# Cessna T207 - Type: Aircraft model (FAA registry) - Registry code: 2073612 - Manufacturer (registry): CESSNA - Model: T207 - Aircraft type: Fixed wing single engine - Category: Airplane - Engines: 1 · Reciprocating - Seats: 6 - Weight class: Up to 12,499 lb - Cruise speed: 67 mph - Certification: Type certificated - Data sheet: [TCDS A16CE](https://openairdocs.org/tcds/A16CE) (OpenAirDocs) - Holder: Textron Aviation Inc. - Registered aircraft: 21 - Page: https://openairdocs.org/model/cessna-t207 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 2020-18-01](https://openairdocs.org/ad/2020-18-01): Fuselage · Textron 172N, 172P, 172Q and 62 more. Effective Nov 12, 2020 - [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 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 2006-03-08](https://openairdocs.org/ad/2006-03-08): Vacuum pumps · Aero Advantage 14-19, 14-19-2, 14-19-3 and 299 more. Effective Mar 10, 2006 - [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 2002-07-01](https://openairdocs.org/ad/2002-07-01): Horizontal Stabilizer Attachment Reinforcement Brackets · Cessna 207, 207A, 210G and 32 more. Effective May 13, 2002 - [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 88-22-07](https://openairdocs.org/ad/88-22-07): Hose Assemblies · Cessna P210N, P210R, T207 and 22 more. Effective Nov 24, 1988 - [AD 84-10-01 R1](https://openairdocs.org/ad/84-10-01-R1): Bladder Fuel Cells · Cessna 180, 180A, 180B and 103 more. Effective Jul 5, 1988 - [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 86-24-07](https://openairdocs.org/ad/86-24-07): Engine Controls Installation · Cessna 150C, 150D, 150E and 142 more. Effective Jan 7, 1987 - [AD 71-09-07 R1](https://openairdocs.org/ad/71-09-07-R1): Exhaust Gases Entering Cabin · Cessna T207, T207A, T210F and 19 more. Effective Nov 26, 1986 - [AD 86-19-11](https://openairdocs.org/ad/86-19-11): Contaminated Fuel · Cessna 177, 177A, 177B and 83 more. Effective Oct 4, 1986 - [AD 85-17-07](https://openairdocs.org/ad/85-17-07): Wing Rear Spar · Cessna 207, 207A, T207 and 5 more. Effective Sep 30, 1985 - [AD 85-03-01](https://openairdocs.org/ad/85-03-01): Throttle and Mixture Controls · Cessna 206, 207, 210-5 (205) and 31 more. Effective Mar 15, 1985 - [AD 85-02-07](https://openairdocs.org/ad/85-02-07): Fuel Selector · Cessna 206, 207, 207A and 45 more. Effective Mar 6, 1985 - [AD 72-03-03 R3](https://openairdocs.org/ad/72-03-03-R3): Wing Flap Actuators Jack Screw · Cessna F150F, F150G, F150H and 83 more. Effective Oct 15, 1984 - [AD 80-07-01](https://openairdocs.org/ad/80-07-01): Oil Pressure · Cessna T207, T207A, T210F and 20 more. Effective Mar 28, 1980 - [AD 79-25-07](https://openairdocs.org/ad/79-25-07): Alternator Ground · Cessna 180, 180A, 180B and 95 more. Effective Dec 13, 1979 - [AD 79-15-01](https://openairdocs.org/ad/79-15-01): Fuel Flow Distribution · Cessna 206, 206H, 207 and 57 more. Effective Jul 26, 1979 - [AD 78-07-01](https://openairdocs.org/ad/78-07-01): Engine Oil Pump · Cessna T207, T207A, T210F and 20 more. Effective Apr 6, 1978 - [AD 77-16-05](https://openairdocs.org/ad/77-16-05): Fuel Selector Valve · Cessna 206, 206H, 207 and 55 more. Effective Aug 11, 1977 - [AD 77-12-08](https://openairdocs.org/ad/77-12-08): External Electrical Ground Power Receptacle · Cessna 172M, 172N, 177B and 19 more. Effective Jun 27, 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 - [AD 75-16-01](https://openairdocs.org/ad/75-16-01): Wing Fuel Tanks · Cessna 180, 180A, 180B and 68 more. Effective Jul 30, 1975 - [AD 72-07-09](https://openairdocs.org/ad/72-07-09): Cracks And Loose Bolts In Fin & Rudder · Cessna 182, 182A, 182B and 74 more. Effective Oct 17, 1974 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 (21) - [N1754U](https://openairdocs.org/aircraft/N1754U): [Sutton Aircraft Salvage LLC](https://openairdocs.org/faa-owner/SUTTON%20AIRCRAFT%20SALVAGE%20LLC), [Palmer, AK](https://openairdocs.org/faa-place/AK/Palmer), built 1976, S/N 20700354 - [N1758U](https://openairdocs.org/aircraft/N1758U): [Bas Part Sales LLC](https://openairdocs.org/faa-owner/BAS%20PART%20SALES%20LLC), [Greeley, CO](https://openairdocs.org/faa-place/CO/Greeley), built 1976, S/N 20700358 - [N207DG](https://openairdocs.org/aircraft/N207DG): [Rwr Air Inc](https://openairdocs.org/faa-owner/RWR%20AIR%20INC), [Tok, AK](https://openairdocs.org/faa-place/AK/Tok), built 1969, S/N 207-00070 - [N207PA](https://openairdocs.org/aircraft/N207PA): [Mcnutt Ross T](https://openairdocs.org/faa-owner/MCNUTT%20ROSS%20T), [Xenia, OH](https://openairdocs.org/faa-place/OH/Xenia), built 1970, S/N 20700162 - [N211AS](https://openairdocs.org/aircraft/N211AS): [Bas Part Sales LLC](https://openairdocs.org/faa-owner/BAS%20PART%20SALES%20LLC), [Greeley, CO](https://openairdocs.org/faa-place/CO/Greeley), built 1974, S/N 20700259 - [N21RG](https://openairdocs.org/aircraft/N21RG): [Macair Aviation LLC](https://openairdocs.org/faa-owner/MACAIR%20AVIATION%20LLC), [Xenia, OH](https://openairdocs.org/faa-place/OH/Xenia), built 1969, S/N 20700066 - [N26CF](https://openairdocs.org/aircraft/N26CF): [Kustatan Leasing LLC](https://openairdocs.org/faa-owner/KUSTATAN%20LEASING%20LLC), [Nikiski, AK](https://openairdocs.org/faa-place/AK/Nikiski), built 1975, S/N 20700306 - [N305PY](https://openairdocs.org/aircraft/N305PY): [Ufly Vi LLC](https://openairdocs.org/faa-owner/UFLY%20VI%20LLC), [St Thomas, VI](https://openairdocs.org/faa-place/VI/St%20Thomas), S/N 207-00156 - [N345AL](https://openairdocs.org/aircraft/N345AL): [Itm Aircraft LLC](https://openairdocs.org/faa-owner/ITM%20AIRCRAFT%20LLC), [Charleston, SC](https://openairdocs.org/faa-place/SC/Charleston), built 1974, S/N 20700262 - [N377CF](https://openairdocs.org/aircraft/N377CF): [Cohen Rolando S](https://openairdocs.org/faa-owner/COHEN%20ROLANDO%20S), [New York, NY](https://openairdocs.org/faa-place/NY/New%20York), built 1974, S/N 20700275 - [N424AD](https://openairdocs.org/aircraft/N424AD): [Sky West Aviation Inc Trustee](https://openairdocs.org/faa-owner/SKY%20WEST%20AVIATION%20INC%20TRUSTEE), [Albuquerque, NM](https://openairdocs.org/faa-place/NM/Albuquerque), S/N 20700337 - [N456BW](https://openairdocs.org/aircraft/N456BW): [Custom Wholesale Supply Co Inc](https://openairdocs.org/faa-owner/CUSTOM%20WHOLESALE%20SUPPLY%20CO%20INC), [Odessa, TX](https://openairdocs.org/faa-place/TX/Odessa), built 1975, S/N 20700298 - [N684S](https://openairdocs.org/aircraft/N684S): [Second Wind Aviation Corp](https://openairdocs.org/faa-owner/SECOND%20WIND%20AVIATION%20CORP), [Friday Harbor, WA](https://openairdocs.org/faa-place/WA/Friday%20Harbor), built 1969, S/N 20700147 - [N745KP](https://openairdocs.org/aircraft/N745KP): [Paklook Air Inc Dbi](https://openairdocs.org/faa-owner/PAKLOOK%20AIR%20INC%20DBI), [Bethel, AK](https://openairdocs.org/faa-place/AK/Bethel), built 1974, S/N 20700238 - [N77CK](https://openairdocs.org/aircraft/N77CK): [Raiz Coaching LLC](https://openairdocs.org/faa-owner/RAIZ%20COACHING%20LLC), [Fort Worth, TX](https://openairdocs.org/faa-place/TX/Fort%20Worth), built 1976, S/N 20700343 - [N90193](https://openairdocs.org/aircraft/N90193): [Renfro Michael W](https://openairdocs.org/faa-owner/RENFRO%20MICHAEL%20W), [Bethel, AK](https://openairdocs.org/faa-place/AK/Bethel), built 1969, S/N 20700007 - [N91016](https://openairdocs.org/aircraft/N91016): [Gosselin Edward M Trustee](https://openairdocs.org/faa-owner/GOSSELIN%20EDWARD%20M%20TRUSTEE), [Bridgewater, NJ](https://openairdocs.org/faa-place/NJ/Bridgewater), built 1969, S/N 20700011 - [N91025](https://openairdocs.org/aircraft/N91025): [Arctic Aviation Leasing LLC](https://openairdocs.org/faa-owner/ARCTIC%20AVIATION%20LEASING%20LLC), [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage), built 1969, S/N 20700016 - [N91060](https://openairdocs.org/aircraft/N91060): [Second Wind Aviation Corp](https://openairdocs.org/faa-owner/SECOND%20WIND%20AVIATION%20CORP), [Friday Harbor, WA](https://openairdocs.org/faa-place/WA/Friday%20Harbor), S/N 20700047 - [N91183](https://openairdocs.org/aircraft/N91183): [Hatch Hyrum G](https://openairdocs.org/faa-owner/HATCH%20HYRUM%20G), [Gilbert, AZ](https://openairdocs.org/faa-place/AZ/Gilbert), built 1969, S/N 20700106 - [N9490Y](https://openairdocs.org/aircraft/N9490Y): [Kearins John M](https://openairdocs.org/faa-owner/KEARINS%20JOHN%20M), [North Hampton, NH](https://openairdocs.org/faa-place/NH/North%20Hampton), built 1969, S/N 20700110 ## STCs approved for it (270, 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 SA00123DE](https://openairdocs.org/stc/SA00123DE): Installation of Oilamatic preoiler system.. Oilamatic 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 (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 SA00162SE](https://openairdocs.org/stc/SA00162SE): Installation of telemetry antennas.. US Dept of Interior - [STC SA00173AT](https://openairdocs.org/stc/SA00173AT): Installation of a Teledyne Continental model IO-550F engine and various Hartzell and McCauley propellers.. Davis Aviation Services Inc - [STC SA00243BO (2 OF 5)](https://openairdocs.org/stc/SA00243BO%20(2%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 SA00353BO](https://openairdocs.org/stc/SA00353BO): Installation of an auto lean system. Flight Enhancements LLC - [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation - [STC SA00406WI](https://openairdocs.org/stc/SA00406WI): Installation of replacement flap trailing edge bulbs with AOG Drawing. Athena Aircraft, LLC - [STC SA00425DE](https://openairdocs.org/stc/SA00425DE): Installation of model FB-02 'Fixed Arm' Pilot Arm Rest on R/H side of pilot seat and optional GPS Support Arm System.. Quality Aircraft Components LC - [STC SA00426DE](https://openairdocs.org/stc/SA00426DE): Installation of Model FB-01 "Swing Arm" Pilot Arm Rest System on R/H side of pilot seat.. Quality Aircraft Components LC - [STC SA00432SE](https://openairdocs.org/stc/SA00432SE): Installation of EGT 701 series fuel flow instrument.. J P Instruments - [STC SA00648SE](https://openairdocs.org/stc/SA00648SE): Fabrication of R.M.D. Aircraft Lighting, Inc., wing-tip and landing light Kit No. 00190-C.. Knots 2U Ltd. - [STC SA00678SE](https://openairdocs.org/stc/SA00678SE): Installation of J. P. Instruments 8Jimline EGT-100 series primary instruments. J P Instruments - [STC SA00680SE (3 OF 6](https://openairdocs.org/stc/SA00680SE%20(3%20OF%206): Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.. Electronics International - [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 SA00709LA](https://openairdocs.org/stc/SA00709LA): Installation of control wheel. Includes provisions only for a push-to-talk (PTT) switch. Separate FAA approval of PTT switch is required.. Trevor Burward-Hoy - [STC SA00709SE](https://openairdocs.org/stc/SA00709SE): Installation of replacement control surface skin panels.. Athena Aircraft, LLC - [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 SA00871SE](https://openairdocs.org/stc/SA00871SE): Installation of cockpit sunvisors. Rosen Sunvisor Systems LLC - [STC SA00887SE](https://openairdocs.org/stc/SA00887SE): Installation of vortex generators on the wings, tail surfaces, and vertical fin, in accordance with Micro AeroDynamics Drawing Package MA2146, Revision A, dated March 11, 2004, and installed in accordance with Installation Manual MA2147, Revision IR, dated January 25, 2001 (for the 206 series) or MA2196, Revision IR, dated March 11, 2004 (for the 207 series), or later FAA approved revisions.. Micro AeroDynamics Inc - [STC SA00897WI](https://openairdocs.org/stc/SA00897WI): Installation of Concorde Battery Corporation (VRSLA) Valve regulated sealed lead acid battery.. Aero-Mach Wilco LLC - [STC SA00954SE (1 OF 2)](https://openairdocs.org/stc/SA00954SE%20(1%20OF%202)): Installation of J.P. Instruments (JPI) Primary Temperature Indicating System in accordance with JPI Installation Manual for the EDM 711, Report 106P, Revision B, dated August 2, 2001, or later FAA approved revision.. J P Instruments - [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 SA01107SE](https://openairdocs.org/stc/SA01107SE): RMD Aircraft Lighting high intensity discharge wingtip light. Knots 2U Ltd. - [STC SA01118WI](https://openairdocs.org/stc/SA01118WI): Installation of the Concorde FLA or VRSLA RG series batteries. Concorde Battery Corporation - [STC SA01120SE](https://openairdocs.org/stc/SA01120SE): Installation of Door Steward.. Mountain View Aviation LLC - [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 SA01206SE](https://openairdocs.org/stc/SA01206SE): Fabrication of Robair middle gear leg fairing assembly. Robair Repair - [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 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 SA01283WI](https://openairdocs.org/stc/SA01283WI): Installation of McCauley D3A34C401/90DFA-6, -8, and -10 Propeller on Cessna Model 207 Series airplanes equipped with TCM IO-520F, IO-550F, TSIO-520-G and TSIO-520-M engines.. P Ponk Aviation - [STC SA01328LA](https://openairdocs.org/stc/SA01328LA): Modification of right hand side door to provide an openable window.. Ellis & Associates CADD/Technical Illustrations - [STC SA01380CH](https://openairdocs.org/stc/SA01380CH): Installation of wing fuel tank quick valve drains.. Storehouse LLC All 270: https://openairdocs.org/model/cessna-t207/stcs.md ## NTSB investigations (33) 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 ANC25FA035](https://openairdocs.org/ntsb/ANC25FA035), Apr 28, 2025: Cessna T207 (N91025), Nanwalek, AK, substantial damage, 2 fatal, investigation ongoing - [NTSB ANC24FA094](https://openairdocs.org/ntsb/ANC24FA094), Sep 16, 2024: Cessna 207 (N90193), Saint Mary's, AK, destroyed, 4 fatal, investigation ongoing - [NTSB WPR22LA092](https://openairdocs.org/ntsb/WPR22LA092), Feb 7, 2022: Cessna T207 (N684S), Crane Island, WA, substantial damage. Probable cause: The pilot’s failure to obtain a proper touch down location on a wet grass runway, resulting in a runway overrun and impact with terrain. - [NTSB ANC17LA043](https://openairdocs.org/ntsb/ANC17LA043), Aug 14, 2017: Cessna T207 (N745KP), Juneau, AK, substantial damage. Probable cause: The total loss of engine power due to fuel starvation. - [NTSB GAA16CA445](https://openairdocs.org/ntsb/GAA16CA445), Aug 23, 2016: Cessna T207 (N91025), Nanwalek, AK, substantial damage. Probable cause: The pilot’s unstabilized approach and a subsequent runway overrun while landing on a short runway in variable wind conditions. - [NTSB CEN14LA327](https://openairdocs.org/ntsb/CEN14LA327), Jun 27, 2014: Cessna T207 (N207AB), Indianapolis, IN, substantial damage. Probable cause: A loss of engine power due to fuel starvation, which resulted from the pilot's failure to monitor the fuel level and switch tanks in a timely fashion. - [NTSB CEN13LA539](https://openairdocs.org/ntsb/CEN13LA539), Sep 4, 2013: Cessna T207 (N211AS), Colorado Springs, CO, substantial damage. Probable cause: The pilot’s failure to establish the proper pitch attitude and airspeed during takeoff with the engine at maximum power, which resulted in the exceedance of the airplane’s climb performance… - [NTSB ANC08CA120](https://openairdocs.org/ntsb/ANC08CA120), Sep 9, 2008: Cessna T207 (N1754U), Nyac, AK, substantial damage. Probable cause: The pilot's selection of unsuitable terrain for landing, which resulted in the nose wheel separating from the airplane during the landing roll. - [NTSB ANC05FA090](https://openairdocs.org/ntsb/ANC05FA090), Jul 1, 2005: Cessna T207 (N1621U), Nanwalek, AK, destroyed, 3 fatal. Probable cause: The pilot's continued VFR flight into instrument meteorological conditions, which resulted in an in-flight collision with an island cliff during cruise flight. A factor contributing to the accident… - [NTSB FTW03LA070](https://openairdocs.org/ntsb/FTW03LA070), Dec 30, 2002: Cessna T207 (N1599U), Brownsville, TX, substantial damage. Probable cause: The loss of engine power due to the separation of the crankshaft. A factor was the lack of suitable terrain for the forced landing. - [NTSB ANC02LA128](https://openairdocs.org/ntsb/ANC02LA128), Sep 15, 2002: Cessna 207 (N207DG), Circle, AK, substantial damage. Probable cause: The pilot's inadequate wind evaluation during takeoff resulting in a downwind takeoff and subsequent overrun during an aborted takeoff. Factors in the accident were a tailwind and the pilot's failure… - [NTSB ANC98LA149](https://openairdocs.org/ntsb/ANC98LA149), Sep 13, 1998: Cessna 207 (N1754U), Sleetmute, AK, substantial damage. Probable cause: The pilot's selection of unsuitable terrain for departure. A factor in the accident was a narrow runway. - [NTSB ANC98FA019](https://openairdocs.org/ntsb/ANC98FA019), Feb 6, 1998: Cessna 207 (N91029), Homer, AK, destroyed, 1 fatal. Probable cause: A fatigue failure, and partial separation of the number 6 engine cylinder head assembly, the operator's inadequate progressive inspection performed by company maintenance personnel, and the pilot's… - [NTSB LAX95FA302](https://openairdocs.org/ntsb/LAX95FA302), Aug 23, 1995: Cessna T207 (N91004), San Diego, CA, destroyed. Probable cause: the pilot's improper fuel management and improper use of the fuel selector valve. - [NTSB ANC94LA078](https://openairdocs.org/ntsb/ANC94LA078), Jul 9, 1994: Cessna T207 (N91056), Kenai, AK, substantial damage. Probable cause: THE FAILURE OF THE ENGINE CRANKSHAFT. FACTORS IN THE ACCIDENT WERE THE PILOT'S INADEQUATE COMPENSATION FOR THE WIND CONDITIONS AND NOT ATTAINING THE PROPER TOUCHDOWN POINT AT THE SUITABLE LANDING… - [NTSB SEA92LA058](https://openairdocs.org/ntsb/SEA92LA058), Jan 9, 1992: Cessna 207 (N91056), Seattle, WA, substantial damage. Probable cause: THE CARGO DOOR UNLATCHED FOR UNDETERMINED REASONS. - [NTSB LAX90FA145](https://openairdocs.org/ntsb/LAX90FA145), Apr 13, 1990: Cessna T207 (N91081), Grand Canyon, AZ, destroyed. Probable cause: IMPROPER ADJUSTMENT OF THE TURBO-CHARGER ABSOLUTE PRESSURE CONTROLLER, AND IMPROPER MANIPULATION OF THE POWER PLANT CONTROLS BY THE PILOT DURING THE GO-AROUND. FACTORS RELATED TO THE ACCIDENT WERE:… - [NTSB DEN90LA060](https://openairdocs.org/ntsb/DEN90LA060), Feb 22, 1990: Cessna T207 (N91146), Hungry Horse, MT, destroyed. Probable cause: FAILURE OF THE #4 CONNECTING ROD. FACTORS RELATED TO THE ACCIDENT WERE: THE ADVERSE WEATHER CONDITIONS AND LACK OF SUITABLE TERRAIN FOR A FORCED LANDING. - [NTSB ATL88FA254](https://openairdocs.org/ntsb/ATL88FA254), Jul 3, 1988: Cessna T207 (N1724U), Petros, TN, destroyed, 1 fatal - [NTSB ANC84LA174](https://openairdocs.org/ntsb/ANC84LA174), Sep 15, 1984: Cessna T-207 (N1540U), Daniels Creek, AK, substantial damage - [NTSB CHI84FA058](https://openairdocs.org/ntsb/CHI84FA058), Dec 10, 1983: Cessna 207 (N208JP), Put-In-Bay, OH, substantial damage, 4 fatal - [NTSB SEA80FA042](https://openairdocs.org/ntsb/SEA80FA042), Aug 11, 1980: Cessna T207 (N91115), Salmon, ID, destroyed, 2 fatal - [NTSB LAX80FA103](https://openairdocs.org/ntsb/LAX80FA103), Jun 1, 1980: Cessna T207 (N1535U), Furnace Creek, CA, destroyed, 6 fatal - [NTSB ANC80FA033](https://openairdocs.org/ntsb/ANC80FA033), Mar 6, 1980: Cessna 207 (N1722U), South Naknek, AK, destroyed - [NTSB OAK79DA022](https://openairdocs.org/ntsb/OAK79DA022), Mar 27, 1979: Cessna 207 (N1551U), Boulder, NV, no damage - [NTSB LAX78DUM04](https://openairdocs.org/ntsb/LAX78DUM04), Nov 24, 1977: Cessna T207 (N91029), Calexico, CA, substantial damage - [NTSB FTW770A003](https://openairdocs.org/ntsb/FTW770A003), Jun 6, 1977: Cessna 207 (N1520U), Matamoros, Mexico, substantial damage - [NTSB DEN76FQA37](https://openairdocs.org/ntsb/DEN76FQA37), Mar 10, 1976: Cessna T207 (N14450), Gallup, NM, substantial damage - [NTSB ANC76AA025](https://openairdocs.org/ntsb/ANC76AA025), Aug 19, 1975: Cessna 207 (N91146), Cinder River, AK, substantial damage - [NTSB LAX76DUG09](https://openairdocs.org/ntsb/LAX76DUG09), Jul 26, 1975: Cessna 207 (N91101), Hesperia, CA, destroyed - [NTSB ANC71AA022](https://openairdocs.org/ntsb/ANC71AA022), Oct 2, 1970: Cessna 207 (N91117), Sitkinak, AK, destroyed - [NTSB DEN70D0127](https://openairdocs.org/ntsb/DEN70D0127), Oct 12, 1969: Cessna 207 (N91042), Aspen, CO, substantial damage - [NTSB DEN69A0037](https://openairdocs.org/ntsb/DEN69A0037), Mar 24, 1969: Cessna T207 (N91029), Aspen, CO, substantial damage ## FAA accident and incident reports (51, newest 50) 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 20251013014249I](https://openairdocs.org/incident/20251013014249I), Oct 13, 2025: Cessna T207 (N684S), Center Island, WA, Minor damage. On October 13, 2025, around 1321 local time, a Cessna 207 aircraft was on part 135 flight (cargo only, no passengers) departed decatur Island airport (WN07)… - [Accident 20250428014169A](https://openairdocs.org/incident/20250428014169A), Apr 28, 2025: Cessna T207 (N91025), Nanwalek, AK, Destroyed, 2 fatal. Aircraft was on approach to rwy 19. Witnesses report there was a dog on the runway. Other company aircraft flying behind accident aircraft says he heard… - [Accident 20240915012289A](https://openairdocs.org/incident/20240915012289A), Sep 15, 2024: Cessna T207 (N90193), St. Mary'S, AK, Destroyed, 4 fatal. Aircraft departed bet (bethel, AK) in marginal VFR conditions, continued the flight into IMC conditions and subsequently crashed into the side of a hill,… - [Accident 20220207001669A](https://openairdocs.org/incident/20220207001669A), Feb 7, 2022: Cessna T207 (N684S), Crane Island, WA, Substantial damage. Misjudged approach and landed short of runway. - [Accident 20170814020669A](https://openairdocs.org/incident/20170814020669A), Aug 14, 2017: Cessna T207 (N745KP), Juneau, AK, Substantial damage. On August 14, 2017, about 0633 Alaska daylight time, a Cessna T207 airplane, N745KP, sustained substantial damage after it ditched in auke bay near coghlan… - [Accident 20160823015179A](https://openairdocs.org/incident/20160823015179A), Aug 23, 2016: Cessna T207 (N91025), Nanwalek, AK, Substantial damage. Nanwalek, AK (keb): N91025, Cessna T207, landed on runway 1 and ran off the end of the runway. Pilot decision to first touchdown 500 feet down the runway… - [Incident 20151120020169I](https://openairdocs.org/incident/20151120020169I), Nov 20, 2015: Cessna T207 (N90193), Kwethluk, AK, Minor damage. The PIC was attempting to take off from runway 18, which was covered with ice and slush. During the takeoff roll, the aircraft departed the centerline to the… - [Accident 20140627010319A](https://openairdocs.org/incident/20140627010319A), Jun 27, 2014: Cessna T207 (N207AB), Indianapolis, IN, Substantial damage. On June 27, 2014, at 1219 eastern daylight time, a Cessna T207, N207AB, landed short of the runway after a power loss at Indianapolis international airport… - [Accident 20130904016709A](https://openairdocs.org/incident/20130904016709A), Sep 4, 2013: Cessna T207 (N211AS), Colorado Spring, CO, Substantial damage. On 09/04/2013 at approximately 0755 MDT, N211AS a Cessna 207 aircraft sustained substantial damaged after impacting terrain just after takeoff from the… - [Accident 20080909857749A](https://openairdocs.org/incident/20080909857749A), Sep 9, 2008: Cessna T207 (N1754U), Substantial damage. On September 9, 2008, at approximately 4:00 pm Alaska daylight time (adt), an inland aviation services, inc. flight, number 004 sustained substantial damage… - [Accident 20050706014889A](https://openairdocs.org/incident/20050706014889A), Jul 6, 2005: Cessna T207 (N1621U), Nanwalek, AK, Destroyed, 3 fatal. (-23) The FAA was first notified of the accident on July 6, 2005. The accident occurred in a rented, wheel equipped Cessna 207 aircraft from merrill field… - [Accident 20021230035879A](https://openairdocs.org/incident/20021230035879A), Dec 30, 2002: Cessna T207 (N1599U), Brownsville, TX, Substantial damage. (.19) On December 30, 2002, at 1440 central standard time, a Cessna T207 single-engine airplane, N1599U, was substantially damaged when it impacted terrain… - [Incident 20021106032139I](https://openairdocs.org/incident/20021106032139I), Nov 6, 2002: Cessna T207 (N91060), Bethel, AK, Minor damage. (-23) While two airplanes were involved in this incident, only one was in motion. N91060, a CE-207 was being taxiied for departure by Mr. Brawn. A CE-152,… - [Accident 20020915024549A](https://openairdocs.org/incident/20020915024549A), Sep 15, 2002: Cessna T207 (N207DG), Circle, AK, Minor damage. (-23) [privacy data omitted] crashed on takeoff after attempt to abort; flaps were set to takeoff position of 10* degrees but extended only to 3* degrees.… - [Accident 19980913023679A](https://openairdocs.org/incident/19980913023679A), Sep 13, 1998: Cessna T207 (N1754U), Sleetmute, AK, Substantial damage. Air taxi struck an unidentified object with its tail on rotation for takeoff, acft returned to the arpt with some difficulty and landed safely with substantail… - [Accident 19980206002389A](https://openairdocs.org/incident/19980206002389A), Feb 6, 1998: Cessna T207 (N91029), Homer, AK, Destroyed, 1 fatal. Aircraft climbed to 150 ft AGL on takeoff. Banked into steep turn and dove into snow covered ground. (.4)the certificated commercial pilot was departing on a… - [Incident 19961123041779I](https://openairdocs.org/incident/19961123041779I), Nov 23, 1996: Cessna T207 (N1644U), San Luis Obispo, CA, Minor damage. Lost power. Activated boost pump. Restored then failed again. Landed off airport. Fuel selected empty tank. - [Incident 19951031042309I](https://openairdocs.org/incident/19951031042309I), Oct 31, 1995: Cessna T207 (N91029), Anchorage, AK, Minor damage. Narrative: on October 31, 1995, a cargo CE-207 operated by southcentral air experienced engine difficulties on approach to the Anchorage International Airport.… - [Accident 19950823046899A](https://openairdocs.org/incident/19950823046899A), Aug 23, 1995: Cessna T207 (N91004), San Diego, CA, Destroyed. Lost power on go around. Crash landed on a freeway. Fuel selector between right main and off position. - [Incident 19940826034089I](https://openairdocs.org/incident/19940826034089I), Aug 26, 1994: Cessna T207 (N1599U), Stanley, ID, Minor damage. Rough engine. Vision restricted on landing due engine oil on windshield. Overshot runway. Connecting rod failure. - [Accident 19940708018279A](https://openairdocs.org/incident/19940708018279A), Jul 8, 1994: Cessna T207 (N91056), Kenai, AK, Substantial damage. Engine failed en route. Siezed. Overshot landing on nearby strip. Crankshaft failed. Had altitude to land on strip. - [Accident 19920109005069A](https://openairdocs.org/incident/19920109005069A), Jan 9, 1992: Cessna 207 (N91056), Seattle, WA, Substantial damage. Rear half baggage door opened on descent. Slammed fuselage. Distorted tailcone bulkhead. Cause undetermined. - [Incident 19910804038979I](https://openairdocs.org/incident/19910804038979I), Aug 4, 1991: Cessna T207 (N1621U), Denali, AK. Engine seized in flight. Landed safely at airstrip. NR3 cylinder exhaust valve had come off. Oil lost. - [Accident 19900413008809A](https://openairdocs.org/incident/19900413008809A), Apr 13, 1990: Cessna T207 (N91081), Grand Canyon, AZ, Destroyed. Engine backfired on go around in gusty wind. Untrained pilot lost control. Struck trees. Fuel control maladjusted. - [Accident 19900221005709A](https://openairdocs.org/incident/19900221005709A), Feb 21, 1990: Cessna T207 (N91146), Hungry Horse, MT, Destroyed. Engine threw rod at night in IFR. Saw cloud obscured ridge too late to avoid impact. Cylinder work prior to flight. - [Incident 19890628038629I](https://openairdocs.org/incident/19890628038629I), Jun 28, 1989: Cessna T207 (N91056), Helena, MT, Minor damage. Collided with a parked aircraft while taxiing to the ramp for a routine engine runup. - [Accident 19880702035659A](https://openairdocs.org/incident/19880702035659A), Jul 2, 1988: Cessna T207 (N1724U), Petros, TN, Destroyed, 1 fatal. Flew into trees at night near top of a ridge. Low ceiling, light rain and haze in area. No weather briefing. - [Incident 19880126009139I](https://openairdocs.org/incident/19880126009139I), Jan 26, 1988: Cessna T207 (N91060), Minneapolis, MN. Fuel flow fluctuation and rough engine. Engine quit on final. Left 30 minutes later. Possible ice in fuel tanks. - [Accident 19870629034259A](https://openairdocs.org/incident/19870629034259A), Jun 29, 1987: Cessna T207 (N91131), Walkers Cay, Bahamas, Destroyed. The aircraft reportedly bounced on landing, veered off the runway, and hit a wind sock, trees and tennis court. - [Incident 19870605039909I](https://openairdocs.org/incident/19870605039909I), Jun 5, 1987: Cessna T207 (N91029), Great Falls, MT. Electrical power loss en route. Safe landing at destination. Battery had shorted internally. - [Incident 19850509035709I](https://openairdocs.org/incident/19850509035709I), May 9, 1985: Cessna T207 (N91016), Crystal, MN, Minor damage. As pilot taxied and storm passed through area, a gust of wind caused swerve. Struck VASI lights. - [Accident 19840914051359A](https://openairdocs.org/incident/19840914051359A), Sep 14, 1984: Cessna T207 (N1540U), Daniels Creek, AK, Substantial damage. Struck trees during a belated go around. Made go around in lieu of overshooting the runway. - [Incident 19840315020969I](https://openairdocs.org/incident/19840315020969I), Mar 15, 1984: Cessna T207 (N91029), Broomfield, CO. Engine malfunction. Loss of engine turbo charger. On teardown engine showed lack of lubrication. No oil in engine. - [Incident 19840127015339I](https://openairdocs.org/incident/19840127015339I), Jan 27, 1984: Cessna T207 (N91056), Douglas, WY. Engine failed. Landed on an interstate highway. A cylinder had separated from the engine. - [Accident 19831209075299A](https://openairdocs.org/incident/19831209075299A), Dec 9, 1983: Cessna T207 (N208JP), Put In Bay, OH, Destroyed, 3 fatal. Crashed into cold lake waters at night with fog in area. No mechanical defects found. Exposure and drowning fatals. - [Incident 19831116071139I](https://openairdocs.org/incident/19831116071139I), Nov 16, 1983: Cessna T207 (N91146), Berthoud, CO, Minor damage. Engine failure on leveling off to cruise. Broken connecting rod from a loose lower rod bolt for no 3 cylinder. - [Incident 19830412024129I](https://openairdocs.org/incident/19830412024129I), Apr 12, 1983: Cessna T207 (N1678U), Denver, CO. Loss of engine power on climbout. Returned to other runway. Loose intake hoses caused manifold pressure loss. - [Incident 19811203087819I](https://openairdocs.org/incident/19811203087819I), Dec 3, 1981: Cessna T207 (N1635U), Laramie, WY. Lost manifold pressure. Landed at airport. Engine turbo system totally seized. 130 hours since overhaul. - [Accident 19810821051149A](https://openairdocs.org/incident/19810821051149A), Aug 21, 1981: Cessna T207 (N1746U), Casper, WY, Destroyed. Impacted trees in box canyon. Over gross weight. Cargo not properly secured. Under appeal for license suspension. - [Incident 19810601039109I](https://openairdocs.org/incident/19810601039109I), Jun 1, 1981: Cessna T207 (N1754U), Noorvik, AK, Minor damage. Nosewheel sank into mud with prop damage during landing on a notamed closed muddy runway under construction. - [Incident 19810428029749I](https://openairdocs.org/incident/19810428029749I), Apr 28, 1981: Cessna T207 (N1724U), Fremont, CA, Minor damage. Pilot landed aircraft about halfway down runway and blew a tire using excessive braking. - [Accident 19800811037329A](https://openairdocs.org/incident/19800811037329A), Aug 11, 1980: Cessna T207 (N91115), Salmon, ID, Destroyed, 1 fatal. Indicates operation of aircraft at low altitude, mountain area to observe wild game. Failed to clear rising terrain - [Accident 19800601023939A](https://openairdocs.org/incident/19800601023939A), Jun 1, 1980: Cessna T207 (N1535U), Furnace Creek, CA, Destroyed, 5 fatal. Aircraft reported missing and crash was found 2 days later. Pilot was not certificated. - [Accident 19800306010069A](https://openairdocs.org/incident/19800306010069A), Mar 6, 1980: Cessna T207 (N1722U), South Naknek, AK, Destroyed. Tried to land in low ceiling and visibility with windshield ice covered. Hit runway on angle, bounced, hit bank. - [Incident 19790610014829I](https://openairdocs.org/incident/19790610014829I), Jun 10, 1979: Cessna 207 (N1552U), Dillon, MT. Engine stopped, operated with high boost, then quit again. 1st failure from fuel contamination. 2nd high boost. - [Incident 19790327011719I](https://openairdocs.org/incident/19790327011719I), Mar 27, 1979: Cessna 207 (N1551U), Las Vegas, NV. Flight encountered sever turbulance near mt wilson at 6500 ft. - [Incident 19780719043739I](https://openairdocs.org/incident/19780719043739I), Jul 19, 1978: Cessna 207 (N91115), Thomas Creek, ID, Minor damage. Pilot landed too FAR down a short runway and overshot. - [Accident 19771024034419A](https://openairdocs.org/incident/19771024034419A), Oct 24, 1977: Cessna T207 (N91029), Calexico, CA, Substantial damage. Struck lighted taxiway barrier. Plt asked for full flaps,son lowered partial flaps. Close in apch. - [Accident 19770606021929A](https://openairdocs.org/incident/19770606021929A), Jun 6, 1977: Cessna T207 (N1520U), Matamoros, Substantial damage. Invest under jurisdiction of govt of Mexico. - [Accident 19760310028489A](https://openairdocs.org/incident/19760310028489A), Mar 10, 1976: Cessna T207 (N14450), Gallup, NM, Substantial damage. Acft went on its back. Engine ran normal during post-accident test. Acft landed on dirt road. All 51: https://openairdocs.org/model/cessna-t207/incidents.md ## Service difficulty reports (30) As reported by operators and repair stations, by the model named in the report. - [SDR 2020F00280](https://openairdocs.org/sdr/2020F00280), Jan 22, 2020: LIFTER. SPALLED. REMOVED ALL HYDRAULIC LIFTERS TO INSPECT FOR SPALLING, DISCOVERED BADLY SPALLED EXHAUST LIFTER ON CYLINDER #4. INSPECTED CAM IN ACCORDANCE WITH CONTINENTAL SERV - [SDR OW6A202001220062](https://openairdocs.org/sdr/OW6A202001220062), Dec 27, 2018: BRAKE CALIPER. LEAKING. LEFT BRAKE FAILED, IT HAD WORKED FINE DURING RUN-UP. PILOT TOOK OFF AND THEN FOUND IT INOPERATIVE ON LANDING. LANDING WAS UNEVENTFUL. - [SDR YAAA20150428005](https://openairdocs.org/sdr/YAAA20150428005), Apr 26, 2015: CYLINDER HEAD. CRACKED. DURING 100 HR INSPECTION BORESCOPED ENG & FOUND NR 6 CYLINDER CRACKED FROM LOWER SPARK PLUG BOSS TOWARDS EXHAUST VLV SEAT. - [SDR YAAA20150428004](https://openairdocs.org/sdr/YAAA20150428004), Apr 26, 2015: CYLINDER HEAD. CRACKED. DURING 100 HR INSPECTION BORESCOPED ENG & FOUND NR 5 CYLINDER CRACKED FROM LOWER SPARK PLUG BOSS TOWARDS EXHAUST VLV SEAT. - [SDR YAAA20150428003](https://openairdocs.org/sdr/YAAA20150428003), Apr 26, 2015: CYLINDER HEAD. CRACKED. DURING 100 HR INSPECTION BORESCOPED ENG & FOUND NR 4 CYLINDER CRACKED FROM LOWER SPARK PLUG BOSS TOWARDS EXHAUST VLV SEAT. - [SDR YAAA20150428002](https://openairdocs.org/sdr/YAAA20150428002), Apr 26, 2015: CYLINDER HEAD. CRACKED. DURING 100 HR INSPECTION BORESCOPED ENG & FOUND NR 3 CYLINDER CRACKED FROM LOWER SPARK PLUG BOSS TOWARDS EXHAUST VLV SEAT. - [SDR YAAA20150428001](https://openairdocs.org/sdr/YAAA20150428001), Apr 26, 2015: CYLINDER HEAD. CRACKED. DURING 100 HR INSPECTION BORESCOPED ENG & FOUND NR 2 CYLINDER CRACKED FROM LOWER SPARK PLUG BOSS TOWARDS EXHAUST VLV SEAT. - [SDR CKE2013F00001](https://openairdocs.org/sdr/CKE2013F00001), Mar 12, 2013: BUSHING. LOOSE. FUEL INJECTOR BUSHINGS DID NOT STAY IN PLACE WHEN FUEL INJECTORS WERE REMOVED. INJECTORS WERE REMOVED FOR CLEANING. THIS ENGINE HAS 11TSMOH AND 4 OUT OF THE 6 B - [SDR YAA2010F00000](https://openairdocs.org/sdr/YAA2010F00000), Dec 18, 2009: UNKNOWN. ODOR. DEPARTED NORTH BOUND. EXPERIENCED A BURNING SCENT IN CABIN IN FLIGHT AND LATER CLAIMED TO SEE SMOKE EMITTING FROM ENGINE INSTRUMENT CLUSTER. PILOT THEN DIVERTED - [SDR 2005FA0001065](https://openairdocs.org/sdr/2005FA0001065), Apr 14, 2005: ANTENNA. INOPERATIVE. FOUND UPPER UAT ANTENNA UNSERVICEABLE. (K) - [SDR 2005FA0001054](https://openairdocs.org/sdr/2005FA0001054), Apr 14, 2005: ANTENNA. INOPERATIVE. FOUND UPPER UAT ANTENNA UNSERVICEABLE. (K) - [SDR FMA2004F00000](https://openairdocs.org/sdr/FMA2004F00000), Oct 4, 2004: CONTACTOR. DEFECTIVE. PILOT REPORTED MISFIRE DURING MAG CHECK. TROUBLESHOOTING REVEALED RIVETING OF GROUND SIDE OF CONTACT TO MOUNTING BASE HAD FAILED ALLOWING ELECTRICAL CONTACT TO - [SDR FMAA2002002](https://openairdocs.org/sdr/FMAA2002002), Sep 15, 2002: SWITCH. INOPERATIVE. FLAP SWITCH IS HELD TO THE ARM ASSEMBLY WITH SMALL NR 40 MACHINE SCREWS. IF SCREWS ARE OVER TIGHTENED, THE PLASTIC SWITCH CRACKS, IF IT IS NOT TIGHTENED ENOUGH, - [SDR VDQ2001F00005](https://openairdocs.org/sdr/VDQ2001F00005), Oct 12, 2001: CYLINDER. CRACKED. ALL 6 CYLINDERS CRACKED AT 781.6 HOURS SINCE NEW. SERIAL NUMBERS: 52A0016149, 52A0016150, 52A0016201, 52A0016202, 52A0016215, 52A0016217. - [SDR VDQ2001F00004](https://openairdocs.org/sdr/VDQ2001F00004), Oct 12, 2001: CYLINDER. CRACKED. ALL 6 CYLINDERS CRACKED AT 781.6 HOURS SINCE NEW. SERIAL NUMBERS: 52A0016149, 52A0016150, 52A0016201, 52A0016202, 52A0016215, 52A0016217. - [SDR VDQ2001F00003](https://openairdocs.org/sdr/VDQ2001F00003), Oct 12, 2001: CYLINDER. CRACKED. ALL 6 CYLINDERS CRACKED AT 781.6 HOURS SINCE NEW. SERIAL NUMBERS: 52A0016149, 52A0016150, 52A0016201, 52A0016202, 52A0016215, 52A0016217. - [SDR VDQ2001F00002](https://openairdocs.org/sdr/VDQ2001F00002), Oct 12, 2001: CYLINDER. CRACKED. ALL 6 CYLINDER CRACKED AT 781.6 HOURS SINCE NEW. SERIAL NUMBERS: 52A0016149, 52A0016150, 52A0016201, 52A0016202, 52A0016215, 52A0016217. - [SDR VDQ2001F00001](https://openairdocs.org/sdr/VDQ2001F00001), Oct 12, 2001: CYLINDER. CRACKED. ALL 6 CYLINDERS CRACKED AT 781.6 HOURS SINCE NEW. SERIAL NUMBERS: 52A0016149, 52A0016150, 52A0016201, 52A0016202, 52A0016215, 52A0016217. - [SDR VDQ2001F00000](https://openairdocs.org/sdr/VDQ2001F00000), Oct 12, 2001: CYLINDER. CRACKED. ALL 6 CYLINDER CRACKED AT 781.6 HOURS SINCE NEW. SERIAL NUMBERS: 52A0016149, 52A0016150, 52A0016201, 52A0016202, 52A0016215, 52A0016217 - [SDR HUK2001F00001](https://openairdocs.org/sdr/HUK2001F00001), Sep 6, 2001: INDICATOR. SHORTED. OIL TEMPERATURE GAUGE SUPPLIED WITH SERVICE KIT-OIL GAUGE SHORTED OUT INTERNALLY BLOWING OUT POWER CONVERTER. THIS WAS THE 3RD GAUGE IN 4 YEARS. WHEN POWER CONV - [SDR HUK2001F00000](https://openairdocs.org/sdr/HUK2001F00000), Sep 3, 2001: GAUGE. DAMAGED. OIL TEMPERATURE GUAGE (ROCHESTER SERVICE KIT) FAILED CAUSEING OVER VOLTAGE PROBLEM THROUGH-OUT. SHORTING OUT ALTERNATOR, VOLTAGE REGULATOR, OVER VOLTAGE SENSOR, - [SDR 20001101SH005](https://openairdocs.org/sdr/20001101SH005), Oct 9, 2000: MAGNETO. DEFECTIVE. ON INITIAL POWER-UP FOR THE FLIGHT''S TAKEOFF ROLL, THE ENGINE LOST SUBSTANTIAL POWER. THE PILOT ROLLED OFF TO A TAXIWAY AND SHUT DOWN. AFTER TROUBLESHOOTING TH - [SDR 97ZZZX276](https://openairdocs.org/sdr/97ZZZX276), Dec 24, 1996: BULKHEAD. CRACKED. DURING C/W OF AD 72 07-09, FOUND 4 CRACKS IN BULKHEAD P/N 1212859-1 AND 3 CRACKS IN BULKHEAD P/N 1212409-6. THE REST OF THE FIN STRUCTURE WAS DYE CHCKED AND INS - [SDR 97ZZZX275](https://openairdocs.org/sdr/97ZZZX275), Dec 24, 1996: BULKHEAD. CRACKED. DURING C/W OF AD 72 07-09, FOUND 4 CRACKS IN BULKHEAD P/N 1212859-1 AND 3 CRACKS IN BULKHEAD P/N 1212409-6. THE REST OF THE FIN STRUCTURE WAS DYE CHCKED AND INS - [SDR 97ZZZX191](https://openairdocs.org/sdr/97ZZZX191), Dec 18, 1996: BULKHEAD. CRACKED. INSPECTION FOUND 3 CRACKS IN BULKHEAD AND 4 IN BULKHEAD DOUBLER. INSPECTION AND REPLACEMENT OF PARTS DONE IAW AD 72-07-09 AND CESSNA SE 72-3 AND SE 72-29. - [SDR 95ZZZX7019](https://openairdocs.org/sdr/95ZZZX7019), Dec 1, 1995: CLAMP. BROKEN. PRE-FLIGHT REVEALED LOOSE TAILPIPE. FOUND CLAMP BROKEN. CLAMP APPEARED TO BE HIGH-TIME, BUT ENGINE WAS INSTALLED LESS THAN 50 HOURS EARLIER. SUBMITTER RECOMMEND - [SDR 95ZZZX6450](https://openairdocs.org/sdr/95ZZZX6450), Oct 31, 1995: CYLINDER. DEPARTED. NR 6 CYLINDER DEPARTED THE CASE. ALL THE CYLINDER BASE STUDS WERE BROKEN. - [SDR 95ZZZX6175](https://openairdocs.org/sdr/95ZZZX6175), Oct 13, 1995: CYLINDER. CRACKED. ROUGHLY 15 MINUTES INTO FLIGHT, THE ENGINE LOST MANIFOLD PRESSURE. MAXIMUM M/P WAS 25 INCHES. INSPECTION FOUND THE NR 4 CYLINDER CRACKED AND STARTING TO MELT TH - [SDR 95ZZZX6743](https://openairdocs.org/sdr/95ZZZX6743), Sep 1, 1995: CYLINDER. CRACKED. INSPECTION FOUND CYLINDER HEAD WAS SUBSTANTIALLY CRACKED FROM BOTTOM SPARK PLUG HOLE TO TOP SPARK PLUG HOLE THROUGH THE EXHAUST PORT. SUBMITTER STATED THIS IS T - [SDR 95ZZZX1306](https://openairdocs.org/sdr/95ZZZX1306), Feb 27, 1995: MOUNT ARM. FAILED. FOUND TURBOCHARGER MOUNT EAR CRACKED IN TWO PIECES. SUBMITTER SUSPECTS THE MOUNTING ARMS WERE IMPROPERLY INSTALLED AND HARDWARE WAS OVERTORQUED. SUBMITTER SUGGE --- 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.