# Cessna T337E

- Type: Aircraft model (FAA registry)
- Registry code: 2075723
- Manufacturer (registry): CESSNA
- Model: T337E
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Reciprocating
- Seats: 6
- Weight class: Up to 12,499 lb
- Cruise speed: 142 mph
- Certification: Type certificated
- Data sheet: [TCDS A6CE](https://openairdocs.org/tcds/A6CE) (OpenAirDocs)
- Holder: Textron Aviation Inc.
- Registered aircraft: 6
- Page: https://openairdocs.org/model/cessna-t337e

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 2023-09-09](https://openairdocs.org/ad/2023-09-09): Exhaust Turbine System (Recip) · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 292 more. Effective Jul 17, 2023
- [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 2011-15-11](https://openairdocs.org/ad/2011-15-11): Wings · Nineteen and a half(19.5 U.S.) gallons wing tip fuel tank (Flint Aero STC SA5090NM). Effective Sep 6, 2011
- [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 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 2004-19-01](https://openairdocs.org/ad/2004-19-01): Upper shoulder harness adjusters · Cessna F150G, F150H, F150J and 129 more. Effective Nov 1, 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 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 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 78-20-12](https://openairdocs.org/ad/78-20-12): Aircraft Tires · Cessna 336, 337, T337B and 15 more. Effective Oct 5, 1978
- [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 76-04-03](https://openairdocs.org/ad/76-04-03): ARC PA-500A Actuators · Cessna 172L, 172M, 177B and 43 more. Effective Feb 26, 1976

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
- [AD 86-26-04](https://openairdocs.org/ad/86-26-04) (historical): Shoulder Harness Adjuster · Cessna Aircraft Company, The 120, 140, 140A and 134 more. Effective Jan 6, 1987

## Information bulletins (advisory) (6)

- [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-12-14](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-09-10](https://openairdocs.org/saib/CE-09-10): Availability of Secondary Seat Stops for Pilot and Copilot Seats. Issued Feb 5, 2009

## Registered aircraft (6)

- [N19EZ](https://openairdocs.org/aircraft/N19EZ): [Air Mobile Ministries](https://openairdocs.org/faa-owner/AIR%20MOBILE%20MINISTRIES), [Sneedville, TN](https://openairdocs.org/faa-place/TN/Sneedville), built 1970, S/N 33701315
- [N337BT](https://openairdocs.org/aircraft/N337BT): [Krall Jeff](https://openairdocs.org/faa-owner/KRALL%20JEFF), [Mitchell, SD](https://openairdocs.org/faa-place/SD/Mitchell), built 1969, S/N 33701223
- [N5LQ](https://openairdocs.org/aircraft/N5LQ): [Collignon William A Jr](https://openairdocs.org/faa-owner/COLLIGNON%20WILLIAM%20A%20JR), [Muscle Shoals, AL](https://openairdocs.org/faa-place/AL/Muscle%20Shoals), built 1969, S/N 33701202
- [N86452](https://openairdocs.org/aircraft/N86452): [Lazy Ta Legend Aircraft LLC](https://openairdocs.org/faa-owner/LAZY%20TA%20LEGEND%20AIRCRAFT%20LLC), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), S/N 33701199
- [N86539](https://openairdocs.org/aircraft/N86539): [Skymaster Stc LLC](https://openairdocs.org/faa-owner/SKYMASTER%20STC%20LLC), [Mena, AR](https://openairdocs.org/faa-place/AR/Mena), built 1969, S/N 33701229
- [N919B](https://openairdocs.org/aircraft/N919B): [Guastadisegni Joseph A Trustee](https://openairdocs.org/faa-owner/GUASTADISEGNI%20JOSEPH%20A%20TRUSTEE), [Oak Hills, CA](https://openairdocs.org/faa-place/CA/Oak%20Hills), built 1970, S/N 33701307

## STCs approved for it (196, 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 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 SA00556AT](https://openairdocs.org/stc/SA00556AT): Installation of Appalachian Accessories carbon steel brake discs, P/N AA-27A.. Aviation Products, Inc
- [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 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 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 (2 OF 5)](https://openairdocs.org/stc/SA01487SE%20(2%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 SA01560WI-D](https://openairdocs.org/stc/SA01560WI-D): Installation of the Honeywell KFD 840 Primary Flight Display System.. Honeywell 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 (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.
- [STC SA01835WI](https://openairdocs.org/stc/SA01835WI): Installation of Trig Avionics TY-96 or TY-97 VHF Communications Radio. Peregrine
- [STC SA01838WI](https://openairdocs.org/stc/SA01838WI): Installation of a FreeFlight 1201 GPS receiver, with an Avidyne AXP340 Transponder, for ADS-B Out. Trego Dugan Aviation

All 196: https://openairdocs.org/model/cessna-t337e/stcs.md

## NTSB investigations (8)

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 SEA05LA068](https://openairdocs.org/ntsb/SEA05LA068), Mar 29, 2005: Cessna T337E (N1711M), Orcas Island, WA, substantial damage, 1 fatal. Probable cause: The loss of power for undetermined reasons which resulted in a forced landing and impact with water.
- [NTSB NYC00LA227](https://openairdocs.org/ntsb/NYC00LA227), Aug 14, 2000: Cessna T337E (N86485), Columbus, OH, substantial damage. Probable cause: The pilot's failure to maintain airspeed, resulting from his improper go-around procedures following a rear engine failure. A factor was the pilot's improper fuel management, which resulted in the…
- [NTSB SEA98LA162](https://openairdocs.org/ntsb/SEA98LA162), Aug 13, 1998: Cessna T337E (N78SC), Hillsboro, OR, substantial damage. Probable cause: The disengagement of the pilot seat forward and aft movement locking pin, followed by the pilot's seat sliding to the rear of the seat track.
- [NTSB SEA94LA012](https://openairdocs.org/ntsb/SEA94LA012), Oct 10, 1993: Cessna T-337E (N1244M), Yamhill, OR, substantial damage. Probable cause: THE PILOT FAILED TO ATTAIN THE PROPER TOUCHDOWN POINT. THE TAILWIND WAS A FACTOR.
- [NTSB LAX84FUJ03](https://openairdocs.org/ntsb/LAX84FUJ03), Sep 1, 1984: Cessna T337E (N1280M), Chandler, AZ, substantial damage
- [NTSB DEN78FQD19](https://openairdocs.org/ntsb/DEN78FQD19), Apr 13, 1978: Cessna T337E (N86505), Deming, NM, substantial damage
- [NTSB DEN78FTE07](https://openairdocs.org/ntsb/DEN78FTE07), Oct 30, 1977: Cessna T337E (N1289M), Peyton, CO, substantial damage
- [NTSB MKC74FER42](https://openairdocs.org/ntsb/MKC74FER42), Feb 26, 1974: Robertson T337E (N1711M), St Paul, MN, substantial damage

## FAA accident and incident reports (15)

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 20240708008329I](https://openairdocs.org/incident/20240708008329I), Jul 8, 2024: Cessna T337E (N19EZ), Titusville, FL, Minor damage. Pilot was landing and forgot to extend the landing gears.
- [Incident 20160610008879I](https://openairdocs.org/incident/20160610008879I), Jun 10, 2016: Cessna T337E (N27LK), Pullman, WA, Minor damage. The aircraft was being utilized for flight training. During the landing phase the gear handle was moved to the gear down position. Once it was realized that…
- [Accident 20050329005359A](https://openairdocs.org/incident/20050329005359A), Mar 29, 2005: Cessna T337E (N1711M), Orcas Island, WA, Destroyed, 1 fatal. (-23) Two minutes after departing the blakely Island airport enroute to the bellingham airport both engines quit. The aircraft ditched near pt. Lawrence, on…
- [Incident 20040626019019I](https://openairdocs.org/incident/20040626019019I), Jun 26, 2004: Cessna T337E (N1711M), Blakely Island, WA, Minor damage. (-23) Pilot forgot to put landing gear down.
- [Accident 20000814043179A](https://openairdocs.org/incident/20000814043179A), Aug 14, 2000: Cessna T337E (N86485), Columbus, OH, Substantial damage. (-23) Aircraft N86485 approached Bolton airport with aft engine shut down and feathered. An attempted landing was initiated with a decision to go around after…
- [Accident 19980813020699A](https://openairdocs.org/incident/19980813020699A), Aug 13, 1998: Cessna T337E (N78SC), Portland, OR, Substantial damage. Acft bounced on landing, lost control, and veered off the rwy. (-23)pilot stated that he had made a number of touch and go's. on the last touch and go, he…
- [Incident 19980712025829I](https://openairdocs.org/incident/19980712025829I), Jul 12, 1998: Cessna T337E (N1247M), Ontario, CA. Cessna 337, N1247M reportedly lost power on both engines and diverted to Ontario International Airport, Ontario, CA. Aircraft landed safely. Aircraft engines…
- [Accident 19931009052619A](https://openairdocs.org/incident/19931009052619A), Oct 9, 1993: Cessna T337E (N1244M), Yamhill, OR, Substantial damage. Landed long on short strip. Overran end into a fence. Had quartering tail wind. One way strip and misjudgement.
- [Incident 19850610065179I](https://openairdocs.org/incident/19850610065179I), Jun 10, 1985: Cessna T337 (N1247M), Fullerton, CA. Front engine quit after takeoff. Fuel vaporization due to unknown cause. Off airport landing without damage.
- [Accident 19840901045229A](https://openairdocs.org/incident/19840901045229A), Sep 1, 1984: Cessna T337E (N1280M), Chandler, AZ, Substantial damage. Over gross and hot day, briefly retarted rear engine due to overboost. Unabel to climb , ran off end, hit ditch.
- [Incident 19811127086319I](https://openairdocs.org/incident/19811127086319I), Nov 27, 1981: Cessna T337E (N1280M), Phoenix, AZ, Minor damage. Failed to extend gear for landing. Landed gear up.
- [Incident 19791218046369I](https://openairdocs.org/incident/19791218046369I), Dec 18, 1979: Cessna T337E (N1711M), Rochester, NY. In cruise, number 1 engine oil pressure lost. Feathered number 1, landed safely. Oil pump had failed.
- [Accident 19780413008809A](https://openairdocs.org/incident/19780413008809A), Apr 13, 1978: Cessna 337G (N86505), Deming, NM, Substantial damage. L main fuel tank full,l aux empty,r aux EST 5GAL,r main undet amtsel on l aux,rear on r aux.
- [Accident 19771030040309A](https://openairdocs.org/incident/19771030040309A), Oct 30, 1977: Cessna T337E (N1289M), Peyton, CO, Substantial damage. Fuel selector valve for rear engine jammed. Landing gear reservoir not properly serviced.d.a.9000FT
- [Accident 19740226004139A](https://openairdocs.org/incident/19740226004139A), Feb 26, 1974: Cessna T337E (N1711M), St Paul, MN, Substantial damage. Auto plt acdtly engaged prior to tkof. Demonstrating stol characteristics of acft mod.

## Service difficulty reports (2)

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

- [SDR CA090126008](https://openairdocs.org/sdr/CA090126008), Dec 16, 2008: SUMP. CORRODED. DURING A ANNUAL INSPECTION, FOUND THE RT WING SUMP TO HAVE CORROSION PIN HOLES IN BOTTOM, REMOVED, REPAIRED AND REINSTALLED SUMP.
- [SDR CA090126007](https://openairdocs.org/sdr/CA090126007), Dec 16, 2008: HEADER TANK. CRACKED. DURING A ANNUAL INSPECTION, FOUND CRACKS AND CORROSION HOLE IN HEADER AND AUXILIARY FUEL TANK, PARTS WERE REMOVED, REPAIRED AND REINSTALLED.

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