# Beech 65-B80 - Type: Aircraft model (FAA registry) - Registry code: 1152812 - Manufacturer (registry): BEECH - Model: 65-B80 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Reciprocating - Seats: 9 - Weight class: Up to 12,499 lb - Cruise speed: 174 mph - Certification: Type certificated - Data sheet: [TCDS 3A20](https://openairdocs.org/tcds/3A20) (OpenAirDocs) - Holder: Textron Aviation Inc. - Registered aircraft: 15 - Page: https://openairdocs.org/model/beech-65-b80 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 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 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 2000-18-02](https://openairdocs.org/ad/2000-18-02): Elevator Skin Assemblies · Textron 56TC, 58, 58P and 12 more. Effective Sep 22, 2000 - [AD 99-05-13 R1 WD](https://openairdocs.org/ad/99-05-13-R1-WD): Withdrawal of AD 99-05-13 · Beech B17B, B17L, B17R (Army UC-43H) and 107 more. Effective Jul 5, 2000 - [AD 98-04-24](https://openairdocs.org/ad/98-04-24): AFM - Limitations Section - Icing · Textron 100, 300, 58 and 13 more. Effective Mar 13, 1998 - [AD 97-16-10](https://openairdocs.org/ad/97-16-10): Filters · Cessna 310R, T310R, 36 and 17 more. Effective Sep 18, 1997 - [AD 95-26-15 R1](https://openairdocs.org/ad/95-26-15-R1): Traffic Alert and Collision Avoidance Systems · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 159 more. Effective Dec 26, 1996 - [AD 89-25-08](https://openairdocs.org/ad/89-25-08): Wing Main Spar Inspection · Textron 65, 65-80, 65-A80 and 1 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 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 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 79-01-02 R2](https://openairdocs.org/ad/79-01-02-R2): In-Flight Fires · Textron 65, 65-80, 65-88 and 17 more. Effective Sep 22, 1980 - [AD 78-11-01](https://openairdocs.org/ad/78-11-01): Powerplant Fires · Textron 65, 65-80, 65-88 and 11 more. Effective Feb 6, 1979 - [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 77-22-01](https://openairdocs.org/ad/77-22-01): Fuselage Structure · Textron 65, 65-80, 65-88 and 11 more. Effective Aug 23, 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 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 76-09-01](https://openairdocs.org/ad/76-09-01): Emergency Exit Door · Textron 65, 65-80, 65-A80 and 5 more. Effective Apr 30, 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 74-16-04](https://openairdocs.org/ad/74-16-04): Restricted Elevator Travel · Textron 65-B80, C90 and E90. Effective Aug 6, 1974 - [AD 69-06-06](https://openairdocs.org/ad/69-06-06): Rudder Spar · Textron 65-80, 65-88, 65-90 and 12 more. Effective Jun 3, 1971 - [AD 66-02-01](https://openairdocs.org/ad/66-02-01): Air Conditioners · Beechcraft 56TC, 58, 58A and 39 more. Effective Feb 10, 1966 Historical (superseded or no longer in force): - [AD 99-05-13](https://openairdocs.org/ad/99-05-13) (historical): Fuel Tank Selector · Beech B17B, B17L, B17R (Army UC-43H) and 107 more. Effective Apr 19, 1999 - [AD 87-22-01 R1](https://openairdocs.org/ad/87-22-01-R1) (historical): Nose Landing Gear Fork · Raytheon 100 Model or Series (all), 1900, 1900C and 50 more. Effective Sep 30, 1989 ## Information bulletins (advisory) (5) - [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) - [N103BA](https://openairdocs.org/aircraft/N103BA): [Bemidji Aviation Services Inc](https://openairdocs.org/faa-owner/BEMIDJI%20AVIATION%20SERVICES%20INC), [Bemidji, MN](https://openairdocs.org/faa-place/MN/Bemidji), built 1971, S/N LD-435 - [N106BA](https://openairdocs.org/aircraft/N106BA): [Bemidji Aviation Services Inc](https://openairdocs.org/faa-owner/BEMIDJI%20AVIATION%20SERVICES%20INC), [Bemidji, MN](https://openairdocs.org/faa-place/MN/Bemidji), built 1969, S/N LD-409 - [N110BA](https://openairdocs.org/aircraft/N110BA): [Bemidji Aviation Services Inc](https://openairdocs.org/faa-owner/BEMIDJI%20AVIATION%20SERVICES%20INC), [Bemidji, MN](https://openairdocs.org/faa-place/MN/Bemidji), built 1966, S/N LD-279 - [N131BA](https://openairdocs.org/aircraft/N131BA): [Bemidji Aviation Svcs Inc](https://openairdocs.org/faa-owner/BEMIDJI%20AVIATION%20SVCS%20INC), [Bemidji, MN](https://openairdocs.org/faa-place/MN/Bemidji), built 1966, S/N LD-297 - [N132BA](https://openairdocs.org/aircraft/N132BA): [Bemidji Aviation Services Inc](https://openairdocs.org/faa-owner/BEMIDJI%20AVIATION%20SERVICES%20INC), [Bemidji, MN](https://openairdocs.org/faa-place/MN/Bemidji), S/N LD-331 - [N2038W](https://openairdocs.org/aircraft/N2038W): [Yanagida Kazuaki](https://openairdocs.org/faa-owner/YANAGIDA%20KAZUAKI), [Norco, CA](https://openairdocs.org/faa-place/CA/Norco), built 1973, S/N LD-459 - [N306D](https://openairdocs.org/aircraft/N306D): [Bemidji Aviation Services Inc](https://openairdocs.org/faa-owner/BEMIDJI%20AVIATION%20SERVICES%20INC), [Bemidji, MN](https://openairdocs.org/faa-place/MN/Bemidji), S/N LD-439 - [N44MA](https://openairdocs.org/aircraft/N44MA): [Pacific Mission Aviation](https://openairdocs.org/faa-owner/PACIFIC%20MISSION%20AVIATION), [Hagatna, GU](https://openairdocs.org/faa-place/GU/Hagatna), S/N LD-412 - [N46MA](https://openairdocs.org/aircraft/N46MA): [Pacific Mission Aviation](https://openairdocs.org/faa-owner/PACIFIC%20MISSION%20AVIATION), Yap, built 1969, S/N LD-413 - [N648DC](https://openairdocs.org/aircraft/N648DC): [Somerset Regional Water Resources](https://openairdocs.org/faa-owner/SOMERSET%20REGIONAL%20WATER%20RESOURCES), [Friedens, PA](https://openairdocs.org/faa-place/PA/Friedens), S/N LD-351 - [N747VW](https://openairdocs.org/aircraft/N747VW): [Hammer Aviation LLC](https://openairdocs.org/faa-owner/HAMMER%20AVIATION%20LLC), [Miami, FL](https://openairdocs.org/faa-place/FL/Miami), built 1967, S/N LD-360 - [N7502N](https://openairdocs.org/aircraft/N7502N): [Bemidji Aviation Services Inc](https://openairdocs.org/faa-owner/BEMIDJI%20AVIATION%20SERVICES%20INC), [Bemidji, MN](https://openairdocs.org/faa-place/MN/Bemidji), S/N LD-391 - [N7817L](https://openairdocs.org/aircraft/N7817L): [Nyerges James](https://openairdocs.org/faa-owner/NYERGES%20JAMES), [Midland, TX](https://openairdocs.org/faa-place/TX/Midland), built 1967, S/N LD-340 - [N80RR](https://openairdocs.org/aircraft/N80RR): [Bemidji Aviation Services Inc](https://openairdocs.org/faa-owner/BEMIDJI%20AVIATION%20SERVICES%20INC), [Bemidji, MN](https://openairdocs.org/faa-place/MN/Bemidji), built 1966, S/N LD-296 - [N810AD](https://openairdocs.org/aircraft/N810AD): [Gulf States Air Inc](https://openairdocs.org/faa-owner/GULF%20STATES%20AIR%20INC), [Bossier City, LA](https://openairdocs.org/faa-place/LA/Bossier%20City), S/N LD-328 ## STCs approved for it (201, first 50) - [STC SA00024NY](https://openairdocs.org/stc/SA00024NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine fixed wing light aircraft incorporating Lycoming reciprocating engines of 450 horsepower or less.. Airwolf Filter Corporation - [STC SA00061LA](https://openairdocs.org/stc/SA00061LA): Installation of JPI digital tachometer.. J P Instruments - [STC SA00068SE](https://openairdocs.org/stc/SA00068SE): Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1). Electronics International Inc. - [STC SA00149BO](https://openairdocs.org/stc/SA00149BO): Installation of Aircraft Components, Inc. Volt and Vac Alert System, P/N 2044-1. Aircraft Components 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 SA00237WI](https://openairdocs.org/stc/SA00237WI): Installation of a Bendix/King EFIS-4 0electronic flight instrument system. Elliott Aviation Technical Products - [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 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 SA00432SE](https://openairdocs.org/stc/SA00432SE): Installation of EGT 701 series fuel flow instrument.. J P Instruments - [STC SA00622WI](https://openairdocs.org/stc/SA00622WI): Shoulder harness anchor installation. Aviation Fabricators Inc - [STC SA00729SE](https://openairdocs.org/stc/SA00729SE): Installation of twin temperature indicating system with fuel flow in accordance with J.P. Instruments (JPI) Installation manual Report No. 760, Revision -, dated 7/20/99, or later FAA approved revision.. J P Instruments - [STC SA00744DE](https://openairdocs.org/stc/SA00744DE): Installation of the Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT31 Transponder and an approved position sensor. Peregrine - [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 SA00756DE](https://openairdocs.org/stc/SA00756DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT22 Transponder and an approved Global Positioning System (GPS) Position Sensor. Peregrine - [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine - [STC SA00780SE](https://openairdocs.org/stc/SA00780SE): Installation of the True Lock Safety Retention Axle Lock Nut System. True Lock LLC - [STC SA00804SE](https://openairdocs.org/stc/SA00804SE): Installation of an engine failure indicator system, also referred to as a 'low Thrust Detector system.'. Advanced Aero Safety Inc. - [STC SA00861SE](https://openairdocs.org/stc/SA00861SE): Installation of J.P. Instruments (JPI) fuel flow indicating system. J P Instruments - [STC SA00865AT-D](https://openairdocs.org/stc/SA00865AT-D): Installation of replacement fuel cell assemblies. FFC Manufacturing - [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 SA01157LA](https://openairdocs.org/stc/SA01157LA): Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument.. Electronics International Inc. - [STC SA01158WI](https://openairdocs.org/stc/SA01158WI): Installation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System.. Aero Enhancements 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 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 SA01280CH](https://openairdocs.org/stc/SA01280CH): Installation of Challenger Spin-On Oil Filters.(For Cessna 182 model, s/n 67042 and up) (For Cessna 421C model, s/n 1017 thru 1404). D & K Aviation - [STC SA01335AT-D](https://openairdocs.org/stc/SA01335AT-D): Installation of replacement fuel cell assemblies. FFC Manufacturing - [STC SA01452CH](https://openairdocs.org/stc/SA01452CH): Installation of an air ambulance conversion kit.. Med-Pac Inc. - [STC SA01473SE (5 OF 5)](https://openairdocs.org/stc/SA01473SE%20(5%20OF%205)): Installation of a GTX 32 (mode C), GTX 33 (mode S), or GTX 33D (mode S with diversity) Remote Transponde. Garmin AT Inc. - [STC SA01487SE (4 OF 5)](https://openairdocs.org/stc/SA01487SE%20(4%20OF%205)): Installation of a GDL 69 or GDL 69A XM Satellite Receiver in accordance with Garmin Supplemental Type Certificate Master Data List, P/N 005-C0217-00, Revision A, dated December 20, 2004, or later FAA approved revision.. Garmin AT Inc. - [STC SA01487SE-D](https://openairdocs.org/stc/SA01487SE-D): Installation of a GDL 69 or GDL 69A XM Satellite Receiver. Garmin International Inc - [STC SA01625AT-D](https://openairdocs.org/stc/SA01625AT-D): Installation of replacement fuel cell assemblies. FFC Manufacturing - [STC SA01626AT-D](https://openairdocs.org/stc/SA01626AT-D): Installation of replacement fuel cell assemblies. FFC Manufacturing - [STC SA01639NY](https://openairdocs.org/stc/SA01639NY): Replacement of 12 refrigerant in air conditioning system with Enviro Refrigerant Hotshot R414B.. Scale Modelbuilders Inc. - [STC SA01670SE](https://openairdocs.org/stc/SA01670SE): Installation of a GWX 68 Weather Radar. Garmin AT Inc. - [STC SA01670SE-D](https://openairdocs.org/stc/SA01670SE-D): Installation of a GWX 68 Weather Radar. Garmin International Inc - [STC SA01692SE (PAGE 1 OF 2)](https://openairdocs.org/stc/SA01692SE%20%20(PAGE%201%20OF%202)): Installation of a Garmin GMX 200 Multi-Function Display. Garmin International Inc - [STC SA01695SE (5 OF 5)](https://openairdocs.org/stc/SA01695SE%20(5%20OF%205)): Installation of an antenna. Garmin AT Inc. - [STC SA01714WI (2 OF 2)](https://openairdocs.org/stc/SA01714WI%20(2%20OF%202)): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems.. Garmin International Inc - [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.. TCW Technologies, LLC - [STC SA01809WI](https://openairdocs.org/stc/SA01809WI): Installation of an Operator Seat onto an existing Cabin Seat Track.. Aviation Fabricators Inc All 201: https://openairdocs.org/model/beech-65-b80/stcs.md ## NTSB investigations (26) 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 ANC24LA065](https://openairdocs.org/ntsb/ANC24LA065), Jul 12, 2024: Beech 65-B80 (N44MA), Woleai Atoll, Micronesia, substantial damage. Probable cause: The pilot's selection of an unsuitable takeoff area, resulting in a loss of directional control. Contributing to the accident was a flooded runway. - [NTSB CEN13CA129](https://openairdocs.org/ntsb/CEN13CA129), Jan 11, 2013: Beech 65-B80 (N110BA), Alexandria, MN, substantial damage. Probable cause: The pilot’s failure to stop the airplane on the downsloping, ice-contaminated runway after landing with a tailwind. Contributing to the accident was the pilot’s failure to account for the wind… - [NTSB CEN10LA127](https://openairdocs.org/ntsb/CEN10LA127), Feb 24, 2010: Hawker Beechcraft 65-B80 (N132BA), Minneapolis, MN, minor damage. Probable cause: The pilot of the other airplane not setting the parking brake adequately while holding for departure. Contributing to the accident was the pilot of the other airplane being distracted while doing his… - [NTSB CHI01LA082](https://openairdocs.org/ntsb/CHI01LA082), Feb 8, 2001: Beech 65-B80 (N107BA), Sioux Falls, SD, substantial damage. Probable cause: The pilot initiated the flight into known icing conditions which resulted in his ability to maintain control of the airplane. Factors associated with the accident were the ice accumulation and the… - [NTSB FTW00LA095](https://openairdocs.org/ntsb/FTW00LA095), Mar 10, 2000: Beech 65-B80 (N8071R), Midland, TX, substantial damage. Probable cause: The separation of the right main landing gear tire tread which resulted in damage to the right main landing gear mounting structure. - [NTSB CHI99LA008](https://openairdocs.org/ntsb/CHI99LA008), Oct 17, 1998: Beech 65-B80 (N138BA), Brainerd, MN, substantial damage. Probable cause: the pilot's failure to maintain the proper glidepath and his diversion of attention during a critical phase of flight. - [NTSB FTW96FA027](https://openairdocs.org/ntsb/FTW96FA027), Oct 26, 1995: Beech 65-B80 (N9NP), Paint Rock, TX, destroyed, 1 fatal. Probable cause: The pilot's impairment of judgment and performance due to alcohol which resulted in his improper decision to shutdown an engine, and his failure to maintain adequate airspeed for single-engine flight. - [NTSB CHI95LA287](https://openairdocs.org/ntsb/CHI95LA287), Aug 20, 1995: Beech 65-B80 (N8347N), Anderson, IN, substantial damage. Probable cause: seizure of the landing gear wheel bearing and separation of the landing gear outer wheel-half and tire from the aircraft after which directional control of the aircraft by the pilot was not possible. - [NTSB CHI95FA124](https://openairdocs.org/ntsb/CHI95FA124), Apr 12, 1995: Beech 65-B80 (N7057J), Great Bend, ND, destroyed, 1 fatal. Probable cause: the pilot/mechanic's inadequate maintenance (inspection) of aircraft and the pilot's failure to maintain airspeed (VMC). Factors were icing conditions, deteriorated induction air ducting, and failure… - [NTSB MIA94LA149](https://openairdocs.org/ntsb/MIA94LA149), May 23, 1994: Beech 65 (N6166Y), Pensacola, FL, minor damage. Probable cause: IMPROPER INSTALLATION OF NUTS ON THE NOSEWHEEL (SPLIT RIM) THROUGH-BOLTS BY UNKNOWN PERSONNEL, WHICH RESULTED IN A SUBSEQUENT FAILURE (SEPARATION OF THE WHEEL HALVES). - [NTSB MIA91LA151](https://openairdocs.org/ntsb/MIA91LA151), May 25, 1991: Beech 80 (N5128Y), Fort Lauderdale, FL, destroyed. Probable cause: THE IMPROPER MAINTENANCE WORK BY AN UNKNOWN PERSON WHO CROSSTHREADED A FUEL NOZZLE INJECTOR FITTING WHICH ALLOWED FUEL TO LEAK ON THE EXHAUST SYSTEM INITIATING A FIRE. NO REASON FOR THE RIGHT ENGINE… - [NTSB MKC90LA039](https://openairdocs.org/ntsb/MKC90LA039), Dec 13, 1989: Beech 80 (N525GT), Cape Girardeau, MO, substantial damage. Probable cause: AN INOPERATIVE LANDING GEAR EXTENSION SYSTEM DUE TO FAILURE OF AN ELECTRIC MOTOR AND A MISPLACED EMERGENCY CRANK HANDLE. - [NTSB MKC89LA198](https://openairdocs.org/ntsb/MKC89LA198), Sep 21, 1989: Beech 80 (N132BA), Littlefork, MN, substantial damage. Probable cause: TOTAL FAILURE OF THE ELECTRICAL SYSTEM DURING IFR OPERATIONS & THE AIRCRAFT'S COLLISION WITH A ROCK FENCE DURING THE SUBSEQUENT GEAR-UP PRECAUTIONARY LANDING. - [NTSB ATL85LA087](https://openairdocs.org/ntsb/ATL85LA087), Feb 1, 1985: Beech B-80 (N640K), Newbern, NC, substantial damage - [NTSB LAX82DA335](https://openairdocs.org/ntsb/LAX82DA335), Sep 5, 1982: Schleicher ASW-20 (N44MA), California City, CA, substantial damage - [NTSB MIA81FA102](https://openairdocs.org/ntsb/MIA81FA102), Jul 28, 1981: Beech 65-B80 (N1028C), Groveland, FL, destroyed, 2 fatal - [NTSB ATL81FA062](https://openairdocs.org/ntsb/ATL81FA062), Apr 10, 1981: Beech 65-B80 (N3768Z), Pine Knot, KY, destroyed, 2 fatal - [NTSB MIA77DA070](https://openairdocs.org/ntsb/MIA77DA070), Jul 12, 1977: Beech 65B80 (N99JL), Ponce, PR, destroyed - [NTSB MIA77DKT56](https://openairdocs.org/ntsb/MIA77DKT56), Mar 29, 1977: Beech 65 (N580CA), W.Palm Beach, FL, substantial damage - [NTSB MIA74FKG57](https://openairdocs.org/ntsb/MIA74FKG57), Mar 11, 1974: Beech 65-B80 (N208E), Thomasville, GA, substantial damage - [NTSB DEN72AD055](https://openairdocs.org/ntsb/DEN72AD055), May 19, 1972: Beech 65-B80 (N841NS), Albuquerque, NM, destroyed, 9 fatal - [NTSB SEA72AS033](https://openairdocs.org/ntsb/SEA72AS033), Feb 20, 1972: Beech 65-B80 (N1027C), Fairfield, ID, destroyed, 5 fatal - [NTSB SEA72AS024](https://openairdocs.org/ntsb/SEA72AS024), Dec 16, 1971: Beech 65-B80 (N1028C), Mccall, ID, substantial damage - [NTSB UNK72X0102](https://openairdocs.org/ntsb/UNK72X0102), Dec 10, 1971: Beech 65-B80 (N929V), Frbshr By, Canada, destroyed, 3 fatal - [NTSB DEN70A0023](https://openairdocs.org/ntsb/DEN70A0023), Oct 3, 1969: Beech 65-B80 (N590CA), Denver, CO, destroyed, 5 fatal - [NTSB NYC70I0039](https://openairdocs.org/ntsb/NYC70I0039), Sep 30, 1969: Beech B80 (N9525Q), Oneonta, NY, incident, minor damage ## FAA accident and incident reports (37) 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 20240711014619A](https://openairdocs.org/incident/20240711014619A), Jul 11, 2024: Beech 65-B80 (N44MA), Woleai, Substantial damage. Pilot performed a short field takeoff and accelerated the airplane to approximately 60MPH upon reaching the low spot of the runway. As the nose wheel hit the… - [Accident 20130111000379A](https://openairdocs.org/incident/20130111000379A), Jan 11, 2013: Beech 65-B80 (N110BA), Alexandria, MN, Substantial damage. Pilot on IFR flight plan from msp to axn decided to land on rwy 31 at axn with wind 190 @ 8 knots. Decision to land on 31 with a tailwind was made due to rwy… - [Accident 20100224028141A](https://openairdocs.org/incident/20100224028141A), Feb 24, 2010: Beech 65-B80 (N132BA), Minneapolis, MN, Substantial damage. Right engine prop 2 blades curled. 1 blade lost some metal with nicks and scratches. Sudden engine stoppage. Minor scratches on right top side of nose section.… - [Incident 20010831030229I](https://openairdocs.org/incident/20010831030229I), Aug 31, 2001: Beech 65B80 (N131BA), Marshall, MN, Minor damage. (-23) 08/31/2001 On landing roll out at Marshall, MN, pilot reached for the wing flap control to raise them. He assumes that he moved the landing gear handle… - [Accident 20010207009979A](https://openairdocs.org/incident/20010207009979A), Feb 7, 2001: Beech 65B80 (N107BA), Sioux Falls, SD, No damage. (.19)On February 7, 2001, at 2030 central standard time, a Beech 65-B80, N107BA, operated by bemidji aviation services, as bemidji flight 25, collided with… - [Accident 20000310039849A](https://openairdocs.org/incident/20000310039849A), Mar 10, 2000: Beech 65B80 (N8071R), Midland, TX, Substantial damage. (.4)On March 10, 2000, at 1705 central standard time, a Beech 65-B80 twin-engine airplane, N8071R, was substantially damaged during landing at the Midland… - [Accident 19991115046839A](https://openairdocs.org/incident/19991115046839A), Nov 15, 1999: Beech 65B80 (N8071R), Midland, TX, No damage. (-23)This commerical pilot was operating under 14 CFR part 135 on a cargo flight in visual meteorological conditions. During his takeoff roll a deer ran across… - [Incident 19990312039109I](https://openairdocs.org/incident/19990312039109I), Mar 12, 1999: Beech 65B80 (N900NH), Keystone Height, FL, Minor damage. Pilot forgot to lower landing gear: aircraft landed gear up. Minor damage. - [Accident 19981017029469A](https://openairdocs.org/incident/19981017029469A), Oct 17, 1998: Beech 65B80 (N138BA), Brainerd, MN, Substantial damage. (.19) On October 17, 1998, at 0033 central daylight time, a Beech 65-B80, N138BA, registered to bemidji aviation services, inc. of bemidji, Minnesota, and… - [Incident 19970422012749I](https://openairdocs.org/incident/19970422012749I), Apr 22, 1997: Beech 65B80 (N95HM), Christiansted, U.S. Virgin Islands, Substantial damage. Narrative: see accompanying sheet for pilot statement. Damage to aircraft: engine broke from top lord mounts. Fire caused substantial damage to engine and… - [Accident 19951026034599A](https://openairdocs.org/incident/19951026034599A), Oct 26, 1995: Beech 65B80 (N9NP), Paint Rock, TX, Destroyed, 1 fatal. Indicates lost power right engine. Mishandled fuel system. Below VMC. No engine defects. Alcohol impairment. - [Accident 19950820025729A](https://openairdocs.org/incident/19950820025729A), Aug 20, 1995: Beech 65B80 (N8347N), Anderson, IN, Substantial damage. Lost directional control on takeoff skidded sideways off runway. Folded main gear. Wheel assembly broke up. (-23) aircraft started a take off with eleven… - [Accident 19950412007539A](https://openairdocs.org/incident/19950412007539A), Apr 12, 1995: Beech 65B80 (N7057J), Great Bend, ND, Destroyed, 1 fatal. Began icing at cruise. Descended lost one engine other rough. Lost control air duct blocked. Burnt piston. (-23) the left engine failed due to failure of the… - [Accident 19940524016439A](https://openairdocs.org/incident/19940524016439A), May 24, 1994: Beech 65 (N6166Y), Pensacola, FL, Minor damage. Nose wheel split rim exploded. Tire rim severed ground observers leg. Improper thru bolt nuts. Over inflated tire. - [Incident 19920527022909I](https://openairdocs.org/incident/19920527022909I), May 27, 1992: Beech 65B80 (N106BA), Minneapolis, MN. Electrical failure on climb. Returned. Manually lowered gear. Wire shorted causing both voltage regulators to fail - [Accident 19910525017269A](https://openairdocs.org/incident/19910525017269A), May 25, 1991: Beech 65B80 (N5128Y), Fort Lauderdale, FL, Destroyed. Lost both engines. Hit vehicle on freeway on landing. Fuel line leaking left engine. Water in fuel right engine. - [Incident 19901022053989I](https://openairdocs.org/incident/19901022053989I), Oct 22, 1990: Beech 65B80 (N7806L), Las Vegas, NV. Propeller came off engine. Landed safely. Enforcement action against mechanic who installed propeller. - [Accident 19890921035709A](https://openairdocs.org/incident/19890921035709A), Sep 21, 1989: Beech 6580 (N132BA), Little Fork, MN, Substantial damage. Lost electrical power elected to land gear up slid into stone fence. Found broken wire shorted on cannon plug. - [Incident 19890215020179I](https://openairdocs.org/incident/19890215020179I), Feb 15, 1989: Beech 65B80 (N107BA), Redwood Falls, MN. Right engine lost fuel pressure and failed en route then left engine roughened. Fuel servo and ice in fuel factors. - [Incident 19871027078949I](https://openairdocs.org/incident/19871027078949I), Oct 27, 1987: Beech 65B80 (N107BA), Hibbing, MN, Minor damage. Landing gear collapsed because it was never fully extended and locked. Cause generators were never turned on. - [Incident 19870517033259I](https://openairdocs.org/incident/19870517033259I), May 17, 1987: Beech 65B80 (N240), Ft Lauderdale, FL, Minor damage. Right main tire blew on touchdown. Aircraft departed runway side into a sandy area. - [Incident 19870129004949I](https://openairdocs.org/incident/19870129004949I), Jan 29, 1987: Beech 65B80 (N103BA), Hibbing, MN, Minor damage. During rollout aircraft struck a coyote. Landing gear torque knee failed but runway heading was maintained on snow. - [Incident 19851008056389I](https://openairdocs.org/incident/19851008056389I), Oct 8, 1985: Beech 65B80 (N306D), Bryce Canyon, UT, Minor damage. All deice equipment working during climb. Picked up heavy under wing ice. Uncontrolled descent, possibly overstress - [Accident 19850201073539A](https://openairdocs.org/incident/19850201073539A), Feb 1, 1985: Beech 65B80 (N640K), Newbern, NC, Substantial damage. Left engine fire at start of visual approach. Engine shut down and fire went out. Cause undetermined due to damage - [Incident 19841231059939I](https://openairdocs.org/incident/19841231059939I), Dec 31, 1984: Beech 65B80 (N80JF), Anchorage, AK, Minor damage. Gear collapsed on landing. Damage to gear and propellers. Cause has not been determined. Aircraft sitting on jacks. - [Accident 19820905043902A](https://openairdocs.org/incident/19820905043902A), Sep 5, 1982: Schler ASW20 (N44MA), California City, CA, Minor damage. Was overtaken and struck by N214T while both gliders were circling with others in a thermal to gain altitude. - [Accident 19810728047539A](https://openairdocs.org/incident/19810728047539A), Jul 28, 1981: Beech 65B80 (N1028C), Groveland, FL, Destroyed, 1 fatal. Overdue aircraft found crashed and burned on cleared strip. No ownership claimed. Possible illegal drug flight. - [Accident 19810410015739A](https://openairdocs.org/incident/19810410015739A), Apr 10, 1981: Beech 65 (N3768Z), Pine Knot, KY, Destroyed. Aircraft crashed during takeoff for unknown reason. Pilot not qualified and aircraft over gross. - [Incident 19800215021259I](https://openairdocs.org/incident/19800215021259I), Feb 15, 1980: Rkwell NA26560 (N9NP), Salt Lake City, UT, Minor damage. Loose connection in circuit breaker bus strip caused sufficient heat to ignite insulating pad. - [Incident 19800105013639I](https://openairdocs.org/incident/19800105013639I), Jan 5, 1980: Beech 6580 (N67031), Riverton, WY, Minor damage. Pilot took off with right generator inoperative. Left generator failed in flight. Pilot landed gear up. - [Incident 19790615016349I](https://openairdocs.org/incident/19790615016349I), Jun 15, 1979: Beech 65B80 (N121E), Gainesville, FL. Pilot departed for controlled airport in IFR weather, no clearance. Was handled by approach control to departure. - [Incident 19780720035679I](https://openairdocs.org/incident/19780720035679I), Jul 20, 1978: Beech 6580 (N7833L), Indianapolis, IN, Minor damage. Pilot returned with engine on fire. Cylinder failed, blew off intake hoses and intake filter. - [Incident 19780427013799I](https://openairdocs.org/incident/19780427013799I), Apr 27, 1978: Boeing 80A (N128Z), Medicine Bow, WY. Fuel entering cockpit near fuel gauge. Engine shut down. Diaphram in fuel gauge ruptured. - [Incident 19780416010859I](https://openairdocs.org/incident/19780416010859I), Apr 16, 1978: Rkwell NA265 (N9NP), Washington, DC. Pilot reported unsafe gear indication while preparing to land. Switch was loose on gear. Clamp tightened. - [Accident 19770712032289A](https://openairdocs.org/incident/19770712032289A), Jul 12, 1977: Beech 65B80 (N99JL), Ponce, Destroyed. Ditched abt 32MI sse Ponce VOR.both fuel flowmeters,l eng alternator inop. Wet comp 20-30DEG error. - [Accident 19770329020299A](https://openairdocs.org/incident/19770329020299A), Mar 29, 1977: Beech A658200 (N580CA), W.Palm Beach, FL, Substantial damage. Aircraft had 1670LBS marijuana aboard. Injury index presumed. - [Accident 19740311006639A](https://openairdocs.org/incident/19740311006639A), Mar 11, 1974: Beech 65B80 (N208E), Thomasville, GA, Substantial damage. Eng fire after lndg. Fuel line b nut fm reg unit to nozzle loose.b nut loose at fuel flow modulator ## Service difficulty reports (55, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR 2024F00317](https://openairdocs.org/sdr/2024F00317), Dec 10, 2024: DISPLAY. FAILED. GARMIN 600 PFD FAILED IN CRUISE FLIGHT - [SDR BEMA202111170001](https://openairdocs.org/sdr/BEMA202111170001), Nov 16, 2021: HEATER. ODOR. PILOT REPORTED SEEING A FLASH OF LIGHT AND A BURNING SMELL COMING FROM BELOW THE INTERMENT PANEL ON THE R/H SIDE BY THE RUDDER PEDDLES AREA. THE PILOT REPORTED - [SDR BEMA20201028001](https://openairdocs.org/sdr/BEMA20201028001), Oct 23, 2020: CONNECTING ROD. BROKEN. PILOT NOTICED ONSET OF SIGNIFICANT VIBRATION, FOLLOWED BY OIL PRESSURE LOSS. SHUT DOWN LT ENGINE ON FINAL AT KMSP. PILOT NOTIFIED MSP TOWER OF ENGINE FAILURE. O - [SDR BEMA52](https://openairdocs.org/sdr/BEMA52), Nov 8, 2011: MOTOR. DAMAGED. LANDING GEAR WOULD NOT RETRACT ELECTRICALLY AND HAD TO BE PUMPED DOWN CAUSING AN UNSCHEDULED LANDING IN BJI. REMOVED LANDING GEAR MOTOR AND FOUND STRIPPED TEETH - [SDR BEMA 110BA](https://openairdocs.org/sdr/BEMA%20110BA), Apr 27, 2011: ELECTRICAL SYS. ERRATIC. AVIONICS POWER FAILURE RESULTING IN AN UNSCHEDULED LANDING CAUSED BY SUSPECTED AVIONICS CIRCUIT BREAKER FAILURE. - [SDR CVU2010F00001](https://openairdocs.org/sdr/CVU2010F00001), Apr 7, 2010: ALTERNATOR. DEFECTIVE. DURING RUNUP, THE RT VOLT/AMP METER SHOWED ONLY BATTERY VOLTAGE WHICH INDICATED A PROBLEM WITH THE RT ALTERNATOR. AFTER FURTHER TESTING AND INSPECTION, IT WAS D - [SDR CVU2010F00000](https://openairdocs.org/sdr/CVU2010F00000), Jan 4, 2010: ACTUATOR. MALFUNCTIONED. THE RT MLG FREEFELL TO THE DOWN AND LOCKED POSITION WHILE THE GEAR WAS BEING EXTENDED. INSP REVEALED FAILURE OF THE NUT INSIDE ASSY NR 50-8103672. REPLACED BOTH - [SDR CVU2009F00001](https://openairdocs.org/sdr/CVU2009F00001), Nov 6, 2009: FORK. CRACKED. DURING A RECURRENT INSP REQUIRED BY AD 2004-23-02C, A CRACK WAS FOUND AT THE LOCATION ILLUSTRATED. WERE THE WELD MEETS THE SURFACE, AFTER USING DYE PENETRANT TH - [SDR CVU2009F00000](https://openairdocs.org/sdr/CVU2009F00000), Feb 3, 2009: STARTER. NOISY. ON STARTUP, ONCE THE BENDIX GEAR ENGAGED, A LOUD NOISE WAS HEARD, WHICH SOUNDED LIKE GEARS GRINDING. UPON CLOSER INSP, NO TEETH REMAINED ATTACHED TO THE BENDIX. - [SDR CVU2008F00000](https://openairdocs.org/sdr/CVU2008F00000), Jul 7, 2008: STARTER. INTERMITTENT. PART REMOVED FOR OVERHAUL AFTER INTERMITTENT OPERATION. (K) - [SDR 2008FA0000468](https://openairdocs.org/sdr/2008FA0000468), Jul 1, 2008: HINGE. CRACKED. (2) OF THE HINGE LINKS HAD CRACKED OFF ON ONE END. UPON DISASSEMBLY IT WAS DETERMINED THAT A CRACK HAD FORMED LENGTHWISE BETWEEN THE FASTENERS AND THE HINGE LIN - [SDR 2008FA0000240](https://openairdocs.org/sdr/2008FA0000240), Mar 7, 2008: BOLT. FAILED. NR 1 ENGINE SHUTDOWN IN FLIGHT. SUSPECTED NR 7 CONNECTING ROD BOLT FAILURE. CAUSING CYL SEPARATION FROM CASE AND CRANK CASE CRACK. AC LANDED SAFELY WITHOUT OTHE - [SDR 2006FA0001212](https://openairdocs.org/sdr/2006FA0001212), Nov 22, 2006: BELLCRANK. CRACKED. A CRACK WAS FOUND ON THE RT BELLCRANK SUPPORT ASSY. DURING A MANDITORY 5 YEAR INSPECTION IAW MSB 2231 REV 1. (K) - [SDR CVU2006F00000](https://openairdocs.org/sdr/CVU2006F00000), Feb 2, 2006: CAMSHAFT. WORN. SMALL PARTICLES OF METAL FOUND IN OIL. IDENTIFIED NR 5 AND NR 6 CAM AND ASSOCIATED LIFTERS WORN. REMOVED FOR REPAIR. RECOMMEND THE USE OF 16702 ENGINE OIL ADDIT - [SDR AU510001770](https://openairdocs.org/sdr/AU510001770), Dec 12, 2005: GASKET. FAILED. RT ENGINE OIL COOLER LOWER FITTING GASKET FAILED. LOSS OF ENGINE OIL. - [SDR CVU2005F00003](https://openairdocs.org/sdr/CVU2005F00003), Aug 18, 2005: SHAFT. SHEARED. PUMP FAILED UNDER NORMAL OPERATING CONDITIONS (VFR, DAY). - [SDR CVU2005F00002](https://openairdocs.org/sdr/CVU2005F00002), Jul 15, 2005: LIFTER. WORN. SMALL METAL FLAKES KEPT RE-APPEARING IN THE OIL SCREENS. FOUND WORN CAM NR 5 AND NR 6 CYLINDER INTAKE VALVES. ENGINES REMOVED FOR REPAIR. USE MFG ENGINE OIL ADD - [SDR CVU2005F00001](https://openairdocs.org/sdr/CVU2005F00001), Jul 15, 2005: CAMSHAFT. WORN. SMALL METAL FLAKES KEPT RE-APPEARING IN THE OIL SCREENS. FOUND WORN CAM NR 5 AND NR 6 CYLINDER INTAKE VALVES. ENGINES REMOVED FOR REPAIR. USE MFG ENGINE OIL ADD - [SDR 2004F00431](https://openairdocs.org/sdr/2004F00431), Dec 3, 2004: RING GEAR. CRACKED. OPERATOR REPORTED THAT THE LEFT ENGINE WAS SHUT DOWN AND THE PROPELLER FEATHERED DUE TO ROUGH RUNNING ENGINE SHORTLY AFTER TAKEOFF. MECHANIC INSPECTED ENGINE AF - [SDR CVU2005F00000](https://openairdocs.org/sdr/CVU2005F00000), Nov 23, 2004: PUMP. FAILED. PUMP FAILED UNDER NORMAL OPERATING CONDITIONS. (VFR, DAY) (K) - [SDR CVU2004F00000](https://openairdocs.org/sdr/CVU2004F00000), Sep 23, 2004: PUMP. FAILED. VACUUM PUMP FAILED UNDER NORMAL OPERATING CONDITIONS. (VFR DAY) - [SDR CVU2003F00000](https://openairdocs.org/sdr/CVU2003F00000), Sep 20, 2003: PUMP. FAILED. PUMP FAILED UNDER NORMAL OPERATING CONDITIONS (VFR DAY). - [SDR 2003FA0000197](https://openairdocs.org/sdr/2003FA0000197), Feb 12, 2003: PUMP. FAILED. VACUUM PUMP FAILED UNDER NORMAL OPERATING CONDITIONS. - [SDR 2003FA0000076](https://openairdocs.org/sdr/2003FA0000076), Dec 16, 2002: PUMP. FAILED. PUMP FAILED UNDER NORMAL OPERATING CONDITIONS. - [SDR 2002FA0001123](https://openairdocs.org/sdr/2002FA0001123), Sep 19, 2002: POINTS. MELTED. MELTING OF NYLON WHERE IT CONTACTS POINT ARM DURING OPENING AND CLOSING OF POINTS DURING OPERATION. INFERIOR NYLON USED, NOT RESISTANT TO WEAR OR HEAT. - [SDR CVU2002F00001](https://openairdocs.org/sdr/CVU2002F00001), Dec 20, 2001: PUMP. FAILED. VACUUM PUMP, PUMP FAILED UNDER NORMAL OPERATING CONDITIONS. - [SDR CVU2002F00000](https://openairdocs.org/sdr/CVU2002F00000), Dec 15, 2001: MAGNETO. DAMAGED. PRIMARY COIN HOLD DOWN RETAINERS LOOSE WITHIN MAGNETO CASE. THE LOOSE RETAINERS, IN TURN, GOT CAUGHT IN THE TIMING WHEEL/GEAR AND CHEWED UP SEVERAL TEETH. PROBA - [SDR BEM2001F00000](https://openairdocs.org/sdr/BEM2001F00000), Oct 9, 2001: MOTOR. DAMAGED. FLAPS FAILED TO MOVE. - [SDR 2001FA0000052](https://openairdocs.org/sdr/2001FA0000052), Jun 6, 2001: PLATE. CORRODED. DURING ANNUAL INSPECTION, UPPER AND MID RUDDER ATTACH FITTING PLATES (THESE CONTAIN THE BEARINGS) WERE FOUND TO BE SEVERELY EXFOLIATED. THE UPPER RUDDER ATTACH - [SDR 20000720SH034](https://openairdocs.org/sdr/20000720SH034), Jun 26, 2000: SPRING. CRACKED. EXHAUST VALVE SPRING RETAINING CAP BROKE IN HALF AND BURNED EXHAUST VALVE. (X) - [SDR AU981058](https://openairdocs.org/sdr/AU981058), Aug 17, 1998: FUEL CELL. LEAKING. (AUS) REAR OUTBOARD AND LEADING EDGE FUEL TANKS P/N 50T389034-8 AND P/N 50-921552-8 LEAKING. - [SDR AU981057](https://openairdocs.org/sdr/AU981057), Aug 17, 1998: FUEL CELL. LEAKING. (AUS) RIGHT INBOARD FUEL CELL LEAKING IN AREA ADJACENT TO THE RT ENGINE NACELLE. - [SDR 98ZZZX2638](https://openairdocs.org/sdr/98ZZZX2638), Jun 30, 1998: PUMP. FAILED. VACUUM PUMP FAILED DURING FLIGHT TRAINING OPERATIONS. WHEN MAXIMUM TAKEOFF POWER WAS USED. - [SDR 98ZZZX2598](https://openairdocs.org/sdr/98ZZZX2598), Jun 11, 1998: STUD. FAILED. CYLINDER HOLD DOWN STUD BROKE UNDER NUT. SUSPECT DEFECTIVE STUD. - [SDR 98ZZZX1478](https://openairdocs.org/sdr/98ZZZX1478), Apr 6, 1998: TIRE. LEAK. SUBMITTER STATED OPERATION HAS BEEN HAVING PROBLEMS WITH TIRES LEAKING FROM WEEP HOLES AFTER HAVING BEEN RETREADED BY REPAIR STATION NR BX3R4131. WE MARK THE TI - [SDR 98ZZZX1383](https://openairdocs.org/sdr/98ZZZX1383), Mar 24, 1998: ADAPTER. CRACKED. WHILE INVESTIGATING AN OIL LEAK ON THE RT ENGINE, DID A DYE PENETRANT INSPECTION OF THE AIR PUMP ADAPTER, AND FOUND IT CRACKED IN THE AREA OF THE FLANGE THAT MA - [SDR 97ZZZX5167](https://openairdocs.org/sdr/97ZZZX5167), Nov 20, 1997: GEAR. FAILED. INVESTIGATION FOR CAUSE OF FLAP GEAR BOX FAILURE FOUND POOR TEETH ENGAGEMENT OF GEARBOX TEETH AND MOTOR GEAR TEETH. - [SDR 97ZZZX5166](https://openairdocs.org/sdr/97ZZZX5166), Nov 20, 1997: GEAR. FAILED. INVESTIGATION FOR CAUSE OF FLAP GEAR BOX FAILURE FOUND POOR TEETH ENGAGEMENT OF GEARBOX TEETH AND MOTOR GEAR TEETH. - [SDR 97ZZZX4957](https://openairdocs.org/sdr/97ZZZX4957), Nov 7, 1997: DEICE BOOT. FAILED. PROPELLER DEICE LEAD BREAK 12 INCHES FROM TERMINALS AFTER FOLLOWING NEW INSTALLATION INSTRUCTIONS. - [SDR 97ZZZX4839](https://openairdocs.org/sdr/97ZZZX4839), Nov 7, 1997: DEICE BOOT. FAILED. DEICE BOOT LEAD BREAKS 12 INCHES FROM TERMINALS AFTER FOLLOWING NEW INSTALLATION SUGGESTIONS. - [SDR 97ZZZX4840](https://openairdocs.org/sdr/97ZZZX4840), Oct 3, 1997: DEICE BOOT. FAILED. DEICE BOOT LEADS ARE CONTINUING TO BREAK APPROXIMATELY 12 INCHES FROM THE TERMINALS EVEN AFTER RAPCO'S NEW INSTALLATION SUGGESTIONS. - [SDR 97ZZZX4386](https://openairdocs.org/sdr/97ZZZX4386), Sep 5, 1997: PUMP. FAILED. VACUUM PUMP FAILED UNDER NORMAL OPERATING CONDITIONS. SUBMITTER STATED THIS PUMP HAD AN EXCEPTIONALLY LONG SERVICE LIFE. - [SDR 97ZZZX2793](https://openairdocs.org/sdr/97ZZZX2793), May 24, 1997: BREAKER. SMOKED. SMOKE COMING FROM CIRCUIT BREAKER PANEL. LEFT BOOST PUMP DID NOT WORK. PILOT TURNED MASTER OFF. SUBMITTER STATED CYCLE CIRCUIT BREAKER ONCE EACH YEAR. - [SDR CA970128011](https://openairdocs.org/sdr/CA970128011), Jan 22, 1997: CHANNEL. CRACKED. (CAN) CABIN DOOR HINGE HAD EXCESSIVE PLAY. WHILE REPLACING THE RIVETS A CRACK WAS FOUND IN THE STRUCTURE. - [SDR CA961011007](https://openairdocs.org/sdr/CA961011007), Oct 2, 1996: SUPPORT. CRACKED. (CAN) CRACKS EXTENDING UPWARDS FROM BOTTOM EDGE OF OUTBOARD SUPPORT WHERE THEY ATTACH TO LOWER FORWARD SPAR CAP. BOTH LOWER BOLT HOLES AT SPAR CAPS, BOTH SIDES - [SDR EY2R9601005](https://openairdocs.org/sdr/EY2R9601005), Sep 1, 1996: CLAMP. CORRODED. CORROSION FOUND ON CLAMP. - [SDR EY2R9601004](https://openairdocs.org/sdr/EY2R9601004), Sep 1, 1996: CLAMP. CORRODED. CORROSION FOUND ON CLAMP. - [SDR EY2R9601003](https://openairdocs.org/sdr/EY2R9601003), Sep 1, 1996: BEARING. CORRODED. BEARING CORRODED. - [SDR EY2R9601002](https://openairdocs.org/sdr/EY2R9601002), Sep 1, 1996: BEARING. CORRODED. BEARING CORRODED. - [SDR EY2R9601001](https://openairdocs.org/sdr/EY2R9601001), Sep 1, 1996: PILOT TUBE. CORRODED. PILOT TUBE FOUND CORRODED. All 55: https://openairdocs.org/model/beech-65-b80/reports.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.