# Textron 182 - Type: Aircraft model (FAA registry) - Registry code: 2072700 - Manufacturer (registry): TEXTRON AVIATION INC - Model: 182 - Aircraft type: Fixed wing single engine - Category: Airplane - Engines: 1 · Reciprocating - Seats: 4 - Weight class: Up to 12,499 lb - Certification: Type certificated - Data sheet: [TCDS 3A13](https://openairdocs.org/tcds/3A13) (OpenAirDocs) - Holder: Textron Aviation Inc. - Registered aircraft: 0 - Page: https://openairdocs.org/model/textron-182 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 2020-21-22](https://openairdocs.org/ad/2020-21-22): Fuselage; Stabilizers · Textron 180, 180A, 180B and 21 more. Effective Dec 7, 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 2008-10-02](https://openairdocs.org/ad/2008-10-02): Part number identification placard · Cessna 172, 172R, 172RG and 64 more. Effective May 12, 2008 - [AD 2006-12-07](https://openairdocs.org/ad/2006-12-07): ECi cylinder assemblies · Aerostar AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 386 more. Effective Jul 11, 2006 - [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 2001-23-17](https://openairdocs.org/ad/2001-23-17): GNS 430 units · Cessna 172, 182, 206 and 209 more. Effective Dec 28, 2001 - [AD 98-21-21 R1](https://openairdocs.org/ad/98-21-21-R1): Electric Inflatable Door Seals · Cessna 17-30, 17-30A, 17-31 and 267 more. Effective May 1, 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 98-16-04](https://openairdocs.org/ad/98-16-04): Inspect Angle Stiffener Along Lower Spar Cap · Cessna 180, 180A, 180B and 37 more. Effective Sep 21, 1998 - [AD 98-14-03](https://openairdocs.org/ad/98-14-03): Transponders · Cessna 172, 172A, 172B and 230 more. Effective Aug 16, 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 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 83-17-06](https://openairdocs.org/ad/83-17-06): Aileron Balance Weights · Flap actuated aileron droop system (Sierra Industries STC SA1382WE or 5 others). Effective Sep 1, 1983 - [AD 83-13-01](https://openairdocs.org/ad/83-13-01): Placard-Improper Fuel Cap Sealing · Cessna 182, 182A, 182B and 14 more. Effective Aug 1, 1983 - [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 79-08-03](https://openairdocs.org/ad/79-08-03): Electrical System · Cessna 120, 140, 140A and 152 more. Effective Jun 6, 1979 - [AD 78-05-06](https://openairdocs.org/ad/78-05-06): Flexible Fuel Cells · Cessna 180, 182, 185 and 98 more. Effective Jun 30, 1978 - [AD 78-01-14](https://openairdocs.org/ad/78-01-14): ELT Installation · Cessna 182, 182A, 182B and 16 more. Effective Jan 23, 1978 - [AD 77-23-11](https://openairdocs.org/ad/77-23-11): ELT Installation · Cessna 182, 182A, 182B and 16 more. Effective Nov 28, 1977 - [AD 77-04-05](https://openairdocs.org/ad/77-04-05): Carburetor Air Intake · Cessna 180, 180A, 180B and 39 more. Effective Mar 1, 1977 - [AD 77-02-09](https://openairdocs.org/ad/77-02-09): Wing Flap System · Cessna 150, 150A, 150B and 61 more. Effective Feb 3, 1977 - [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 75-05-02](https://openairdocs.org/ad/75-05-02): Engine Oil · Beryl D Shannon Aviation Specialties Engine Crankcase… (D'Shannon Products STC SA2653WE). Effective Feb 21, 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 - [AD 73-23-07](https://openairdocs.org/ad/73-23-07): Defective Spar Attachment Fittings · Cessna 150, 150A, 150B and 68 more. Effective Nov 19, 1973 - [AD 73-17-01](https://openairdocs.org/ad/73-17-01): Fuel Transfer Pump Placard · Cessna 170, 170A, 170B and 53 more. Effective Aug 16, 1973 - [AD 71-22-02](https://openairdocs.org/ad/71-22-02): Cracks In Nose Gear Fork · Cessna 150, 150A, 150B and 52 more. Effective Nov 9, 1971 - [AD 59-10-03](https://openairdocs.org/ad/59-10-03): Flasher Switch · Cessna 172, 180, 180A and 2 more 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) (18) - [SAIB 2026-08](https://openairdocs.org/saib/2026-08): Floats. Issued Mar 24, 2026 - [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018 - [SAIB CE-18-23](https://openairdocs.org/saib/CE-18-23): Passenger Compartment Equipment - Installation of F. Atlee Dodge Aircraft Services LLC. Folding Jump Seats. Issued Jul 19, 2018 - [SAIB CE-17-25](https://openairdocs.org/saib/CE-17-25): ELEVATOR TORQUE TUBE Inspections for cracks and corrosion in elevator torque tubes. Issued Aug 25, 2017 - [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-09-42](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-08-02](https://openairdocs.org/saib/CE-08-02): Flight Controls. Issued Nov 2, 2007 - [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 - [SAIB CE-06-46R1](https://openairdocs.org/saib/CE-06-46R1): . Issued Sep 18, 2006 - [SAIB CE-04-72R1](https://openairdocs.org/saib/CE-04-72R1): . Issued Aug 18, 2004 - [SAIB CE-04-72](https://openairdocs.org/saib/CE-04-72) (historical): . Issued Jul 29, 2004 - [SAIB CE-04-11](https://openairdocs.org/saib/CE-04-11): . Issued Oct 28, 2003 - [SAIB CE-90-03R2](https://openairdocs.org/saib/CE-90-03R2): . Issued Aug 26, 2002 - [SAIB CE-01-41](https://openairdocs.org/saib/CE-01-41) (historical): . Issued Sep 10, 2001 - [SAIB CE-90-03R1](https://openairdocs.org/saib/CE-90-03R1) (historical): . Issued Jul 27, 2000 ## Registered aircraft None registered with this model now. ## STCs approved for it (633, first 50) - [STC SA00006WI](https://openairdocs.org/stc/SA00006WI): Replacement of rear passenger bench seat with two individual seats. Richard Barker - [STC SA00021WI](https://openairdocs.org/stc/SA00021WI): Conversion to a tailwheel configuration. Richard C Barker - [STC SA00026IB](https://openairdocs.org/stc/SA00026IB): Validation for the Installation of Beringer Wheels, axles, brake and master-cylinders. Beringer Aero - [STC SA00028WI](https://openairdocs.org/stc/SA00028WI): Installation of flap and aileron gap seals.. Flight Enhancements - [STC SA00057LA](https://openairdocs.org/stc/SA00057LA): Installation of a heat shield.. LOREE AIR - [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 SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector.. Alcor LLC - [STC SA00103BO](https://openairdocs.org/stc/SA00103BO): Installation of Weemax cabin air vent.. Victor Morrel - [STC SA00147AT](https://openairdocs.org/stc/SA00147AT): Installation of Type A sun visor.. Stapleton James W. - [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 SA00165BO](https://openairdocs.org/stc/SA00165BO): Installation of Avidyne Corporation Datalink Coupler, part number 700-00015-000 per Avidyne Corporation Master Document List, Document No. AVACP-006 dtd 1/2/93 or later FAA-approved revisions.. Avidyne Corporation - [STC SA00186AT](https://openairdocs.org/stc/SA00186AT): Installation of carbon steel brake discs that have melonite surface treatment.. Aviation Products, Inc - [STC SA00188AT](https://openairdocs.org/stc/SA00188AT): Installation of Appalachian Accessories carbon steel brake discs that have the melonite surface treatment, P/N AA-26A.. Aviation Products, Inc - [STC SA00194AT](https://openairdocs.org/stc/SA00194AT): Installation of Appalachian Accessories carbon steel brake discs that have the melonite surface treatment, P/N AA-40.. Aviation Products, Inc - [STC SA00210AT](https://openairdocs.org/stc/SA00210AT): Installation of carbon steel brake discs that have melonite surface treatment, P/N AA-90.. Aviation Products, Inc - [STC SA00211AT](https://openairdocs.org/stc/SA00211AT): Installation of carbon steel brake discs that have melonite surface treatment.. Aviation Products, Inc - [STC SA00212AT](https://openairdocs.org/stc/SA00212AT): Installation of carbon steel brake discs that have melonite surface treatment.. Aviation Products, Inc - [STC SA00215NY](https://openairdocs.org/stc/SA00215NY): Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system.. CAVU Products Limited - [STC SA00236SE](https://openairdocs.org/stc/SA00236SE): Installation of an extended baggage compartment. Athena Aircraft, LLC - [STC SA00238SE](https://openairdocs.org/stc/SA00238SE): Installation of Aviation Development Corporation's sump mounted chip detector. Aviation Development Corporation - [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 SA00270WI](https://openairdocs.org/stc/SA00270WI): Installation of fiberglass replacement wing tips.. Aircraft Development Co - [STC SA00276NY](https://openairdocs.org/stc/SA00276NY): Reinforcement of wing assemblies and installation of Air Research Technology wing tip extension.. Air Research Technology, Inc - [STC SA00279LA](https://openairdocs.org/stc/SA00279LA): Installation of Ameri-King AK-950 Global Positioning System Navigation Switching/Annunciator Panel and Associated Equipment. Ameri-King 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 SA00393SE](https://openairdocs.org/stc/SA00393SE): Installation of the G/S 2500 and G/S2500R Aircraft Security Alarm System.. Protective Technologies Int - [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 SA00406WI](https://openairdocs.org/stc/SA00406WI): Installation of replacement flap trailing edge bulbs with AOG Drawing. Athena Aircraft, LLC - [STC SA00410BO](https://openairdocs.org/stc/SA00410BO): Installation of an AV-30-C Multi-Mode Indicator. uAvionix Corporation - [STC SA00419NY](https://openairdocs.org/stc/SA00419NY): Installation of cockpit utility light.. Burns Richard G - [STC SA00424SE](https://openairdocs.org/stc/SA00424SE): Installation of Precise Flight Model 100(electric) Speedbrake System.. Precise Flight Inc - [STC SA00432SE](https://openairdocs.org/stc/SA00432SE): Installation of EGT 701 series fuel flow instrument.. J P Instruments - [STC SA00465NY](https://openairdocs.org/stc/SA00465NY): Installation of Meterological Measurement System, Model A1MMS-10, with optional installation of Telemetry Module, Model AIRDAT-9600.. Aventech Research Inc - [STC SA00478SE](https://openairdocs.org/stc/SA00478SE): Replace existing horizontal stabilizer skins. Athena Aircraft, LLC - [STC SA00496SE](https://openairdocs.org/stc/SA00496SE): Installation of Oregon Aircraft Design Engine Mount Heat Shields.. Oregon Aircraft Design LLC - [STC SA00508WI](https://openairdocs.org/stc/SA00508WI): Energy absorbing seat.. Impact Dynamics, Inc - [STC SA00512SE](https://openairdocs.org/stc/SA00512SE): Fabrication of a vortex generator system.. Aeronautical Testing Service Inc. - [STC SA00642SE](https://openairdocs.org/stc/SA00642SE): Installation of a Ski Tube compartment extending aft of the baggage compartment. Athena Aircraft, LLC - [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. All 633: https://openairdocs.org/model/textron-182/stcs.md ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (90, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR 2024FA0000981](https://openairdocs.org/sdr/2024FA0000981), Dec 23, 2024: FUEL. UNKNOWN. I AM CONCERNED ABOUT ADVERSE EFFECTS FROM A NEW UNLEADED FUEL (G100UL) THAT WAS APPROVED VIA THE STC PROCESS (SA01967WI & SE01966WI) AND RECENTLY INTRODUCED AT - [SDR 2023FA0000344](https://openairdocs.org/sdr/2023FA0000344), Jun 27, 2023: SOLENOID. DEFECTIVE. LANDING GEAR HYDRAULIC POWER PACK SOLENOID FAILED. AIRCRAFT LANDED WITH NOSE GEAR DOWN AND LOCKED BUT LEFT AND RIGHT MAIN GEARS FOLDED ON LANDING. DAMAGE TO RIG - [SDR CA190213015](https://openairdocs.org/sdr/CA190213015), Feb 13, 2019: PIN. DISLODGED. (CAN) IMPULSE COUPLING PIN (NO PART NUMBER FOR ONLY THE PIN) NORMALLY PRESSED INTO MAGNETO HOUSING HAD COME OUT OF THE HOUSING ALLOWING OIL TO ENTER THE CASE OF - [SDR 2017FA0000192](https://openairdocs.org/sdr/2017FA0000192), May 16, 2017: BARREL. BROKEN. NOSE WHEEL SHIMMY DAMPENER BARREL ASSEMBLY. ATTACHMENT BOSS BROKE CAUSING SHIMMY DAMPENER TO LOSE ITS FLUID CAUSING LOSS OF STEERING CONTROL. - [SDR RJWR001](https://openairdocs.org/sdr/RJWR001), Jan 5, 2016: ANGLE. CRACKED. DURING MAINTENANCE, BATTERY MOUNT STRUCTURE FOUND CRACKED ACFT REQUIRING REPLACEMENT. - [SDR 2016FA0000279](https://openairdocs.org/sdr/2016FA0000279), Jul 20, 2015: PAN. MISMANUFACTURED. ENGINE FAILURE DURING FLIGHT ON FACTORY REMANUFACTURED ENGINE WITH 406 HRS. INSPECTION FOUND MIS-MANUFACTURED OIL PAN/SUMP ASSOCIATED WITH STC 09319SC. SPECIFIC - [SDR 2014FA0000202](https://openairdocs.org/sdr/2014FA0000202), Mar 15, 2014: SPAR. CRACKED. LEFT ELEVATOR SPAR, FOUND TO BE CRACKED DURING POST FLIGHT INSPECTION. NO PRIOR GROUND OR FLIGHT DAMAGE INCIDENTS REPORTED. THE LT ELEVATOR FOUND TO BE CRACKED - [SDR CA140211008](https://openairdocs.org/sdr/CA140211008), Feb 5, 2014: BOLT. SHEARED. (CAN) DURING CPCP INSPECTION AND 1000 HR U-BOLT REPLACEMENT. RT GEAR U-BOLT WAS FOUND TO BE SHEARED AT BOTTOM OF REAR THREADS. SUSPECTED NUT WAS OVER TORQUED AN - [SDR CA131219015](https://openairdocs.org/sdr/CA131219015), Dec 16, 2013: SPAR. CORRODED. (CAN) DURING CPCP BASE CORROSION INSPECTION. WHILE ACCOMPLISHING SID 57-11-01 WING STRUCTURE INSPECTION. DURING CLEANING OF SPAR BLOCKS SEVERE EXFOLIATION CORRO - [SDR CA090826015](https://openairdocs.org/sdr/CA090826015), Jul 13, 2009: SHAFT. MISSING. MASSIVE OIL LOSS DURING FLIGHT. ACFT LANDED ON HYW 17. ACFT LOADED ONTO TRANSPORT AND RELOCATED. INSP REVEALED ENG PLUG PN LW-13896 HANGING FROM LOCKING. PROPEL - [SDR 2009FA0000294](https://openairdocs.org/sdr/2009FA0000294), Apr 10, 2009: STRUT. WORN. DURING ENGINE CHANGE AND ENGINE MOUNT CHANGE, THE AIR/OIL SEPARATOR BREATHER TUBE WAS REMOVED (ATTACHED BY THREE CLAMPS TO THE FIREWALL) FROM THE FIREWALL. THE - [SDR 2009FA0000281](https://openairdocs.org/sdr/2009FA0000281), Mar 31, 2009: REINFORCEMENT. CRACKED. FOUND DURING ANNUAL INSP, LT ATTACHMENT PIVOT POINT FOR HORIZ STAB (REINFORCEMENT ASSY PN 07120487) CRACKED AT BOLT HOLE EXTENDING TO EDGE OF BRACKET. REPLACED - [SDR 2008FA0000848](https://openairdocs.org/sdr/2008FA0000848), Nov 19, 2008: HOSE. DETERIORATED. ENGINE LOST RPM AND PARTIAL POWER ON GO-AROUND FROM REJECTED LANDING. ACFT THEN FLEW NORMAL PATTERN AND LANDED WITHOUT INCIDENT. GROUND RUN-UP SHOWED NO ABNORMA - [SDR RIS2006F00000](https://openairdocs.org/sdr/RIS2006F00000), Oct 5, 2006: LINE. CHAFED. FUEL LINE WAS CHAFED 90 PERCENT THRU BY AILERON CABLE. THIS ITEM SHOULD BE CHECKED ON ALL MFG AC WITH FUEL LINES RUNNING ALONG AILERON CABLES. (K) - [SDR 78978](https://openairdocs.org/sdr/78978), Mar 6, 2006: HUB. CORRODED. CORRODED HUB. - [SDR 2005FA0000497](https://openairdocs.org/sdr/2005FA0000497), Feb 23, 2005: FLYWEIGHT. CRACKED. FLYWEIGHT BASE CRACKED ALSO ASSOCIATED PART C20886 SPRING HEAD AND B20882-1. SPRING DRIVE ALSO CRACKED. (K) (22124) - [SDR 2005FA0000191](https://openairdocs.org/sdr/2005FA0000191), Feb 23, 2005: FLYWEIGHT. CRACKED. FLYWEIGHT BASE CRACKED ALSO ASSOCIATED PART, C20886 SPRING HEAD AND B20882-1, SPRING DRIVE ALSO CRACKED. (K) (REF: 22124) - [SDR EY2R0082166A](https://openairdocs.org/sdr/EY2R0082166A), Aug 19, 2004: HUB. CORRODED. FOUND CORROSION ON HUB. - [SDR EY2R00082166](https://openairdocs.org/sdr/EY2R00082166), Aug 19, 2004: HUB. CORRODED. FOUND HUB CORRODED. - [SDR 2004FA0000193](https://openairdocs.org/sdr/2004FA0000193), Feb 11, 2004: SPAR. CRACKED. DURING ANNUAL INSPECTION WHAT APPEARED TO BE A DENT WAS FOUND ON THE LOWER LEADING EDGE SKIN OF THE LEFT ELEVATOR. THIS (DENT) WAS CROSSED BY A CRACK. EXCESSIVE - [SDR 2004FA0000192](https://openairdocs.org/sdr/2004FA0000192), Feb 11, 2004: SPAR. CRACKED. DURING ANNUAL INSPECTION WHAT APPEARED TO BE A DENT WAS FOUND ON THE LOWER LEADING EDGE SKIN OF THE LT ELEVATOR. THIS (DENT) WAS CROSSED BY A CRACK. EXCESSIVE M - [SDR 2003FA0001031](https://openairdocs.org/sdr/2003FA0001031), Oct 8, 2003: CONTROL CABLE. OUT OF POSITION. A SAFETY RECOMMENDATION WAS SUBMITTED IN RESPONSE TO SEVERAL INSTANCES WHERE THE RUDDER CONTROL CABLE HAD BEEN FOUND LODGED UNDER THE MOUNTING BOLT FOR THE ELEV - [SDR CA021105010](https://openairdocs.org/sdr/CA021105010), Oct 11, 2002: SHAFT. LOOSE. (CAN) CARBURETOR RUNNING LEAN AT ALTITUDE, THROTTLE SHAFT LOOSE, ENGINE RUNS POORLY WITH THIS CARBURETOR. TIME SINCE FACTORY OVERHAUL IS 542.1 HOURS. - [SDR 2002FA0001226](https://openairdocs.org/sdr/2002FA0001226), Oct 2, 2002: STARTER. INOPERATIVE. STARTER DOES NOT ALLOW THE STARTER ADAPTER TO DISENGAGE WHEN THE ENGINE STARTS. THE RESULT IS EXCESSIVE HEAT AND WEAR WHICH RAPIDLY DESTROYS THE EFFECTIVENESS O - [SDR CA020430003](https://openairdocs.org/sdr/CA020430003), Apr 10, 2002: RIB. FAILED. (CAN) RT WING STA 172.00 - DURING INSTALATION OF AUXILIARY WING TANKS, AN INSPECTION ACCESS HOLE WAS CUT IN LOWER RING SKIN AT STA. 169.00 SURVEILLANCE INSPECTO - [SDR CA020213011](https://openairdocs.org/sdr/CA020213011), Feb 1, 2002: SUPPORT. CRACKED. (CAN) RT OUTBOARD LANDING GEAR SUPPORT CASTING FOUND TO BE CRACKED IN TWO PLACES. FAULT WAS DISCOVERED WHEN GEAR LEG WAS REMOVED FOR NDT OF LANDING GEAR COMPONE - [SDR 2002FA0001052](https://openairdocs.org/sdr/2002FA0001052), Dec 3, 2001: RHEOSTAT. SHORTED. FLYING LOW THROUGH A MOUNTAIN PASS TRIED TO TURN ON INSTRUMENTS LIGHTS. SMOKE IN CABIN. TURNED OFF MASTER. FOUND RESISTOR WINDINGS FAILED. CONTACT ARM BURNED TH - [SDR 2002FA0000443](https://openairdocs.org/sdr/2002FA0000443), Dec 3, 2001: RHEOSTAT. SHORTED. FLYING LOW THRU MOUNTAIN PASS, TRIED TO TURN ON INSTRUMENT LIGHTS. MUCH SMOKE IN CABIN, TURNED OFF MASTER. FOUND RESISTOR WINDINGS FAILED, CONTACT ARM BURNED TH - [SDR 2001FA0000646](https://openairdocs.org/sdr/2001FA0000646), Oct 25, 2001: VALVE. WORN. CYLINDER REMOVED DUE TO LOW COMPRESSION. VALVE STEM WORN TO 0.005. - [SDR 20010418CW005](https://openairdocs.org/sdr/20010418CW005), Apr 18, 2001: GYRO. MISINSTALLED. THE DIRECTIONAL GYRO WAS POWERED BY A WIRE OF THREE SIZES NR 12, NR 16 AND NR 18, SPLICED TOGETHER OVER A LENGTH OF 20 INCHES, THE LARGE END WAS BENT INTO A HOO - [SDR 20010418CW004](https://openairdocs.org/sdr/20010418CW004), Apr 18, 2001: WIRE. DAMAGED. THE BATTERY CABLE WAS BARE IN MANY PLACES INCLUDING THE PENETRATION OF THE FIREWALL. IT HAD ALSO BEEN PENETRATED BY A SCREW THROUGH THE BELLY OF AIRCRAFT, JUST - [SDR 20010418CW003](https://openairdocs.org/sdr/20010418CW003), Apr 18, 2001: HEAT SHIELD. MISSING. THE ENGINE MOUNT HEAT SHIELDS HAD BEEN REMOVED AT SOME POINT ALLOWING HEAT DAMAGE REQUIRING 3 WELD REPAIRS. - [SDR 20010418CW002](https://openairdocs.org/sdr/20010418CW002), Apr 18, 2001: FASTENER. LOOSE. OWNER REPORTED 2 LOOSE RIVETS AT THE FIREWALL ATTACH POINT STA. 5. INVESTIGATION REVEALED 2 MISSING RIVET HEADS AN426AD4 AND A FURTHER 25 RIVET HEADS HELD ON BY - [SDR 20010418CW001](https://openairdocs.org/sdr/20010418CW001), Apr 18, 2001: GYRO. INOPERATIVE. DURING ROUTINE ANNUAL INSPECTION THE ELEVATOR WAS FOUND TO TRAVEL ONLY 19 DEGREE UP. THE TYPE CERTIFICATE CALLS FOR 25 DEGREE. INVESTIGATION FOUND THE D. G. MOU - [SDR 20010420CW007](https://openairdocs.org/sdr/20010420CW007), Apr 2, 2001: O-RING. LEAKING. THE QUICK DRAIN ORING THAT CAME WITH THE NEW QUICK DRAIN, SWELLED UP SO THAT IT IS PUSHED OUT OF THE GROOVE. OIL LEAKS PASSED IT EASILY. - [SDR 20000829SH009](https://openairdocs.org/sdr/20000829SH009), Jul 15, 2000: GEAR. FAILED. DURING TAXI, LANDING GEAR SPRING FAILED AT MATING AREA OF P/N 0541121-2 SUPPORT. CAUSED SUBSTANTIAL DAMAGE TO RIGHT CABIN AFT OF CREW DOOR, RIGHT SIDE OF HORIZO - [SDR 20000712SH033](https://openairdocs.org/sdr/20000712SH033), Jun 21, 2000: COOLER. LEAKING. PART HAD BEEN REPAIRED USING EPOXY TO STOP A LEAK. DURING NORMAL SERVICE, EPOXY FAILED CAUSING THE OIL COOLER TO LEAK AT POINT OF ORIGINAL REPAIR. SUBMITTER REC - [SDR AU000567](https://openairdocs.org/sdr/AU000567), Jun 12, 2000: FITTING. CORRODED. (AUS) LEFT ABD RIGHT WING ATTACHMENT BLOCKS CONTAIN EXFOLIATION CORROSION. - [SDR 99ZZZX3620](https://openairdocs.org/sdr/99ZZZX3620), Aug 30, 1999: SUPPORT. CRACKED. BATTERY BOX SUPPORT ANGLES WERE FOUND CRACKED DURING ANNUAL INSPECTION. - [SDR 20000714SH013](https://openairdocs.org/sdr/20000714SH013), Aug 11, 1999: SPRING. BROKEN. AIRCRAFT TT 7,577 HOURS. RIGHT SIDE MAIN SPRING LANDING GEAR BROKE ON LANDING. SPRING LANDING GEAR BROKE APPROXIMATELY 3 INCHES FROM FUSELAGE ON A LINE THROUGH - [SDR 99ZZZX2616](https://openairdocs.org/sdr/99ZZZX2616), Jun 30, 1999: OIL COOLER. LEAKING. PART WS REPAIRED USING EPOXY. EPOXY FAILED DURING NORMAL SERVICE ALLOWING PART TO LEAK AT POINT OF ORIGINAL REPAIR. EPOXY FAILURE IS COMMON. SUBMITTER RECOMMEND - [SDR 99ZZZX2508](https://openairdocs.org/sdr/99ZZZX2508), Jun 14, 1999: HUB. CORRODED. SUBMITTER STATED PART SHOULD HAVE BEEN REJECTED AT OVERHAUL FOR CORROSION CAUSING METAL TO FLAKE OFF THE EXTERIOR HUB SERVICES. - [SDR AU980474](https://openairdocs.org/sdr/AU980474), Apr 21, 1998: SCREW. DISLODGED. (AUS) RT CONTROL COLUMN SCREW P/N NAS22014 WAS FOUND ADRIFT ALONG WITH GLIDE P/N 0760651-2 AND PLUG P/N 0760681-1. THE LT CONTROL COLUMN WAS CHECKED AND ITS SCR - [SDR 98ZZZX893](https://openairdocs.org/sdr/98ZZZX893), Nov 15, 1997: GEAR SUPPORT. CRACKED. BOTH LANDING GEAR OUTBOARD SUPPORT CASTINGS FOUND CRACKED AT ANNUAL INSPECTION. AIRCRAFT CARRY 5 PERSONS (PER STC) DURING SKYDIVING OPERATIONS. NO RECORD OF PRE - [SDR 98ZZZX892](https://openairdocs.org/sdr/98ZZZX892), Nov 15, 1997: GEAR SUPPORT. CRACKED. BOTH LANDING GEAR OUTBOARD SUPPORT CASTINGS FOUND CRACKED AT ANNUAL INSPECTION. AIRCRAFT CARRY 5 PERSONS (PER STC) DURING SKYDIVING OPERATIONS. NO RECORD OF PRE - [SDR 98ZZZX888](https://openairdocs.org/sdr/98ZZZX888), Nov 15, 1997: GEAR SUPPORT. CRACKED. BOTH LANDING GEAR OUTBOARD SUPPORT CASTINGS FOUND CRACKED DURING ANNUAL INSPECTION. AIRCRAFT CARRIES 5 PERSONS (PER STC) DURING SKYDIVING OPERATIONS. NO RECORD - [SDR 98ZZZX887](https://openairdocs.org/sdr/98ZZZX887), Nov 15, 1997: GEAR SUPPORT. CRACKED. BOTH LANDING GEAR OUTBOARD SUPPORT CASTINGS FOUND CRACKED DURING ANNUAL INSPECTION. AIRCRAFT CARRIES 5 PERSONS (PER STC) DURING SKYDIVING OPERATIONS. NO RECORD - [SDR 97ZZZX4388](https://openairdocs.org/sdr/97ZZZX4388), Jul 15, 1997: BUSHING. BROKEN. PILOT REPORTED VIBRATION AND POWER LOSS. INVESTIGATION FOUND PITCH CHANGE PHENOLIC BUSHING ON ONE BLADE BROKEN ALLOWING BLADE TO MOVE TO LOWER PITCH THAN OTHER - [SDR CA970421092](https://openairdocs.org/sdr/CA970421092), Apr 10, 1997: SUPPORT. CRACKED. (CAN) BOTH MLG CASTING HAD BEEN REPLACED. - [SDR EY2R9601341](https://openairdocs.org/sdr/EY2R9601341), Dec 1, 1996: HUB. CORRODED. CORROSION FOUND ON HUB. All 90: https://openairdocs.org/model/textron-182/reports.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Cessna 182](https://openairdocs.org/model/cessna-182): 446 registered aircraft, registry code 2072702 --- 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.