# Cessna 337H - Type: Aircraft model (FAA registry) - Registry code: 2075732 - Manufacturer (registry): CESSNA - Model: 337H - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Reciprocating - Seats: 6 - Weight class: Up to 12,499 lb - Certification: Type certificated - Data sheet: [TCDS A6CE](https://openairdocs.org/tcds/A6CE) (OpenAirDocs) - Holder: Textron Aviation Inc. - Registered aircraft: 9 - Page: https://openairdocs.org/model/cessna-337h 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 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI). Effective Mar 21, 2022 - [AD 2011-10-09](https://openairdocs.org/ad/2011-10-09): Seat Rails and Roller Housing Inspections · Cessna 150A, 150B, 150C and 221 more. Effective Jun 17, 2011 - [AD 2010-21-18](https://openairdocs.org/ad/2010-21-18): Wings · Wing tip extension fuel tanks (Aviation Enterprises STC SA02055AT or 3 others). Effective Nov 3, 2010 - [AD 2008-26-10](https://openairdocs.org/ad/2008-26-10): Alternate static air source selector valve · Cessna 172, 172A, 172B and 179 more. Effective Jan 5, 2009 - [AD 2004-25-16 R1](https://openairdocs.org/ad/2004-25-16-R1): Fuel regulator shutoff valve · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant), CL-215-6B11 (CL-415 Variant) and 64 more. Effective Jun 20, 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 2004-21-05](https://openairdocs.org/ad/2004-21-05): B-Seires Combustion Heaters · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant), CL-215-6B11 (CL-415 Variant) and 41 more. Effective Nov 19, 2004 - [AD 2000-06-01](https://openairdocs.org/ad/2000-06-01): Fuel Strainer Assembly · Cessna 150F, 150G, 150H and 163 more. Effective May 5, 2000 - [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 97-01-13](https://openairdocs.org/ad/97-01-13): Fuel, Oil and Hydraulic Hoses · Cessna 150, 150A, 150B and 232 more. Effective Feb 3, 1997 - [AD 96-12-22](https://openairdocs.org/ad/96-12-22): Full Flow Engine Oil Adapter · Bellanca CH-300 Pacemaker, 120, 140 and 361 more. Effective Jul 31, 1996 - [AD 79-10-14 R1](https://openairdocs.org/ad/79-10-14-R1): Fuel Tank Venting · Cessna 140A, 150, 150A and 172 more. Effective May 30, 1988 - [AD 78-09-05](https://openairdocs.org/ad/78-09-05): Wing Spar Caps and Web Doublers · Cessna 336, 337, 337A and 16 more. Effective May 11, 1978 - [AD 77-08-05](https://openairdocs.org/ad/77-08-05): Single Engine Takeoffs · Cessna 337, 337A, 337B and 15 more. Effective Apr 28, 1977 - [AD 75-09-05](https://openairdocs.org/ad/75-09-05): Pitot System · Drooped ailerons in flaps down mode, recontoured wing leading… (Sierra Industries STC SA1627WE). Effective Apr 22, 1975 - [AD 72-23-03](https://openairdocs.org/ad/72-23-03): Wing Flap Actuator · Cessna 336, 337, 337A and 7 more. Effective Nov 10, 1972 - [AD 71-17-08](https://openairdocs.org/ad/71-17-08): Rear Engine Stoppage On Take Off · Cessna 337, 337A, 337B and 6 more. Effective Aug 24, 1971 Historical (superseded or no longer in force): - [AD 87-20-03 R2](https://openairdocs.org/ad/87-20-03-R2) (historical): Seat Tracks · Cessna 150A, 150B, 150C and 212 more. Effective Sep 24, 1990 ## Information bulletins (advisory) (14) - [SAIB CE-13-27R1](https://openairdocs.org/saib/CE-13-27R1): Flight Controls Frayed Flap Extend Cables. Issued Jan 5, 2022 - [SAIB AIR-21-16](https://openairdocs.org/saib/AIR-21-16): FLIGHT COMPARTMENT EQUIPMENT, Cessna Seat Back Attachment Bolt Inspection. Issued Aug 26, 2021 - [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018 - [SAIB CE-12-41](https://openairdocs.org/saib/CE-12-41): Flight Controls Loose Glide Screw. Issued Aug 9, 2012 - [SAIB CE-12-24R1](https://openairdocs.org/saib/CE-12-24R1): Flight Controls Frayed Flap Extend Cables. Issued May 21, 2012 - [SAIB CE-12-24](https://openairdocs.org/saib/CE-12-24) (historical): Flight Controls Frayed Flap Extend Cables. Issued Apr 6, 2012 - [SAIB CE-12-14](https://openairdocs.org/saib/CE-12-14): Three Alternative Methods of Compliance for AD 2011-10-09. Issued Jan 25, 2012 - [SAIB CE-10-40R1](https://openairdocs.org/saib/CE-10-40R1): Aircraft Fuel System; water contamination of fuel tank systems on Cessna single engine airplanes. Issued Jul 30, 2010 - [SAIB CE-10-20R1](https://openairdocs.org/saib/CE-10-20R1): Wing Structure; Wingtip Extensions. Issued May 12, 2010 - [SAIB CE-10-20](https://openairdocs.org/saib/CE-10-20) (historical): Wing Structure; Wingtip Extensions. Issued Mar 16, 2010 - [SAIB CE-09-42](https://openairdocs.org/saib/CE-09-42): Lights - Landing Light, Beacon Light and Taxi Light Switch Applications. Issued Jul 24, 2009 - [SAIB CE-09-10](https://openairdocs.org/saib/CE-09-10): Availability of Secondary Seat Stops for Pilot and Copilot Seats. Issued Feb 5, 2009 - [SAIB CE-01-41R2](https://openairdocs.org/saib/CE-01-41R2): Flight Controls. Issued Oct 1, 2007 - [SAIB CE-01-41R1](https://openairdocs.org/saib/CE-01-41R1) (historical): Cracks in plastic or non-metallic control wheels. Issued Jan 10, 2007 ## Registered aircraft (9) - [N1258S](https://openairdocs.org/aircraft/N1258S): [N76bt LLC](https://openairdocs.org/faa-owner/N76BT%20LLC), [Lynnfield, MA](https://openairdocs.org/faa-place/MA/Lynnfield), S/N 33701894 - [N1360L](https://openairdocs.org/aircraft/N1360L): [Koukol Orin Trustee](https://openairdocs.org/faa-owner/KOUKOL%20ORIN%20TRUSTEE), [Sacramento, CA](https://openairdocs.org/faa-place/CA/Sacramento), built 1978, S/N 33701852 - [N1365L](https://openairdocs.org/aircraft/N1365L): [Kropp Christian Trustee](https://openairdocs.org/faa-owner/KROPP%20CHRISTIAN%20TRUSTEE), [Azle, TX](https://openairdocs.org/faa-place/TX/Azle), S/N 33701857 - [N27CT](https://openairdocs.org/aircraft/N27CT): [Clinic-Air Aviation](https://openairdocs.org/faa-owner/CLINIC-AIR%20AVIATION), [Chapmansboro, TN](https://openairdocs.org/faa-place/TN/Chapmansboro), built 1979, S/N 33701888 - [N337DE](https://openairdocs.org/aircraft/N337DE): [Airbermz LLC](https://openairdocs.org/faa-owner/AIRBERMZ%20LLC), [Bloomfield Hills, MI](https://openairdocs.org/faa-place/MI/Bloomfield%20Hills), built 1980, S/N 33701943 - [N738JR](https://openairdocs.org/aircraft/N738JR): [Rutkosky John J DBA](https://openairdocs.org/faa-owner/RUTKOSKY%20JOHN%20J%20DBA), [Palm Coast, FL](https://openairdocs.org/faa-place/FL/Palm%20Coast), S/N 33701878 - [N745AS](https://openairdocs.org/aircraft/N745AS): [A2g International LLC](https://openairdocs.org/faa-owner/A2G%20INTERNATIONAL%20LLC), [San Juan Capo, CA](https://openairdocs.org/faa-place/CA/San%20Juan%20Capo), built 1977, S/N 33701817 - [N746AS](https://openairdocs.org/aircraft/N746AS): [A2g International LLC](https://openairdocs.org/faa-owner/A2G%20INTERNATIONAL%20LLC), [San Juan Capo, CA](https://openairdocs.org/faa-place/CA/San%20Juan%20Capo), built 1978, S/N 33701850 - [N76BT](https://openairdocs.org/aircraft/N76BT): [Estes David Edward](https://openairdocs.org/faa-owner/ESTES%20DAVID%20EDWARD), [Kennesaw, GA](https://openairdocs.org/faa-place/GA/Kennesaw), S/N 33701935 ## STCs approved for it (189, first 50) - [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 SA00079NY](https://openairdocs.org/stc/SA00079NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less.. Airwolf Filter Corporation - [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 (1 OF 3)](https://openairdocs.org/stc/SA00161BO%20(1%20OF%203)): Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.. Avidyne Corporation - [STC SA00243BO (3 OF 5)](https://openairdocs.org/stc/SA00243BO%20(3%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 SA00272WI](https://openairdocs.org/stc/SA00272WI): Replacement of hydraulic system pressure switch.. APPH Wichita 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 SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation - [STC SA00402SE](https://openairdocs.org/stc/SA00402SE): Installation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed). Aviation Development Corporation - [STC SA00432SE](https://openairdocs.org/stc/SA00432SE): Installation of EGT 701 series fuel flow instrument.. J P Instruments - [STC SA00678SE](https://openairdocs.org/stc/SA00678SE): Installation of J. P. Instruments 8Jimline EGT-100 series primary instruments. J P Instruments - [STC SA00680SE (4 OF 6](https://openairdocs.org/stc/SA00680SE%20(4%20OF%206): Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.. Electronics International - [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 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 SA00861SE](https://openairdocs.org/stc/SA00861SE): Installation of J.P. Instruments (JPI) fuel flow indicating system. J P Instruments - [STC SA00897WI](https://openairdocs.org/stc/SA00897WI): Installation of Concorde Battery Corporation (VRSLA) Valve regulated sealed lead acid battery.. Aero-Mach Wilco LLC - [STC SA00944CH](https://openairdocs.org/stc/SA00944CH): Replace Janitrol combustion heater Model 81D94-X (XX) with C&D Associates combustion heater Model CD25K, CD35K, and CD45K. Hartzell Engine Technologies, LLC - [STC SA01085LA](https://openairdocs.org/stc/SA01085LA): Installation of the VNS 1000 Voice Navigation System.. VNS Incorporated - [STC SA01105WI-D (1 OF 2)](https://openairdocs.org/stc/SA01105WI-D%20(1%20OF%202)): Installation of Bendix/King KMD 550/850 Multi-Function Display System with Optional Traffic, Terrain and Weather Sensors. This STC also is approved for some single-engine aircraft. See SA01105WI-D (2 of 2).. Honeywell International Inc. - [STC SA01114CH](https://openairdocs.org/stc/SA01114CH): Installation of P2 Incorporated 6600 Audio Advisory system. P2 Incorporated - [STC SA01118WI](https://openairdocs.org/stc/SA01118WI): Installation of the Concorde FLA or VRSLA RG series batteries. Concorde Battery Corporation - [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 SA01179AT](https://openairdocs.org/stc/SA01179AT): Installation of an external cargo Pod.. RT Aerospace Corp - [STC SA01205WI-D (1 OF 2)](https://openairdocs.org/stc/SA01205WI-D%20(1%20OF%202)): Installation of the KMD 250 Multi-Function Display System with Optional Internal VFR GPS and Optional Traffic and Weather Sensors.. Honeywell International Inc - [STC SA01215SE](https://openairdocs.org/stc/SA01215SE): Installation of vortex generators on the leading edge of the upper side of the wing on the underside of the horizontal stabilizer, and on both vertical stabilizers.. Micro AeroDynamics Inc - [STC SA01229SE PAGE 1](https://openairdocs.org/stc/SA01229SE%20PAGE%201): Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Garmin International Inc - [STC SA01344AT](https://openairdocs.org/stc/SA01344AT): Installation of a baggage door on the aft right side of the fuselage.. RT Aerospace Corp - [STC SA01473SE (2 OF 5)](https://openairdocs.org/stc/SA01473SE%20(2%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-D](https://openairdocs.org/stc/SA01487SE-D): Installation of a GDL 69 or GDL 69A XM Satellite Receiver. Garmin International Inc - [STC SA01560WI-D](https://openairdocs.org/stc/SA01560WI-D): Installation of the Honeywell KFD 840 Primary Flight Display System.. Honeywell International Inc - [STC SA01669CH](https://openairdocs.org/stc/SA01669CH): Installation of Challenger Reusable Air Filter. Challenger Aviation Products 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 (2 OF 5)](https://openairdocs.org/stc/SA01695SE%20(2%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 SA01734SE](https://openairdocs.org/stc/SA01734SE): Application of Stewart Systems synthetic fabric covering system to aircraft fuselage, wings, tail surfaces, control surfaces and related parts.. Andrew D. Humphrey - [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 SA01816WI](https://openairdocs.org/stc/SA01816WI): Installation of an ADS-B compliant system, comprised of a Garmin GTX 330 Mode S Transponder and a Free Flight 1201 GPS receiver.. Trego Dugan Aviation - [STC SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc. - [STC SA01828SE](https://openairdocs.org/stc/SA01828SE): Installation of J.P. Instruments (JPI) EDM-960 Primary Engine Data Management System. J. P. Instruments - [STC SA01834CH (1 OF 2)](https://openairdocs.org/stc/SA01834CH%20(1%20OF%202)): Installation of the High Intensity Discharge Light Assembly Kit.. Knots 2U Ltd. All 189: https://openairdocs.org/model/cessna-337h/stcs.md ## NTSB investigations (7) 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 LAX98LA104](https://openairdocs.org/ntsb/LAX98LA104), Mar 4, 1998: Boeing 737-242C (N746AS), Reno, NV, no damage. Probable cause: Unforecasted and sudden encounter with clear air turbulence when passengers and flight attendants were not secured in their seats. - [NTSB MIA93LA047](https://openairdocs.org/ntsb/MIA93LA047), Jan 9, 1993: Cessna 337H (N1443S), New Smyrna Bch, FL, destroyed, 1 fatal. Probable cause: THE PILOT-IN-COMMAND'S FAILURE TO MAINTAIN ALTITUDE WHILE MANEUVERING IN A TURN AT A LOW ALTITUDE, RESULTING IN AN IN-FLIGHT COLLISION WITH THE OCEAN. - [NTSB FTW81FA044](https://openairdocs.org/ntsb/FTW81FA044), Mar 10, 1981: Cessna 337H (N1361L), Alpine, TX, destroyed, 3 fatal - [NTSB CHI81FA001](https://openairdocs.org/ntsb/CHI81FA001), Oct 14, 1980: Cessna 337H (N1333L), Waterford, MI, destroyed, 3 fatal - [NTSB MIA80DLA36](https://openairdocs.org/ntsb/MIA80DLA36), Aug 29, 1980: Cessna 337 (N1395L), Gainsville, FL, substantial damage - [NTSB DEN78FTE73](https://openairdocs.org/ntsb/DEN78FTE73), Jul 8, 1978: Cessna 337 (N1371L), Longmont, CO, substantial damage - [NTSB OAK74DJY03](https://openairdocs.org/ntsb/OAK74DJY03), Sep 20, 1973: Beech C-45H (N9157Z), Phan Rang, VM, substantial damage ## FAA accident and incident reports (13) 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. - [Incident 20200608007931I](https://openairdocs.org/incident/20200608007931I), Jun 8, 2020: Cessna 337H (N27CT), Nashville, TN, Minor damage. On June 8, 2020 N69MK was parked and tied down on the ramp at John Tune Airport. At approx. 0840 N27CT had landed and taxied in to park on the ramp. As N27CT… - [Incident 20011205037239I](https://openairdocs.org/incident/20011205037239I), Dec 5, 2001: Cessna 337H (N888NH), Olive Branch, MS, Minor damage. (-23) Aircraft landed gear up at olv.[privacy data omitted] - [Incident 20000328022199I](https://openairdocs.org/incident/20000328022199I), Mar 28, 2000: Cessna 337H (N1244S), Springfield, IL. (-23)N1244S, a CE-337, enroute form kpis to kspi in visual meteorological conditions, was being vectored by the Springfield ATC for a landing on runway 31 at… - [Accident 19980304010239A](https://openairdocs.org/incident/19980304010239A), Mar 4, 1998: Boeing 737242C (N746AS), Reno, NV. Encountered cat enroute at FL350. Diverted to rno. Flight attendant broke an ankle. 7 passengers injured. (.4)the flight encountered sever clear air turbulence… - [Incident 19930520019019I](https://openairdocs.org/incident/19930520019019I), May 20, 1993: Cessna 337H (N1372L), Long Beach, CA, Minor damage. Unable to lower landing gear. Landed gear up. Found landing gear door actuator rods were disconnected. - [Accident 19930109000229A](https://openairdocs.org/incident/19930109000229A), Jan 9, 1993: Cessna 337H (N1443S), New Smyrna Beac, FL, Destroyed, 1 fatal. Flying low over water offshore. Made steep banks right and left. Wing hit water. Aircraft disintragated. - [Incident 19810914071419I](https://openairdocs.org/incident/19810914071419I), Sep 14, 1981: Cessna 337H (N1327L), Old Town, ME, Minor damage. Jack pad fell from wing during takeoff, struck and damaged rear propeller. Pilot could not syncronize propellers. - [Incident 19810517034429I](https://openairdocs.org/incident/19810517034429I), May 17, 1981: Cessna 337H (N1351L), San Antonio, TX, Minor damage. Nose gear collapsed during rollout. No malfunction found. - [Accident 19810310008989A](https://openairdocs.org/incident/19810310008989A), Mar 10, 1981: Cessna 337H (N1361L), Alpine, TX, Destroyed, 2 fatal. Impacted mountain during NDB approach. Failed to follow missed approach procedure. Weather below minima. - [Accident 19801014058481A](https://openairdocs.org/incident/19801014058481A), Oct 14, 1980: Cessna 337H (N1333L), Pontiac, MI, Destroyed. Collided with N2555R during descent to airport of destination. Had been advised of opposing outbound traffic. - [Accident 19800829041159A](https://openairdocs.org/incident/19800829041159A), Aug 29, 1980: Cessna 337H (N1395L), Gainesville, FL, Substantial damage. Pilot was attempting short field landing and hit runway too hard, causing substantial damage. - [Accident 19780708020369A](https://openairdocs.org/incident/19780708020369A), Jul 8, 1978: Cessna 337H (N1371L), Longmont, CO, Substantial damage. Battery dead. Engine would't start after intentional shutdown infl--aft engine. - [Accident 19730920042829A](https://openairdocs.org/incident/19730920042829A), Sep 20, 1973: Beech C45H (N9157Z), Phan Rang, Substantial damage. Investigation under jurisdiction of goverment of south vietnam. ## Service difficulty reports (21) As reported by operators and repair stations, by the model named in the report. - [SDR CA130710010](https://openairdocs.org/sdr/CA130710010), Jul 10, 2013: STOP PIN. BACKED OUT. (CAN) THE PILOT REPORTED THAT HIS MIXTURE CONTROLS WHERE A FULL KNOB OUT FROM EACH OTHER AND FUEL FLOWS WHERE OUT FROM EACH OTHER DURING GROUND RUN. INSPECTION - [SDR CA100608014](https://openairdocs.org/sdr/CA100608014), Jun 1, 2010: DRIVE GEAR. WORN. ON INSP OF OIL SCREEN METAL WAS FOUND AND INSP WAS CARRIED OUT AND FOUND THAT THE MAGNETO DRIVE GEAR WAS MISSING SEVERAL TEETH AND THE REST OF THE TEETH WHERE W - [SDR 2009FA0000510](https://openairdocs.org/sdr/2009FA0000510), Jun 9, 2009: AIR FILTER. DEFECTIVE. UPON RECEIVING INSP OF NEW MFG AIR FILTERS PN P107336 IT WAS FOUND THAT 3 OUT OF 4 NEW FILTERS HAD A DEFECTIVE SEALING SURFACE CAUSING THE SEALING/MATING SURFAC - [SDR 2006FA0000863](https://openairdocs.org/sdr/2006FA0000863), Jul 18, 2006: CLAMP. CRACKED. WHILE DOING A PRE-TOW WALKAROUND INSPECTION, NOTICED THE FRONT ENGINE EXHAUST TAIL PIPES WERE LOOSE AND SUPPORT CLAMPS PN 15501261 BROKEN ON BOTH LT AND RT SIDE - [SDR 2004FA0000690](https://openairdocs.org/sdr/2004FA0000690), Jul 1, 2004: POINTS. WORN. PILOT REPORTED REAR ENGINE LT MAGNETO INOPERABLE ON RUN-UP. TROUBLESHOT AND FOUND CONTACT POINTS NOT OPENING FAR ENOUGH. NYLON CAM FOLLOWER FOUND MELTED AT CONT - [SDR 2004FA0000266](https://openairdocs.org/sdr/2004FA0000266), Feb 18, 2004: SAFETY SWITCH. DAMAGED. AFTER TAKE OFF PILOT WAS UNABLE TO RETRACT THE LANDING GEAR, THE GEAR DID SHOW DOWN AND LOCKED. THE PLANE LANDED WITHOUT INCIDENT. FOUND NOSE GEAR SAFETY SWITCH - [SDR AUS20031318](https://openairdocs.org/sdr/AUS20031318), Nov 28, 2003: CONTROL CABLE. FRAYED. (AUS) IB FLAP CABLE CONTAINED BROKEN WIRES LOCATED AT TIGHT BEND AROUND THE BELLCRANK. APPROXIMATELY 50 PERCENT OF THE WIRES WERE BROKEN. INSPECTION CARRIED OUT - [SDR 2002FA0000005](https://openairdocs.org/sdr/2002FA0000005), Dec 20, 2001: ARM. WORN. DURING ANNUAL INSPECTION FOUND MIXTURE ARM ROD END ATTACHING BOLT LOOSE. ATTEMPTED TO TIGHTEN BOLT BUT FOUND THERE WAS STILL PLAY. DISASSEMBLED ROD END ATTACHIN - [SDR 20010529CW007](https://openairdocs.org/sdr/20010529CW007), Apr 23, 2001: GEAR. WORN. A DETAINLED INVESTIGATION OF THE STARTER DRIVE REVEALED THAT ALL OF THE GEAR TEETH WERE WORN EXCESSIVELY ON ONE OF THE BEVEL GEARS WHICH DRIVES THE VACUUM PUMP. - [SDR CA001228030](https://openairdocs.org/sdr/CA001228030), Nov 15, 2000: FUEL TANK. CRACKED. (CAN) WHILE BEING STORED IN A HANGAR RIGHT WING WAS DISCOVERED TO BE LEAKING FUEL. UPON FURTHER INSPECTION NR3 FUEL TANK P/N 1516132-16 HAD A CRACK ON TOP NEAR - [SDR CA001211005](https://openairdocs.org/sdr/CA001211005), Oct 20, 2000: BRACKET. CRACKED. (CAN) DISCOVERED DURING A 100 HOUR INSPECTION. THE TOP OF THE BRACKET WHERE THE SHIMMY DAMPER ATTACHES WAS FOUND CRACKED. - [SDR CA001211004](https://openairdocs.org/sdr/CA001211004), Oct 20, 2000: CAM. CRACKED. (CAN) DISCOVERED DURING A 100-HOUR INSPECTION. THE SHIMMY DAMPER ATTACH BRACKET WAS FOUND CRACKED. DUE TO THIS, THE LANDING GEAR (NOSE) WAS REMOVED AND THE STEE - [SDR 20000504SH014](https://openairdocs.org/sdr/20000504SH014), Mar 28, 2000: CIRCUIT BREAKER. FAILED. THE CIRCUIT BREAKER FAILED TO THE OPEN POSITION PREVENTING A NORMAL EXTENSION OF THE AIRCRAFT LANDING GEAR. (X) - [SDR CA000713003](https://openairdocs.org/sdr/CA000713003), Mar 3, 2000: CLEVIS PIN. SHEARED. (CAN) ON INSPECTION OF LANDING GEAR DOWNLOCK ACTUATOR THE RT CLEVIS PIN HALF WAS MISSING. THE CLEVIS PIN WAS REMOVED AND FOUND TO BE SHEARED. A NEW PIN WAS INST - [SDR 98ZZZX874](https://openairdocs.org/sdr/98ZZZX874), Feb 5, 1998: PUMP. FAILED. FOLLOWING TAKEOFF, AIRSPEED SLOWED. REAR ENGINE INSTRUMENTS INDICATED ENGINE WAS LOSING POWER. OIL PRESSURE WAS DROPPING AND THE PROPELLER WENT INTO FEATHER. TH - [SDR CA970610001](https://openairdocs.org/sdr/CA970610001), Jun 2, 1997: OIL PUMP. DRIVE SHEARED. (CAN) PROPELLER FEATHERED AND ENGINE SHUTDOWN IN FLIGHT. AIRCRAFT RETURNED TO BASE. POST FLIGHT INSPECTION FOUND THE OIL PUMP DRIVE GEAR SHEARED. - [SDR EY2R9600923](https://openairdocs.org/sdr/EY2R9600923), Aug 1, 1996: DOWEL. CORRODED. DOWEL CORRODED. - [SDR EY2R9600922](https://openairdocs.org/sdr/EY2R9600922), Aug 1, 1996: CYLINDER PIN. CORRODED. CORROSION FOUND CYLINDER PIN. - [SDR EY2R9600921](https://openairdocs.org/sdr/EY2R9600921), Aug 1, 1996: DOWEL. CORRODED. DOWEL CORRODED. - [SDR EY2R9600920](https://openairdocs.org/sdr/EY2R9600920), Aug 1, 1996: CYLINDER PIN. CORRODED. CYLINDER PIN CORRODED. - [SDR 96ZZZX2501](https://openairdocs.org/sdr/96ZZZX2501), Mar 6, 1996: HUB. BROKEN. THIS FAILURE OCCURRED DESPITE C/W TCM SB 95-3. THE BUSHING AND RETAINER WERE SHOWING WEAR, HOWEVER, NOT NEAR FAILURE. SUSPECT THIS FAILURE IS A BY-PRODUCT OF TH --- 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.