# Beech A100

- Type: Aircraft model (FAA registry)
- Registry code: 1152915
- Manufacturer (registry): BEECH
- Model: A100
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-prop
- Seats: 11
- Weight class: Up to 12,499 lb
- Cruise speed: 146 mph
- Certification: Type certificated
- Data sheet: [TCDS A14CE](https://openairdocs.org/tcds/A14CE) (OpenAirDocs)
- Holder: Textron Aviation Inc.
- Registered aircraft: 15
- Page: https://openairdocs.org/model/beech-a100

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2020-25-01](https://openairdocs.org/ad/2020-25-01): Wings · Textron 100, 65-90, 65-A90 and 17 more. Effective Jan 11, 2021
- [AD 2006-13-10](https://openairdocs.org/ad/2006-13-10): Rudder trim tab · Textron 100, 65-90, 65-A90 and 18 more. Effective Aug 7, 2006
- [AD 2006-12-25](https://openairdocs.org/ad/2006-12-25): Actuator nut assembly · General Machine - Diecron Actuator nut assembly, 100, 200 and 15 more. Effective Jul 28, 2006
- [AD 2005-18-20](https://openairdocs.org/ad/2005-18-20): "FASTprop" propeller de-icers · Hartzell PHC-C3YF-1RF/F8468A(B,K)-8R constant speed propeller (STC SA00718LA or 17 others). Effective Oct 14, 2005
- [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005
- [AD 2005-01-04](https://openairdocs.org/ad/2005-01-04): Fuel hose · Textron 100, 200, 200C and 29 more. Effective Feb 22, 2005
- [AD 2004-23-02](https://openairdocs.org/ad/2004-23-02): Nose Landing Gear (NLG) Fork · Textron 100, 1900, 1900C and 50 more. Effective Dec 23, 2004
- [AD 2004-17-02](https://openairdocs.org/ad/2004-17-02): Cross shaft attach bolt · Textron 100, 1900, 1900C and 52 more. Effective Oct 4, 2004
- [AD 2003-13-16](https://openairdocs.org/ad/2003-13-16): Aft Pressure Bulkhead of Fuselage · Textron 100, 200, 200C and 33 more. Effective Aug 25, 2003
- [AD 2003-02-03](https://openairdocs.org/ad/2003-02-03): Airstair door and emergency exits · Textron 100, 200, 2000 and 46 more. Effective Mar 7, 2003
- [AD 2001-23-17](https://openairdocs.org/ad/2001-23-17): GNS 430 units · Cessna 172, 182, 206 and 209 more. Effective Dec 28, 2001
- [AD 98-25-02](https://openairdocs.org/ad/98-25-02): Top-mounted Antenna · Bell Helicopter Textron Canada 407, 172, 172A and 243 more. Effective Dec 22, 1998
- [AD 97-25-03](https://openairdocs.org/ad/97-25-03): AFM - Limitations - Power Levers · Textron 100, 1900, 1900C and 44 more. Effective Jan 21, 1998
- [AD 97-25-01](https://openairdocs.org/ad/97-25-01): Outflow/Safety Valve · Textron 100, 200, 2000 and 38 more. Effective Jan 11, 1998
- [AD 97-23-17](https://openairdocs.org/ad/97-23-17): Pneumatic Tubing · Textron 200, 200C, 200CT and 30 more. Effective Dec 29, 1997
- [AD 97-06-06](https://openairdocs.org/ad/97-06-06): Pilot and Copilot Chairs Locking Pins · Textron 100, 1900, 1900C and 43 more. Effective May 9, 1997
- [AD 96-03-13](https://openairdocs.org/ad/96-03-13): Main Landing Gear Drag Leg Lock Link · Textron 100, 200, 200C and 24 more. Effective Apr 1, 1996
- [AD 95-13-03](https://openairdocs.org/ad/95-13-03): Electrical Landing Gear Motor · Textron 100, 200, 200C and 22 more. Effective Jul 28, 1995
- [AD 92-15-01](https://openairdocs.org/ad/92-15-01): Truss-To-Firewall Bolts · Textron 100, 200, 200C and 40 more. Effective Aug 21, 1992
- [AD 90-08-17](https://openairdocs.org/ad/90-08-17): Fuselage Moisture Drain System · Textron 100, 200, 200C and 32 more. Effective May 7, 1990
- [AD 89-25-10](https://openairdocs.org/ad/89-25-10): Wing Main Spar Inspection · Textron 100, 65-90, 65-A90 and 10 more. Effective Jan 4, 1990
- [AD 88-04-07](https://openairdocs.org/ad/88-04-07): Wing Spar Nuts Inspection · Textron 100, 65, 65-80 and 18 more. Effective Apr 18, 1988
- [AD 87-03-06 R1](https://openairdocs.org/ad/87-03-06-R1): Elevator Hinge Attachment · Textron 100, 99, 99A and 5 more. Effective Mar 12, 1987
- [AD 85-22-05](https://openairdocs.org/ad/85-22-05): Nuts and Bolts Replacement · Textron 100, 200, 200C and 60 more. Effective Nov 12, 1985
- [AD 85-01-01](https://openairdocs.org/ad/85-01-01): Acrylic Windows · Textron 100, 65-88, 65-90 and 4 more. Effective Feb 6, 1985
- [AD 81-23-01 R1](https://openairdocs.org/ad/81-23-01-R1): Beech Kit or Supplemental Type Certificate · Textron 100, 65, 65-88 and 20 more. Effective Jan 4, 1982
- [AD 80-09-03 R1](https://openairdocs.org/ad/80-09-03-R1): Placard -Oxygen · Textron 100, 200, 200C and 9 more. Effective Jun 11, 1980
- [AD 79-01-01](https://openairdocs.org/ad/79-01-01): Screws in Control System · Textron 100, 200, 35-B33 and 34 more. Effective Jan 8, 1979
- [AD 78-22-05](https://openairdocs.org/ad/78-22-05): Elevator Control Push Rods · Textron 100, 50, 65 and 31 more. Effective Nov 6, 1978
- [AD 78-05-06](https://openairdocs.org/ad/78-05-06): Flexible Fuel Cells · Cessna 180, 182, 185 and 98 more. Effective Jun 30, 1978
- [AD 77-18-04](https://openairdocs.org/ad/77-18-04): Cabin Pressurization · Textron 200, 200T, A100 and 3 more. Effective Sep 12, 1977
- [AD 76-22-02](https://openairdocs.org/ad/76-22-02): 'Y' Type Shoulder Harness · Textron 200, 58, 58A and 14 more. Effective Jun 2, 1977
- [AD 77-02-04](https://openairdocs.org/ad/77-02-04): Wing Tip Strobe Lights · Textron 100, 58, 58A and 13 more. Effective Mar 3, 1977
- [AD 76-22-03](https://openairdocs.org/ad/76-22-03): Elevator Control · Textron 100, 99, 99A and 4 more. Effective Nov 4, 1976
- [AD 76-10-10](https://openairdocs.org/ad/76-10-10): Cabin Door · Textron 100, 200, 65-88 and 6 more. Effective May 28, 1976
- [AD 76-04-02](https://openairdocs.org/ad/76-04-02): Seat Locking Pins · Textron 200, A100, A200 and 2 more. Effective Feb 26, 1976
- [AD 74-24-03](https://openairdocs.org/ad/74-24-03): Strobe Light System · Textron 100, 200, 58 and 16 more. Effective Nov 22, 1974
- [AD 74-18-04](https://openairdocs.org/ad/74-18-04): Fuel Sump Drain Line · Textron A100, A100-1 (U-21J), A100A and 1 more. Effective Aug 30, 1974
- [AD 74-16-03](https://openairdocs.org/ad/74-16-03): Restricted Elevator Travel · Textron 100, 99, 99A and 4 more. Effective Aug 6, 1974

## Information bulletins (advisory) (6)

- [SAIB 2026-16](https://openairdocs.org/saib/2026-16): Elevator Control System. Issued Sep 10, 2026
- [SAIB CE-10-34R2](https://openairdocs.org/saib/CE-10-34R2): Alternative Methods of Compliance (AMOC) to Airworthiness Directive (AD) 89-25-10 and 89-25-08. Issued Aug 30, 2013
- [SAIB CE-10-34R1](https://openairdocs.org/saib/CE-10-34R1) (historical): Alternative Methods of Compliance (AMOC) to Airworthiness Directive (AD) 89-25-10 and 89-25-08. Issued Aug 20, 2013
- [SAIB CE-12-36](https://openairdocs.org/saib/CE-12-36): Flight Controls: Aileron. Issued Jun 19, 2012
- [SAIB CE-11-04](https://openairdocs.org/saib/CE-11-04): Wings  Wing Spar. Issued Dec 2, 2010
- [SAIB CE-10-34](https://openairdocs.org/saib/CE-10-34) (historical): Alternative Methods of Compliance (AMOC) to Airworthiness Directive (AD) 89-25-10 and AD 89-25-08. Issued May 18, 2010

## Registered aircraft (15)

- [N162MC](https://openairdocs.org/aircraft/N162MC): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), S/N B137
- [N208SR](https://openairdocs.org/aircraft/N208SR): [Bardoo Urias L](https://openairdocs.org/faa-owner/BARDOO%20URIAS%20L), [Massapequa, NY](https://openairdocs.org/faa-place/NY/Massapequa), built 1974, S/N B208
- [N219WW](https://openairdocs.org/aircraft/N219WW): [Tj Air Holdings Inc Trustee](https://openairdocs.org/faa-owner/TJ%20AIR%20HOLDINGS%20INC%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 1975, S/N B-219
- [N223LH](https://openairdocs.org/aircraft/N223LH): [Lelah Holdings Limited Partnership](https://openairdocs.org/faa-owner/LELAH%20HOLDINGS%20LIMITED%20PARTNERSHIP), [Reno, NV](https://openairdocs.org/faa-place/NV/Reno), built 1976, S/N B-223
- [N23605](https://openairdocs.org/aircraft/N23605): [Een Aviation LLC](https://openairdocs.org/faa-owner/EEN%20AVIATION%20LLC), [Arlington, TX](https://openairdocs.org/faa-place/TX/Arlington), built 1977, S/N B-236
- [N24SP](https://openairdocs.org/aircraft/N24SP): [Uzochi Inc DBA](https://openairdocs.org/faa-owner/UZOCHI%20INC%20DBA), [Albuquerque, NM](https://openairdocs.org/faa-place/NM/Albuquerque), built 1972, S/N BB-3
- [N479AK](https://openairdocs.org/aircraft/N479AK): [Safeco Leasing LLC](https://openairdocs.org/faa-owner/SAFECO%20LEASING%20LLC), [Port Alsworth, AK](https://openairdocs.org/faa-place/AK/Port%20Alsworth), built 1970, S/N B-96
- [N711RE](https://openairdocs.org/aircraft/N711RE): [Montana Aircraft Trust Inc Trustee](https://openairdocs.org/faa-owner/MONTANA%20AIRCRAFT%20TRUST%20INC%20TRUSTEE), [Bozeman, MT](https://openairdocs.org/faa-place/MT/Bozeman), built 1976, S/N B-233
- [N720C](https://openairdocs.org/aircraft/N720C): [Oscar Charlie LLC](https://openairdocs.org/faa-owner/OSCAR%20CHARLIE%20LLC), [California, MD](https://openairdocs.org/faa-place/MD/California), built 1973, S/N B-171
- [N799DD](https://openairdocs.org/aircraft/N799DD): [Renfro Michael W](https://openairdocs.org/faa-owner/RENFRO%20MICHAEL%20W), [Bethel, AK](https://openairdocs.org/faa-place/AK/Bethel), built 1971, S/N B-102
- [N86NB](https://openairdocs.org/aircraft/N86NB): [Clairmont Holdings Vi LLC](https://openairdocs.org/faa-owner/CLAIRMONT%20HOLDINGS%20VI%20LLC), [St Thomas, VI](https://openairdocs.org/faa-place/VI/St%20Thomas), S/N B166
- [N902VD](https://openairdocs.org/aircraft/N902VD): [Davis Aviation Inc](https://openairdocs.org/faa-owner/DAVIS%20AVIATION%20INC), [Brandon, MS](https://openairdocs.org/faa-place/MS/Brandon), S/N B-201
- [N91RK](https://openairdocs.org/aircraft/N91RK): [Air Flight Inc](https://openairdocs.org/faa-owner/AIR%20FLIGHT%20INC), [Fort Lauderdale, FL](https://openairdocs.org/faa-place/FL/Fort%20Lauderdale), built 1976, S/N B-226
- [N93GT](https://openairdocs.org/aircraft/N93GT): [Dodson International Parts Inc](https://openairdocs.org/faa-owner/DODSON%20INTERNATIONAL%20PARTS%20INC), [Rantoul, KS](https://openairdocs.org/faa-place/KS/Rantoul), built 1974, S/N B-179
- [N93VD](https://openairdocs.org/aircraft/N93VD): [Absl Construction](https://openairdocs.org/faa-owner/ABSL%20CONSTRUCTION), [Hayward, CA](https://openairdocs.org/faa-place/CA/Hayward), built 1972, S/N B-118

## STCs approved for it (219, first 50)

- [STC SA00114AT](https://openairdocs.org/stc/SA00114AT): Installation of a Marathon KSP 400 battery.. Aviall Services, Inc.
- [STC SA00120IB](https://openairdocs.org/stc/SA00120IB): Installation of the Universal Kapture Cockpit Voice Recorder (CVR) with Recorder Independent Power Supply (RIPS). Avmax Aviation Services Inc.
- [STC SA00161BO (3 OF 3](https://openairdocs.org/stc/SA00161BO%20(3%20OF%203): Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.. Avidyne Corporation
- [STC SA00165BO](https://openairdocs.org/stc/SA00165BO): Installation of Avidyne Corporation Datalink Coupler, part number 700-00015-000 per Avidyne Corporation Master Document List, Document No. AVACP-006 dtd 1/2/93 or later FAA-approved revisions.. Avidyne Corporation
- [STC SA00170WI](https://openairdocs.org/stc/SA00170WI): Installation of camera provisions and camera window.. Avcon Industries Inc
- [STC SA00184WI](https://openairdocs.org/stc/SA00184WI): Installation of Camera Provisions and a Camera Lens. Vector Air Inc
- [STC SA00185LA](https://openairdocs.org/stc/SA00185LA): Installation of Alternate Main Landing Gear Tires, Michelin P/N 026-335-0.. Metrea Special Aerospace ISR Inc.
- [STC SA00227NY](https://openairdocs.org/stc/SA00227NY): Installation of Sky Harbour Aircraft Refinishing Ltd. Ice Damage Prevention Plates.. Sky Harbour Aircraft Refinishing
- [STC SA00242LA](https://openairdocs.org/stc/SA00242LA): Installation of Single Interstate Electronics Corp. 9002 Flight Management System. (A100 (U-21F) S/N B-174). Interstate Electronics Corp
- [STC SA00243BO (4 OF 5)](https://openairdocs.org/stc/SA00243BO%20(4%20OF%205)): Installation of Centurion Consulting, Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100), or without roll steering (p/n 0025-5200).. Icarus Avionics, LLC
- [STC SA00269BO](https://openairdocs.org/stc/SA00269BO): Installation of Avidyne Corporation TWX 670 Tactical Weather Detection System P/N 850-00026-000-( ) consisting of Avidyne Processor P/N 700-00033-000-( ), Sensor Systems Inc. Antenna P/N S72-1715-1 with doubler plate P/N S72-171530-1, and Avidyne Mounting Tray P/N 700-00034-000.. Avidyne Corporation
- [STC SA00273WI](https://openairdocs.org/stc/SA00273WI): Installation of Stretcher, Patient Loading, and Support system.. Lifeport Inc
- [STC SA00281BO](https://openairdocs.org/stc/SA00281BO): Installation of Avidyne Corporation MLX770 MultiLink Broadcast Transceiver P/N 700-00163-( ), Sensor Systems Inc. Antenna P/N S67-1575-109, or equivalent, and optional Avidyne Mounting Tray P/N 700-00165-000. Avidyne Corporation
- [STC SA00290BO](https://openairdocs.org/stc/SA00290BO): Installation of Avidyne Corporation Part Number  700-00167-XXX Multi-Function Display and Mounting Tray Assembly Part Number 700-00168-XXX. Avidyne Corporation
- [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne Corporation
- [STC SA00344BO PAGE 1](https://openairdocs.org/stc/SA00344BO%20PAGE%201): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights.. Whelen Aerospace Technologies
- [STC SA00352BO PAGE 1](https://openairdocs.org/stc/SA00352BO%20PAGE%201): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation
- [STC SA00415WI](https://openairdocs.org/stc/SA00415WI): Installation of a baggage door.. Avcon Industries Inc
- [STC SA00453WI](https://openairdocs.org/stc/SA00453WI): Installation of a Lateral Tracking Seat Base.. Aviation Fabricators Inc
- [STC SA00504NY](https://openairdocs.org/stc/SA00504NY): Installation of Rosemount Aerospace, Inc. advisory ice detectors, P/N0871HL1 & 0871HT3.. Rosemount Aerospace Inc
- [STC SA00622WI](https://openairdocs.org/stc/SA00622WI): Shoulder harness anchor installation. Aviation Fabricators Inc
- [STC SA00635WI](https://openairdocs.org/stc/SA00635WI): Jump seat installation.. Aviation Fabricators Inc
- [STC SA00681WI-D](https://openairdocs.org/stc/SA00681WI-D): Modification of Collins VHF-20/VHF-20A/VHF-20B VHF COMM Receiver Transmitter with CTL-20 Control Pro Line I System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System Installation. Rockwell Collins Inc
- [STC SA00686SE](https://openairdocs.org/stc/SA00686SE): Installation of American Aviation, Inc., engine exhaust stacks.. American Aviation Inc
- [STC SA00692SE](https://openairdocs.org/stc/SA00692SE): Replacement of certain BF Goodrich pneumatic deicer boots. SMR Technologies
- [STC SA00741WI](https://openairdocs.org/stc/SA00741WI): Installation of the Concorde RG-380E/K series VRSLA batteries in airplanes listed on the attached FAA approved Model List (AML). Aero-Mach Wilco LLC
- [STC SA00749AT](https://openairdocs.org/stc/SA00749AT): Modification of flush type fuel caps for installation of a locking cylinder and keeper. (1964 and subsequent). Aero Trim, Inc
- [STC SA00776DE](https://openairdocs.org/stc/SA00776DE): Installation of 9 Passenger or Less Limitation configuration. Cert Works LLC
- [STC SA00780SE](https://openairdocs.org/stc/SA00780SE): Installation of the True Lock Safety Retention Axle Lock Nut System. True Lock LLC
- [STC SA00783WI-D](https://openairdocs.org/stc/SA00783WI-D): Modification of Collins VHF-20/VHF-20A/VHF-20B VHF COMM Receiver Transmitter with CTL-20 Control Pro Line I System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System Installation.. Textron Aviation Inc
- [STC SA00840LA](https://openairdocs.org/stc/SA00840LA): Installation of Infant Transport Module (ITM).. Lifeport Inc
- [STC SA00841CH](https://openairdocs.org/stc/SA00841CH): Installation of four place side facing divan.. Daedalus, Inc
- [STC SA00866AT-D](https://openairdocs.org/stc/SA00866AT-D): Installation of replacement fuel cell assemblies. FFC Manufacturing
- [STC SA00872SE](https://openairdocs.org/stc/SA00872SE): Installation of modified ram air engine induction system (Option I or Option II).. American Aviation Inc
- [STC SA01003AT](https://openairdocs.org/stc/SA01003AT): Installation of left hand side nacelle fuel cell assembly.. Floats & Fuel Cells
- [STC SA01004AT](https://openairdocs.org/stc/SA01004AT): Installation of right hand side nacelle fuel cell assembly.. FFC Manufacturing
- [STC SA01046CH](https://openairdocs.org/stc/SA01046CH): Installation of SMR Technologies engine inlet anti-icer models.. SMR Technologies Inc
- [STC SA01085LA](https://openairdocs.org/stc/SA01085LA): Installation of the VNS 1000 Voice Navigation System.. VNS Incorporated
- [STC SA01110CH](https://openairdocs.org/stc/SA01110CH): Installation of wing fuel tank quick valve drains.. Storehouse LLC
- [STC SA01114CH](https://openairdocs.org/stc/SA01114CH): Installation of P2 Incorporated 6600 Audio Advisory system. P2 Incorporated
- [STC SA01126WI](https://openairdocs.org/stc/SA01126WI): Replacement of wing tie down ring assembly on Classic Beechcraft model airplanes with one piece machined part number APMA35-115632. DER Associates Ltd.
- [STC SA01146AT](https://openairdocs.org/stc/SA01146AT): Installation of left hand side and right hand side leading edge fuel cell assemblies. (F90 S/N LJ1 AND UP, 99 ALL S/N'S, B100 S/N B1-89 AND UP, 65-B80 S/N LD-151 AND UP). FFC Manufacturing
- [STC SA01158WI](https://openairdocs.org/stc/SA01158WI): Installation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System.. Aero Enhancements Inc.
- [STC SA01169WI](https://openairdocs.org/stc/SA01169WI): Installation of Aero-Mach Labs, Inc. propeller RPM tachometer or percent (gas generator/N1) RPM tachometer instruments.. Aero-Mach Labs Inc.
- [STC SA01191AT](https://openairdocs.org/stc/SA01191AT): Installation of Left Hand and Right Hand Box Section Inboard Fuel Cell Assemblies. (E90, F90, B100, B200 ALL S/N'S, 65-B80 S/N LC230 AND UP, LD280 AND UP). FFC Manufacturing
- [STC SA01203AT](https://openairdocs.org/stc/SA01203AT): Installation of left-hand side and right-hand side center section fuel cell assemblies.. FFC Manufacturing
- [STC SA01213CH](https://openairdocs.org/stc/SA01213CH): Install air ambulance conversion in accordance with Spectrum Aeromed Inc.  Drawings as listed on AML SA01213CH, or later FAA approved revision.. Spectrum Aeromed LLC dba Spectrum Aeromed
- [STC SA01229SE PAGE 2](https://openairdocs.org/stc/SA01229SE%20PAGE%202): Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Garmin International Inc
- [STC SA01260WI](https://openairdocs.org/stc/SA01260WI): Installation of the Concorde RG-380E/K and RG2380E/L series VRSLA batteries in the Raytheon King Air Model airplanes listed on the attached FAA Approved Model List (AML) No. SA01260WI, dated June 9, 2004, in accordance with Concorde Battery Corporation, Master Drawing List, Drawing No. 5-0177, Rev. N/C, dated May 1, 2003, or later FAA approved revision.. Concorde Battery Corporation
- [STC SA01335AT-D](https://openairdocs.org/stc/SA01335AT-D): Installation of replacement fuel cell assemblies. FFC Manufacturing

All 219: https://openairdocs.org/model/beech-a100/stcs.md

## NTSB investigations (18)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB CEN22LA085](https://openairdocs.org/ntsb/CEN22LA085), Dec 28, 2021: Beech A100 (N93GT), West Helena, AR, substantial damage. Probable cause: The malfunction of the propeller autofeather system after takeoff for undetermined reasons, which resulted in both propellers going into feather and a hard landing.
- [NTSB ERA19LA123](https://openairdocs.org/ntsb/ERA19LA123), Mar 12, 2019: Beech A100 (N945WS), Latrobe, PA, substantial damage. Probable cause: A landing gear collapse due to the separation of the actuator pinion bearing support from the actuator, which resulted in the failure of the actuator shaft.
- [NTSB LAX08MA277](https://openairdocs.org/ntsb/LAX08MA277), Aug 22, 2008: Beech A100 (N601PC), Moab, UT, substantial damage, 10 fatal. Probable cause: The pilot’s failure to maintain terrain clearance during takeoff for undetermined reasons.
- [NTSB LAX08FA026](https://openairdocs.org/ntsb/LAX08FA026), Nov 6, 2007: Beech A100 (N30GC), Chino, CA, destroyed, 2 fatal. Probable cause: The pilot's failure to maintain a positive climb rate during an instrument takeoff. Contributing to the accident was the low visibility.
- [NTSB CHI06LA062](https://openairdocs.org/ntsb/CHI06LA062), Jan 5, 2006: Beech A100 (N700NC), Sault Ste Marie, MI, substantial damage. Probable cause: The inadequate in-flight decision to continue the approach to land, directional control not maintained, and the contaminated runway. Contributing factors were flight to destination alternate not…
- [NTSB ATL03LA081](https://openairdocs.org/ntsb/ATL03LA081), Mar 17, 2003: Beech A100 (N227BC), Carrollton, GA, substantial damage. Probable cause: The pilot misjudged the approach and touchdown airspeeds that resulted in the overrun of the runway during a landing. Factors were the wet runway and hydroplaning conditions.
- [NTSB DCA03MA008](https://openairdocs.org/ntsb/DCA03MA008), Oct 25, 2002: Beech King Air 100 (N41BE), Eveleth, MN, destroyed, 8 fatal. Probable cause: The flight crew's failure to maintain adequate airspeed, which led to an aerodynamic stall from which they did not recover.
- [NTSB FTW02LA172](https://openairdocs.org/ntsb/FTW02LA172), Jun 5, 2002: Beech BE-100-A100 (N799DD), Little Rock, AR, substantial damage. Probable cause: The malfunction of the left main landing gear retraction/extension assembly due to a missing lock pin/washer/nut on the clevis of the push/pull gear extension tube that resulted from improper…
- [NTSB FTW98FA074](https://openairdocs.org/ntsb/FTW98FA074), Dec 21, 1997: Beech A100 (N100BE), Colo Springs, CO, destroyed, 2 fatal. Probable cause: Failure of the pilot to follow IFR Procedures and maintain the minimum descent altitude (MDA). A related factor was fog.
- [NTSB NYC94FA148](https://openairdocs.org/ntsb/NYC94FA148), Aug 4, 1994: Beech A100 (N7GA), Williamstown, MA, destroyed, 1 fatal. Probable cause: the pilot's failure to maintain minimum control speed after an undetermined loss of engine power, which resulted in an inadvertent stall at too low of an altitude to allow recovery.
- [NTSB DCA90MA017](https://openairdocs.org/ntsb/DCA90MA017), Jan 19, 1990: Beech A100 (N44UE), Atlanta, GA, destroyed, 1 fatal. Probable cause: (1) FAILURE OF THE FEDERAL AVIATION ADMINISTRATION TO PROVIDE AIR TRAFFIC CONTROL PROCEDURES THAT ADEQUATELY TAKE INTO CONSIDERATION HUMAN PERFORMANCE FACTORS SUCH AS THOSE WHICH RESULTED IN THE…
- [NTSB NYC89LA103](https://openairdocs.org/ntsb/NYC89LA103), Mar 22, 1989: Beech A100 (N23605), Johnstown, PA, substantial damage. Probable cause: FAILURE OF THE DOWN LOCK PLATE, WHICH ALLOWED THE LANDING GEAR TO COLLAPSE.
- [NTSB MIA87LA027](https://openairdocs.org/ntsb/MIA87LA027), Nov 8, 1986: Beech A100 (N78L), Brooksville, FL, destroyed
- [NTSB ATL86LA019](https://openairdocs.org/ntsb/ATL86LA019), Nov 6, 1985: Piper Aerostar 601P (N601PC), Sylacauga, AL, substantial damage
- [NTSB FTW85MA317](https://openairdocs.org/ntsb/FTW85MA317), Aug 12, 1985: Beech 200 (N100HC), Quinlan, TX, destroyed, 3 fatal
- [NTSB MIA78FKJ53](https://openairdocs.org/ntsb/MIA78FKJ53), Jun 22, 1978: Beech 100 (N941K), Muscle Shoals, AL, substantial damage
- [NTSB CHI78FEI03](https://openairdocs.org/ntsb/CHI78FEI03), Nov 25, 1977: Cessna 210 (N22220), Vienna, OH, substantial damage
- [NTSB MIA75AM016](https://openairdocs.org/ntsb/MIA75AM016-201275), Apr 26, 1975: Beech A100 (N700SP), Hilton Head Is, SC, destroyed, 6 fatal

## FAA accident and incident reports (42)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Accident 20211228021589A](https://openairdocs.org/incident/20211228021589A), Dec 28, 2021: Beech A100 (N93GT), West Helena, AR, Substantial damage. On December 28, 2021 N93GT departed batesville ms (pmu) at approximately 10:28 CST and arrived uneventfully at Helena ar (hee) at approximately 10:40 CST. Upon…
- [Accident 20190312001209A](https://openairdocs.org/incident/20190312001209A), Mar 12, 2019: Beech A100 (N945WS), Latrobe, PA, Substantial damage. Statement from [privacy data omitted] on king air N945WS on March 12th 2019. On the morning of March 12, I checked weather & filed a IFR flight plan from…
- [Accident 20080822844519A](https://openairdocs.org/incident/20080822844519A), Aug 22, 2008: Beech A100 (N601PC), Moab, UT, Destroyed, 10 fatal. (-23) On August 22, 2008, approximately 1750 MDT, N601PC, a Beech king air A100 impacted hilly terrain shortly after takeoff from the Canyonlands Field Airport…
- [Accident 20071106827069A](https://openairdocs.org/incident/20071106827069A), Nov 6, 2007: Beech A100 (N30GC), Chino, CA, Destroyed, 2 fatal. (-23) N30GC departed the Chino airport on an IFR clearance from runway 26R. The aircraft impacted trees approximately 1/2 mile west of the Chino airport.…
- [Accident 20060105002769A](https://openairdocs.org/incident/20060105002769A), Jan 5, 2006: Beech A100 (N700NC), Sault Ste Marie, MI, Substantial damage. (-23) The flight was an air ambulance flight consisting of the pilot, a flight nurse and a paramedic. After an uneventful flight from traverse city, Michigan…
- [Incident 20050812017129I](https://openairdocs.org/incident/20050812017129I), Aug 12, 2005: Beech A100 (N601PC), Quincy, CA, Minor damage. (-23) The aircraft struck a deer during takeoff rotation.
- [Accident 20030317008009A](https://openairdocs.org/incident/20030317008009A), Mar 17, 2003: Beech A100 (N227BC), Carrollton, GA, Substantial damage. (-23) Ms bomberger landed at ctj after a second no flap approach and ran off the end of the runway causing the nose gear to break off and both props hit the…
- [Accident 20021025033389A](https://openairdocs.org/incident/20021025033389A), Oct 25, 2002: Beech A100 (N41BE), Eleleth, MN, Destroyed, 8 fatal. (-23) At approximately 1024 central daylight time (CST), a Beech king air A-100, N41BE, registered to Beech transportation inc., and operated by aviation…
- [Accident 20020604015769A](https://openairdocs.org/incident/20020604015769A), Jun 4, 2002: Beech A100 (N799DD), Little Rock, AR, No damage. (-23) On June 4, 2002, at 2229 CDT, a Beech BE-100-A100 airplane, N799DD, s/n B-102, registered to and operated by Mr. Christian e. finkbeiner, of Little Rock,…
- [Incident 20001015016549I](https://openairdocs.org/incident/20001015016549I), Oct 15, 2000: Beech A100 (N46JK), Talladega, AL, Minor damage. (-23) While taxiing on a narrow taxiway, the a/c left wing tip hit a fuel truck parked close to the taxiway. The left wing tip lens. Broke.
- [Accident 19971221039259A](https://openairdocs.org/incident/19971221039259A), Dec 21, 1997: Beech A100 (N100BE), Colorado Spring, CO, Destroyed, 2 fatal. Acft was on ILS app when it enterd a fog bank and crashed und unk circ 2 POB suffered fatal inj, Colorado Springs,c
- [Incident 19970219006849I](https://openairdocs.org/incident/19970219006849I), Feb 19, 1997: Beech A100 (N22BJ), Lancaster, TX, Minor damage. Narrative: on February 19, 1997, a Beechcraft B-A100 registered and piloted by anthony mateer landed at lincoln, NE municipal airport. While taxiing to…
- [Incident 19951229046099I](https://openairdocs.org/incident/19951229046099I), Dec 29, 1995: Beech 100BEECH (N777GS), Pittsburgh, PA, Minor damage. Narrative: the pilot stated; while taxiing into corporate jets' ramp, the right brake began to lose pressure. I pumped the brake and again the brake lost…
- [Incident 19950623019569I](https://openairdocs.org/incident/19950623019569I), Jun 23, 1995: Beech A100 (N711RE), Detroit, MI, Minor damage. Lost cabin pressure due captains side window failure. Diverted to dtw.
- [Accident 19940804020179A](https://openairdocs.org/incident/19940804020179A), Aug 4, 1994: Beech A100 (N7GA), North Adams, MA, Destroyed, 1 fatal. Lost thrust left engine on takeoff. Prop had feathered. Got below IMC. Due p factor. Possible prop system rigging.
- [Incident 19940325025779I](https://openairdocs.org/incident/19940325025779I), Mar 25, 1994: Beech A100 (N3100K), Atlanta, GA, Minor damage. Unsafe gear light for landing. Affirmed gear down. Right main collapsed on landing. Manual extension unknown.
- [Incident 19930519018589I](https://openairdocs.org/incident/19930519018589I), May 19, 1993: Piper PA28140 (N777GS), Pittsburgh, PA, Minor damage. Struck a lighted plastic bucket filled with sand on taxiway. Taxiing for takeoff.
- [Incident 19921111054959I](https://openairdocs.org/incident/19921111054959I), Nov 11, 1992: Beech A100 (N710AS), Pago Pago, American Samoa, Minor damage. Gear light failed to go out after takeoff. Burnt off fuel. Returned. Nose gear collapsed on landing.
- [Incident 19911129061479I](https://openairdocs.org/incident/19911129061479I), Nov 29, 1991: Beech A100 (N700AT), South Bend, IN. NR2 engine flamed out en route. Precautionary landing. Hight pressure fuel pump failed.
- [Incident 19900606027949I](https://openairdocs.org/incident/19900606027949I), Jun 6, 1990: Beech A100 (N711RE), Hayward, CA. Dual flame out on approach. Restarted engines. Loss of power to radios. Landed with light signals.
- [Incident 19900223014419I](https://openairdocs.org/incident/19900223014419I), Feb 23, 1990: Beech A100 (N23404), Jamestown, NY. Had malfunctioning anti ice gauge on climb and inadvertently climbed through assigned altitude.
- [Accident 19900118000712A](https://openairdocs.org/incident/19900118000712A), Jan 18, 1990: Beech A100 (N44UE), Atlanta, GA, Destroyed, 1 fatal. On landing roll was struck by N8867E also landing on same runway. ATC failed to separate. Anti collision light inop
- [Accident 19890322065769A](https://openairdocs.org/incident/19890322065769A), Mar 22, 1989: Beech A100 (N23605), Johnstown, PA, Substantial damage. Down lock plate broke on landing. Allowed left main gear to collapse. Aircraft veered off runway,damaged left wing.
- [Incident 19881210068679I](https://openairdocs.org/incident/19881210068679I), Dec 10, 1988: Beech A100 (N22220), Burlington, IA. Smoke in cabin. Landed nearest airport without incident. Overheated heater blower fan assembly caused smoke.
- [Incident 19880830048149I](https://openairdocs.org/incident/19880830048149I), Aug 30, 1988: Dhav DHC4A (N700NC), Los Angeles, CA, Minor damage. Wing tip hit building while taxiing between parked aircraft and building in dark. Taxi line too close to new bldg.
- [Incident 19870623041839I](https://openairdocs.org/incident/19870623041839I), Jun 23, 1987: Beech A100 (N23404), Spring, TX, Minor damage. Unsafe gear indication, diverted, emergency extension used. Left main collapsed on rollout. Gear actuator broken.
- [Accident 19861108054109A](https://openairdocs.org/incident/19861108054109A), Nov 8, 1986: Beech A100 (N78L), Brooksville, FL, Destroyed. Smoke in cockpit on takeoff. Returned to land. Ran off runway into fence and tree due to fog and smoke. Burned.
- [Incident 19861107066689I](https://openairdocs.org/incident/19861107066689I), Nov 7, 1986: Beech A100 (N727LE), Houston, TX. Main gear collapsed as throttles were advanced on takeoff roll. Gear handle was down. Cause to be reported.
- [Incident 19860817055859I](https://openairdocs.org/incident/19860817055859I), Aug 17, 1986: Amd FALCONF (N28C), Mc Allen, TX. Failed to follow clearance as instructed. No conflict of traffic.
- [Incident 19860815076349I](https://openairdocs.org/incident/19860815076349I), Aug 15, 1986: Beech A100 (N22BJ), Chamblee, GA. Aircraft operated by pilot suspected of being intoxicated. Unable to verify pilot in command due to lost flight plan
- [Incident 19860717061399I](https://openairdocs.org/incident/19860717061399I), Jul 17, 1986: Beech A100 (N883CA), Indianapolis, IN. Engine shut down after loss of oil pressure. Found cracked chip detector plug.
- [Accident 19851106056119A](https://openairdocs.org/incident/19851106056119A), Nov 6, 1985: Piper PA60601P (N601PC), Sylacauga, AL, Substantial damage. After several aborted takeoff runs directional control was lost. Aircraft struck trees. No engine malfunction found
- [Accident 19850812052341A](https://openairdocs.org/incident/19850812052341A), Aug 12, 1985: Beech 200BEECH (N100HC), Quinlan, TX, Substantial damage. During a simulated emergency descent, the aircraft struck the wing and empennage of N33177.
- [Incident 19840810051079I](https://openairdocs.org/incident/19840810051079I), Aug 10, 1984: Beech B100 (N110JJ), San Antonio, TX, Minor damage. Electrical overheat. Smoke filled cabin. Returned. Gear pumped down. Gear motor shorted. Possible 135 operation.
- [Incident 19831224072839I](https://openairdocs.org/incident/19831224072839I), Dec 24, 1983: Beech A100 (N23BW), Terre Haute, IN, Minor damage. Severe gusty surface wind blew aircraft off the taxiway into a taxiway light during taxi for takeoff.
- [Incident 19820928056129I](https://openairdocs.org/incident/19820928056129I), Sep 28, 1982: Beech A100 (N764K), Mayo, SC, Minor damage. Cabin door blew off during climb. Improper door seal of 9 psig prevented top latch engagment. Cracks in door frame.
- [Incident 19820212005229I](https://openairdocs.org/incident/19820212005229I), Feb 12, 1982: Beech A100 (N22220), Lexington, KY, Substantial damage. Misjudged edge of snow-covered ramp. Landing gear dropped into unmarked snow-covered hole.
- [Incident 19800910070089I](https://openairdocs.org/incident/19800910070089I), Sep 10, 1980: Beech A100 (N3100K), Hutchinson, KS, Minor damage. Upper cowling section came open in flight, aircraft had just been refueled. Latches worn but satisfactory.
- [Incident 19790113001909I](https://openairdocs.org/incident/19790113001909I), Jan 13, 1979: Beech A100 (N764K), Port Huron, MI, Minor damage. Nose gear brace part #50-820204-27 failed allowing nose gear to retract during takeoff.
- [Accident 19780622030069A](https://openairdocs.org/incident/19780622030069A), Jun 22, 1978: Beech A100 (N941K), Muscle Shoals, AL, Substantial damage. Reduced props instead of throttles on final.
- [Accident 19771125038029A](https://openairdocs.org/incident/19771125038029A), Nov 25, 1977: Cessna T210L (N22220), Vienna, OH, Substantial damage. Cracked rt MLG actuator p/n 1281000-2,s/n 331.
- [Accident 19750426042229A](https://openairdocs.org/incident/19750426042229A), Apr 26, 1975: Beech A100 (N700SP), Hilton Head Is, SC, Destroyed, 4 fatal. Failed to maintain positive rate of clmb aftr tkof twd unlighted area. Aprx 436LBS ovr max tkof gwt

## Service difficulty reports (472, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR HXXC2022031422](https://openairdocs.org/sdr/HXXC2022031422), Mar 12, 2022: HYDRAULIC LINE. CORRODED. PILOT RH BRAKE FAILED WHILE TAXIING. FOUND 1/4" ALUMINUM LINE BELOW FLOOR CORRODED PIN HOLE.
- [SDR 2022FA0000771](https://openairdocs.org/sdr/2022FA0000771), Jan 29, 2020: ENGINE. MALFUNCTIONED. ON 29TH JANUARY 2020, WHILE IN THE CRUISE AT 16000FT, THE PILOT REPORTED HEARING A INCREASING WHISTLING SOUND FROM THE PORT ENGINE WHICH STARTED STARTED TO LOSE
- [SDR CA190822017](https://openairdocs.org/sdr/CA190822017), Jul 25, 2019: RELAY. BURNED. (CAN) AT APPROXIMATELY 9500 FEET IN THE CLIMB, SMOKE WAS NOTICED COMING FROM THE CABIN FLOOR IN THE VICINITY OF THE FLAP MOTOR. THE CREW CARRIED OUT THE APPROPR
- [SDR CA190715014](https://openairdocs.org/sdr/CA190715014), Jul 12, 2019: MASTER LINK. LOOSE. (CAN) DURING ROUTINE INSPECTION ON THE NOSE GEAR RETRACT CHAIN A LINK NEEDED TO BE REMOVED. THE MAINTENANCE TECHNICIAN PROCURED A MASTER LINK FROM INVENTORY, DU
- [SDR CA190313006](https://openairdocs.org/sdr/CA190313006), Mar 11, 2019: SHAFT. WORN. (CAN) THE ELEVATOR TORQUE SHAFT ASSEMBLY WAS FOUND TO HAVE PLAY IN ONE OF THE ARMS. THE ASSEMBLY WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. UPON FURTHER INS
- [SDR CA160205009](https://openairdocs.org/sdr/CA160205009), Feb 3, 2016: RELAY. FAILED. (CAN) DURING TAKEOFF, THE NR 1 INVERTER FAILED. NR 2 INVERTER WAS SELECTED BY CREW BUT IT WAS ALSO FAILED. WITH THIS DOUBLE FAILURE CREW LOST MOST OF ENGINES IN
- [SDR CA160129007](https://openairdocs.org/sdr/CA160129007), Jan 29, 2016: NUT. LOOSE. (CAN) DURING A SCHEDULED FUEL PUMP INSPECTION, THE STARTER GENERATOR AS BEEN REMOVED TO GIVE MORE ACCESS TO THE ENGINE FUEL PUMP. THE MECHANIC DISCOVER THAT SOM
- [SDR CA160128002](https://openairdocs.org/sdr/CA160128002), Jan 26, 2016: TERMINAL. UNSECURE. (CAN) WHILE COMPLETING AD CF-1981-25R6, IT WAS WAS NOTED AFTER REMOVING WING PANEL INBOARD OF RT NACELLE, THAT 2 WIRES (P83D0 P83B0) WERE DISCONNECTED FROM THE 
- [SDR CA160203013](https://openairdocs.org/sdr/CA160203013), Jan 17, 2016: OIL SYSTEM. LEAKING. (CAN) THE AIRCRAFT WAS FORCED TO RETURN TO THE DEPARTURE AIRPORT FOLLOWING THE PRESENCE OF SMOKE IN THE COCKPIT. THE AIRCRAFT LANDED SAFELY. THE SMOKE IN COCKPI
- [SDR CA160115001](https://openairdocs.org/sdr/CA160115001), Jan 11, 2016: CONTROL PANEL. BURNED. (CAN) AFTER HAVING COMPLETED HIS COCKPIT PRE-FLIGHT CHECKS AND WITH ALL ELECTRICAL POWER TURNED OFF, THE PILOT WENT OUTSIDE AND WAS PERFORMING HIS EXTERNAL ACFT
- [SDR CA160107006](https://openairdocs.org/sdr/CA160107006), Dec 28, 2015: SUPPORT. CRACKED. (CAN) DURING VISUAL INSPECTION IN THE ELEVATOR TORQUE TUBE AREA, THE RT ELEVATOR TORQUE TUBE SUPPORT WAS FOUND CRACKED. THE TORQUE TUBE AND SUPPORT ASSY WAS REP
- [SDR CA151016003](https://openairdocs.org/sdr/CA151016003), Oct 13, 2015: VOLT REGULATOR. FAILED. (CAN) ON ACFT SHORT COMING IN TESTING PROCEDURES WAS DISCOVERED WHILE FOLLOWING THE MM FOR THE ADJUSTMENT OF THE VOLTAGE REGULATORS FOR THE GENERATORS. WHEN THE
- [SDR CA151009007](https://openairdocs.org/sdr/CA151009007), Oct 8, 2015: BOLT. CRACKED. (CAN) DEFECT INDICATIONS WERE NOTED DURING LIQUID PENETRANT INSPECTION OF BOTH FORWARD UPPER AND LOWER WING ATTACHMENT BOLTS ON THE LT AND RT SIDES WHILE COMPLE
- [SDR CA151006005](https://openairdocs.org/sdr/CA151006005), Oct 5, 2015: BLADE. FAILED. (CAN) ENGINE WAS SENT FOR INVESTIGATION AND REPAIR AFTER AN IN-FLIGHT SHUTDOWN INCIDENT. THE INCIDENT STARTED WITH A LOUD NOISE FROM THE ENGINE WITH A SUBSEQUEN
- [SDR CA150924009](https://openairdocs.org/sdr/CA150924009), Sep 21, 2015: ALTIMETER. MALFUNCTIONED. (CAN) IMMEDIATELY UPON BECOMING AIRBORNE, FLIGHT CREW NOTICED THE CAPTAIN`S ALTIMETER HAD FLAGGED AND CONTINUED TO INDICATE FIELD ELEVATION THROUGHOUT THE CLIMB
- [SDR CA150903008](https://openairdocs.org/sdr/CA150903008), Sep 3, 2015: CONTROL CABLE. CORRODED. (CAN) DURING AND INSPECTION IN THE LT WING ROOT AREA, IT WAS NOTED THAT THE AILERON TRIM AND AILERON PRIMARY CABLES WERE HEAVILY CORRODED. ONLY LITTLE HAND PRES
- [SDR CA150708004](https://openairdocs.org/sdr/CA150708004), Jul 4, 2015: BONDING STRAP. CRUSHED. (CAN) DURING A TRAINING FLIGHT SMOKE WAS OBSERVED IN THE CABIN. AIRCRAFT LANDED, MAINTENANCE FOUND THE FLAPS CIRCUIT BREAKER HAD POPPED AND THE FLAP MOTOR WAS U
- [SDR CA150618005](https://openairdocs.org/sdr/CA150618005), Jun 11, 2015: TORQUE KNEE. BROKEN. (CAN) AFTER TOUCHDOWN THE PILOTS FELT A VIBRATION, ACFT STOPPED THEN TAXIED TO THE RAMP & IT WAS FOUND THAT THE LT MLG, UPPER & LOWER TORQUE LINK WERE FOUND BRO
- [SDR CA150511007](https://openairdocs.org/sdr/CA150511007), May 10, 2015: TORQUE LINK. BROKEN. (CAN) UPON LANDING, PILOT FELT LIKE HE HAD A FLAT. NO FLAT NOTED BUT UPON INSPECTION, IT WAS NOTED THAT THE RT MLG UPPER TORQUE LINK WAS FOUND TO BE BROKEN IN H
- [SDR CA150428006](https://openairdocs.org/sdr/CA150428006), Apr 24, 2015: PRESSURE SWITCH. INTERMITTENT. (CAN) HYDRAULIC PRESSURE SWITCH INTERMITENT, FOUND DIRTY, LOCATED IN LT WHEEL WELL AREA, CLEANED AND TESTED, RE-INSTALLED AND PERFORMED 18 GEAR CYLCES THROUGHOU
- [SDR CA150417014](https://openairdocs.org/sdr/CA150417014), Apr 14, 2015: B-NUT. SPLIT. (CAN) DURING ROUTINE MAINTENANCE, SOME OIL LOSS, CLEANED AND TUBE B-NUT FOUND SPLIT.
- [SDR CA150407007](https://openairdocs.org/sdr/CA150407007), Mar 31, 2015: RADIO. MALFUNCTIONED. (CAN) CREW HAD A FAILURE OF RADIO`S AND WERE UNABLE TO CONTACT ATC CREW CYCLED AVIONICS MASTER SYS ALL TESTED SERVICEABLE. FLIGHT CONTINUED WITH NO FURTHER PROB
- [SDR CA150324012](https://openairdocs.org/sdr/CA150324012), Mar 24, 2015: TUBE. DISLODGED. (CAN) THE PILOT OF THE ACFT ABORTED TAKEOFF WHEN HE RECEIVED AN OVERTORQUE INDICATION FROM THE RT ENGINE. WHILE TAXIING BACK TO THE TERMINAL, THE PILOT TRIED TO
- [SDR CA150217004](https://openairdocs.org/sdr/CA150217004), Feb 15, 2015: SKIN. CRACKED. (CAN) DURING DAILY INSPECTION, IT WAS NOTICED THAT RT OTBD FLAP HAD DAMAGE TO THE SKIN NEAR THE INBD FLAP TRACK WELL. UPON FURTHER INVESTIGATION, IT WAS ALSO NO
- [SDR CA141219003](https://openairdocs.org/sdr/CA141219003), Dec 17, 2014: GEARBOX. MAKING METAL. (CAN) SHORTLY AFTER TAKEOFF, THE LEFT PROPELLER AUTO FEATHERED. THE ENGINE WAS NOT SHUTDOWN AS THE PROP WAS ALREADY FEATHERED. THE CREW LANDED SAFELY. INVESTIGA
- [SDR CA141208007](https://openairdocs.org/sdr/CA141208007), Nov 20, 2014: SHAFT. CRACKED. (CAN) DETAILED INSPECTION OF BOLTED CONNECTION AT RT INBOUND FLAP ACTUATOR - REVEALED A CRACK- RUNNING FROM THE RIVET HOVE DOWN THE LENGTH OF THE SHAFT APPROX. 
- [SDR CA141014010](https://openairdocs.org/sdr/CA141014010), Oct 11, 2014: HINGE BRACKET. CRACKED. (CAN) THE RIGHT HAND HORIZONTAL STABILIZER HINGE BRACKET WAS FOUND CRACKED DURING VISUAL INSPECTION. THE INSPECTION WAS BEING COMPLETED DUE TO OTHER COMPANY AIR
- [SDR CA141006017](https://openairdocs.org/sdr/CA141006017), Oct 6, 2014: BRACKET. CRACKED. (CAN) DURING INSPECTION, THE LT HORIZONTAL STABILIZER BRACKET WAS FOUND CRACKED.
- [SDR CA141003005](https://openairdocs.org/sdr/CA141003005), Oct 2, 2014: TORQUE KNEE. CRACKED. (CAN) DURING REGULAR ACFT INSPECTION, A CRACK WAS FOUND ON THE LT MLG TORQUE KNEE UPPER LINK.
- [SDR CA140929006](https://openairdocs.org/sdr/CA140929006), Sep 26, 2014: WIRE. MISROUTED. (CAN) ON GEAR DOWN SELECTION ON APPROACH, THE CREW EXPERIENCED A DOUBLE GENERATOR FAILURE WHICH LEFT THE GEAR ONLY PARTIALLY EXTENDED. THE GENERATORS WOULD NOT 
- [SDR CA140918002](https://openairdocs.org/sdr/CA140918002), Sep 17, 2014: TURBINE. FAILED. (CAN) REPORT EIR PT6A 2014-078, ENGINE WAS SENT FOR REPAIR AFTER THE OPERATOR REPORTED THAT THE ENGINE FAILED IN FLIGHT. THE OPERATOR REPORTED THAT THE PT BLADE
- [SDR CA140922012](https://openairdocs.org/sdr/CA140922012), Sep 16, 2014: TORQUE KNEE. BROKEN. (CAN) AFTER TOUCHDOWN THE PILOTS FELT A VIBRATION AND THE AIRCRAFT WANTING TO TURN TO THE RIGHT. AIRCRAFT STOPPED THEN TAXIED TO THE RAMP AND IT WAS FOUND THAT 
- [SDR CA140904001](https://openairdocs.org/sdr/CA140904001), Aug 25, 2014: TORQUE TUBE. CRACKED. (CAN) DURING SCHEDULED VISUAL INSPECTION OF THE ELEVATOR TORQUE TUBE A CRACK WAS FOUND COMMING FROM UNDER THE BUSHING ON THE FLANGE THAT ATTACHES TO THE ELEVATO
- [SDR CA140809001](https://openairdocs.org/sdr/CA140809001), Aug 7, 2014: BLADE. SHEARED. (CAN) LEFT ENGINE FAILED IN FLIGHT. POWER TURBINE BLADES FOUND SHEARED, POWER TURBINE GUIDE VANES DAMAGED, ENGINE BEING REMOVED AND SENT TO OVERHAUL SHOP FOR IN
- [SDR CA140716005](https://openairdocs.org/sdr/CA140716005), Jun 30, 2014: RESISTOR. BURNED. (CAN) EARLY IN THE INVESTIGATION OF THIS INCIDENT, IT WAS DECIDED THAT THIS DID NOT MEET THE REQUIREMENTS NECESSARY TO SUBMIT AN SDR, HOWEVER WE HAVE CHOSEN TO 
- [SDR CA140620012](https://openairdocs.org/sdr/CA140620012), Jun 19, 2014: TORQUE TUBE. CORRODED. (CAN) TORQUE TUBE FOUND CORRODED AND PUNCTURED.
- [SDR CA140530002](https://openairdocs.org/sdr/CA140530002), May 28, 2014: EXCITER. FAILED. (CAN) UNIT FAIL TO PRODUCE SHOWER SPARK TO IGNITER, NO ELECTRICAL POWER OUTPUT. UNIT WAS O/H AT NORMAL TBO 3500 HRS.
- [SDR CA140530003](https://openairdocs.org/sdr/CA140530003), May 27, 2014: EXCITER. FAILED. (CAN) UNIT FAIL, NO ELECTRICAL OUTPUT.
- [SDR CA140527003](https://openairdocs.org/sdr/CA140527003), May 23, 2014: WASHER. DAMAGED. (CAN) DURING ROUTINE INSPECTION, THE KEY WASHER TO INSTALL THE NOSE WHEEL WAS FOUND ELONGATED AND SPUN, WITH COMPARISON TO NEW WASHER. WASHER WAS REPLACED THREA
- [SDR CA140521002](https://openairdocs.org/sdr/CA140521002), May 20, 2014: CONNECTOR. BROKEN. (CAN) INTERIOR NEON BALLAST, BURNED DUE TO CONNECTOR ALIGNMENT NOTCH MISSING/BROKEN INSIDE OF CONNECTOR. THIS ALLOW CONNECTOR TO MOVE AND CREATE A SHORT.
- [SDR CA140505013](https://openairdocs.org/sdr/CA140505013), Apr 25, 2014: TORQUE TUBE. CRACKED. (CAN) DURING SCHEDULED VISUAL INSPECTION OF THE ELEVATOR TORQUE TUBE A CRACK WAS FOUND. THIS MAY HAVE BEEN THE RESULT OF OVER-TORQUEING THE SCREW ATTACHING THE 
- [SDR CA140602022](https://openairdocs.org/sdr/CA140602022), Apr 5, 2014: CAP. UNSECURE. (CAN) THE PILOT REPORTS THAT AT THE SECOND TAKEOFF OF TRAINING JUST AFTER SETTING MAX TAKE-OFF POWER AT ABOUT 40-45 KTS, THEY HEARD A SOUND FROM THE ENGINE THAT
- [SDR CA140327006](https://openairdocs.org/sdr/CA140327006), Mar 25, 2014: DOWNLOCK. BROKEN. (CAN) ON TAKEOFF THE LANDING GEAR FAILED TO FULLY RETACT, WHEN THE GEAR WAS EXTENDED THE RT GEAR FAILED TO LOCKDOWN, THE SOP`S WERE FOLLOWED, GEAR EMERGENCY BOT
- [SDR CA140305001](https://openairdocs.org/sdr/CA140305001), Feb 10, 2014: STATOR. CRACKED. (CAN) THREE CRACKS FOUND ON OUTER RING WHEN INSPECTING BY BORESCOPE IN NOZZLE HOLES PARTS REMOVED FOR OVERHAUL AND REPLACED.
- [SDR CA131218006](https://openairdocs.org/sdr/CA131218006), Dec 17, 2013: PANEL. CORRODED. (CAN) WHEN DOING AN INSPECTION, A TECH FOUND A FUEL LEAK UNDER THE RT NACELLE FUEL TANK. CLEAN THE PANEL UNDER THE TANK AND A STREAM OF FUEL START TO FLOW. EMPT
- [SDR CA131129005](https://openairdocs.org/sdr/CA131129005), Nov 28, 2013: CONTROL HORN. CRACKED. (CAN) WHILE DOING A PHASE INSPECTION ON THE TAIL SECTION, AN EMPLOYEE FOUND SOME LOOSENESS ON THE LT CONTROL HORN ASSY. THE LT ELEVATOR ASSY HAS BEEN REMOVED TO
- [SDR CA131115001](https://openairdocs.org/sdr/CA131115001), Nov 12, 2013: DRIVE ASSY. FAILED. (CAN) WHILE BACK TRACKING ON THE RUNWAY, FLAPS WE RETRACTED BY FLIGHT CREW AND SHORTLY AFTER A BURNING ODOR WAS NOTICED IN THE CABIN. THE ACFT RETURNED TO THE A
- [SDR CA130925001](https://openairdocs.org/sdr/CA130925001), Sep 21, 2013: WIRE. SHORTED. (CAN) AFTER EXTENSION OF THE LANDING GEAR THERE WAS NO DOWN INDICATION, 3 GREEN. PILOTS COULD HEAR THE LANDING GEAR EXTEND AND COULD FEEL THE PARASITE DRAG BUT 
- [SDR CA130920002](https://openairdocs.org/sdr/CA130920002), Sep 17, 2013: TORQUE KNEE. SHEARED. (CAN) THE FLIGHT CREW FELT A VIBRATION FROM THE RT MLG UPON LANDING. POST FLIGHT WALK AROUND REVEALED THAT THE UPPER TORQUE KNEE ON THE RT MLG HAD SHEARED.
- [SDR CA131103007](https://openairdocs.org/sdr/CA131103007), Sep 14, 2013: INDICATOR. FAILED. (CAN) ON CLIMBOUT THE CREW NOTICED THE RT ATTITUDE GYRO HAD BECOME UNSERVICEABLE. THE FLIGHT CONTINUED WITH OUT INCIDENT TO DESTINATION. MAINTENANCE REPLACED TH

All 472: https://openairdocs.org/model/beech-a100/reports.md

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