (MC-12W)
- B300C (C-12W)
Applicable airworthiness directives (12)
ADs joined from the FAA Federal Register by (Beechcraft Corporation × model). Click any AD to see the full Federal Register record. Mandatory; flying out of compliance grounds the airplane.
- 2025-19354 Airworthiness Directives; Textron Aviation Inc. Airplanes 2025-10-02
- 2022-02398 Airworthiness Directives; Textron Aviation Inc. (Type Certificate Previously Held by Raytheon Aircraft Company, Hawker Beechcraft Corporation, and Beechcraft Corporation) Airplanes 2022-02-04
- 2014-21027 Airworthiness Directives; Rockwell Collins, Inc. Transponders 2014-09-09
- 2011-17567 Airworthiness Directives; Hawker Beechcraft Corporation Models B300 and B300C (C-12W) Airplanes 2011-07-15
- 2011-10387 Airworthiness Directives; Hawker Beechcraft Corporation Models B300 and B300C (C-12W) Airplanes 2011-04-29
- 2010-31438 Airworthiness Directives; Hawker Beechcraft Corporation Models B200, B200GT, B300, and B300C Airplanes 2010-12-16
- 2010-4436 Airworthiness Directives; Hawker Beechcraft Corporation (Type Certificate Previously Held by Raytheon Aircraft Company) Models B300 and B300C Airplanes 2010-03-04
- E9-29975 Airworthiness Directives; Hawker Beechcraft Corporation (Type Certificate Previously Held by Raytheon Aircraft Company) Models B300 and B300C Airplanes 2009-12-17
- E8-6959 Airworthiness Directives; Hawker Beechcraft Corporation Models B200, B200GT, B300, and B300C Airplanes 2008-04-07
- E7-10758 Airworthiness Directives; Hawker Beechcraft Corporation (Type Certificate (TC) No. 3A20 and TC No. A24CE Formerly Held by Raytheon Aircraft Corporation and Beech) Models C90A, B200, B200C, B300, and B300C Airplanes 2007-06-11
- 97-31676 Airworthiness Directives; Raytheon Aircraft Company 58, 60, 90, 100, 200, and 300 Series and Model 2000 Airplanes 1997-12-03
- 97-20442 Airworthiness Directives; Raytheon Aircraft Company 58, 60, 90, 100, 200, and 300 Series and Model 2000 Airplanes 1997-08-04
Special Airworthiness Information Bulletins (1)
Advisory bulletins on these airframes. Not mandatory like ADs — but operators tracking AD compliance often miss the SAIB on the same component.
- CE-15-15 Empennage Horizontal & Vertical Stabilizer Structure
Special Conditions + ELOS findings
Certification-time deviations: SCs add requirements where the design is novel; ELOS allows alternative compliance. Most modern types have both.
- ELOS ST05976WI-A-P-1 INFORMATION: Equivalent Level of Safety (ELOS) Finding for 3S Certification, LLC, Installation of BendixKing Electronic Flight Instrumentation System (EFIS), AeroVueTM, Beechcraft Model 200 Airplane, Powerplant Instrumentation, FAA Project #: ST05976WI-A
- ELOS ST11532IB-A-23.805 Requirements of § 23.805; Icarus Aero Inc.
- ELOS ST11527IB-A-23.805 Requirements of § 23.805; Icarus Aero Inc., Project # ST11527IB-A
- ELOS ACE-94-1 Landing gear
- ELOS ACE-90-5 Altimeter instruments
- ELOS ST00539MC-A-C-1 Finding for Aisle
- ELOS ST1933DRB-A-F-1 INFORMATION: Equivalent Level of Safety (ELOS) Finding for BHE & Associates, Ltd., for the Textron-Beechcraft King Air Models B300 and B300C Powerplant Engine Instrument Display, FAA Project # ST1933DRB-A
- ELOS ACE-15-06 INFORMATION: Equivalent Level of Safety (ELOS) Finding for Rockwell Collins, Incorporated, Textron-Beechcraft King Air Models B300 and B300C Powerplant Engine Instrument Display
Certification basis — 14 CFR
Specific sections
- Sec. 23.1
- Sec. 23.67
- Sec. 21.187
- Sec. 23.143
- Sec. 23.145
- Sec. 23.153
- Sec. 23.201
- Sec. 23.203
- Sec. 23.205
- Sec. 23.207
- Sec. 23.335
- Sec. 23.473
- Sec. 23.621
- Sec. 23.729
- Sec. 23.775
- Sec. 23.781
- Sec. 23.951
- Sec. 23.997
- Sec. 25.831
- Sec. 25.929
- Sec. 121.141
- Sec. 23.1301
- Sec. 23.1305
- Sec. 23.1309
- Sec. 23.1321
- Sec. 23.1325
- Sec. 23.1419
- Sec. 23.1443
- Sec. 23.1457
- Sec. 23.1545
- Sec. 25.1419
- Sec. 23.49
- Sec. 23.301
- Sec. 23.305
- Sec. 23.397
- Sec. 23.561
- Sec. 23.603
- Sec. 23.607
- Sec. 23.677
- Sec. 23.777
- Sec. 23.867
- Sec. 23.1322
- Sec. 23.1323
- Sec. 23.1331
- Sec. 23.1547
- Sec. 23.1549
- Sec. 23.1529
- Sec. 23.771
- Sec. 23.1303
Former holders
- Beech Aircraft Corp.
- Raytheon Aircraft Company\Hawker Beechcraft Corporation
- Beech Aircraft Corp.\Raytheon Aircraft Company\Hawker Beechcraft Corporation
- Hawker Beechcraft Corporation\Beechcraft Corporation
- Beech Aircraft Corp.\Raytheon Aircraft Company
- Hawker Beechcraft Corporation
- Raytheon Aircraft Company
Comments
Revision 79 not published in RGL.
Engineering specs · extracted from TCDS PDF
Surface-extracted from the actual TCDS PDF (regex on the agency's own text). Multi-model TCDS have one set of specs per Model section; we show the union. The linked PDF remains the authoritative source.
Max gross
590lbs
Oil
4.6gal
Engines (per TCDS)
- — Pratt
- — Two
Fleet view · 1,665 registered tails
Engineering specs aggregated from the FAA Aircraft Registry — what every actually-flying tail under this TCDS reports. Median + 10th–90th-percentile range across the active fleet.
Seats
11
11–19 (n=1,665)
Horsepower
850
750–1,050
Cruise (kts)
156
142–156
Year of mfr
1991
1968–2016
Engines on the type, by tail count
- P&W CANADA PT6A-60A 465
- P&W PT6A SER 413
- P&W CANADA PT6A-42 146
- P&W CANADA PT6A-52 85
- P&W CANADA PT6A-6 SERIES 62
- P&W CANADA PT6A-65B 61
- U/A CANADA PT6A SERIES 50
- U/A CANADA PT6A-41 42
NTSB events
246
across all model variants
Applicable ADs
572
FAA airworthiness directives
Per-tail rate
0.15 events / tail · 0.34 ADs / tail
The TCDS PDF on drs.faa.gov is the authoritative document for design-as-certified weight limits, performance, equipment, AD compliance times, and operating limitations. Open on drs.faa.gov ↗ DRS frequently breaks — when it does, the fleet view above and the cross-links below are usually what you actually need.