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Atlas / TCDS / A24CE

FAA · Type Certificate Data Sheet

TCDS A24CE

Beechcraft Corporation

Historical Aircraft Small/Large Airplane Rev 113 12/22/2015 📄 TCDS PDF (direct) ↗ drs.faa.gov ↗

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

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.