# Cessna 210R - Type: Aircraft model (FAA registry) - Registry code: 2073458 - Manufacturer (registry): CESSNA - Model: 210R - Aircraft type: Fixed wing single engine - Category: Airplane - Engines: 1 · Reciprocating - Seats: 6 - Weight class: Up to 12,499 lb - Certification: Type certificated - Data sheet: [TCDS 3A21](https://openairdocs.org/tcds/3A21) (OpenAirDocs) - Holder: Textron Aviation Inc. - Registered aircraft: 1 - Page: https://openairdocs.org/model/cessna-210r 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 2023-02-17](https://openairdocs.org/ad/2023-02-17): Fuselage Main, Structure · Textron 210N, 210R, P210N and 8 more. Effective Mar 20, 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 2012-10-04](https://openairdocs.org/ad/2012-10-04): Wings · Cessna 210G, 210H, 210J and 15 more. Effective Jun 5, 2012 - [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 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 2002-26-03](https://openairdocs.org/ad/2002-26-03): Brackett single screen air filter · Cessna 210, 210R, T207A and 21 more. Effective Feb 18, 2003 - [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 98-14-03](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 94-12-08](https://openairdocs.org/ad/94-12-08): Flight Manual Revision · Cessna 210G, 210H, 210J and 15 more. Effective Jul 22, 1994 - [AD 91-22-01](https://openairdocs.org/ad/91-22-01): Electrical Wires · Cessna 210, 210-5 (205), 210-5A (205A) and 14 more. Effective Nov 4, 1991 - [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 86-19-11](https://openairdocs.org/ad/86-19-11): Contaminated Fuel · Cessna 177, 177A, 177B and 83 more. Effective Oct 4, 1986 - [AD 85-23-07](https://openairdocs.org/ad/85-23-07): Autopilot Systems · Aerostar PA-60-700P (Aerostar 700P), 172L, 172P and 37 more. Effective Jan 27, 1986 - [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 79-08-03](https://openairdocs.org/ad/79-08-03): Electrical System · Cessna 120, 140, 140A and 152 more. Effective Jun 6, 1979 - [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 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 69-08-11](https://openairdocs.org/ad/69-08-11): Fuel Boost Pump · Cessna 206, 206H, 210 and 38 more. Effective Apr 22, 1969 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) (11) - [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 CE-17-16](https://openairdocs.org/saib/CE-17-16): Main Landing Gear Actuator Inspection. Issued Jun 9, 2017 - [SAIB CE-13-16](https://openairdocs.org/saib/CE-13-16): Hydraulic Power Pack/Landing Gear System. Issued Feb 8, 2013 - [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-09-42](https://openairdocs.org/saib/CE-09-42): Lights - Landing Light, Beacon Light and Taxi Light Switch Applications. Issued Jul 24, 2009 - [SAIB CE-09-10](https://openairdocs.org/saib/CE-09-10): Availability of Secondary Seat Stops for Pilot and Copilot Seats. Issued Feb 5, 2009 - [SAIB CE-01-41R2](https://openairdocs.org/saib/CE-01-41R2): Flight Controls. Issued Oct 1, 2007 - [SAIB CE-05-27R1](https://openairdocs.org/saib/CE-05-27R1): Stabilizers. Issued Sep 6, 2007 - [SAIB CE-01-41R1](https://openairdocs.org/saib/CE-01-41R1) (historical): Cracks in plastic or non-metallic control wheels. Issued Jan 10, 2007 ## Registered aircraft (1) - [N9057S](https://openairdocs.org/aircraft/N9057S): [Medical Supply X LLC](https://openairdocs.org/faa-owner/MEDICAL%20SUPPLY%20X%20LLC), [Coats, NC](https://openairdocs.org/faa-place/NC/Coats), S/N 21065009 ## STCs approved for it (257, first 50) - [STC SA00061LA](https://openairdocs.org/stc/SA00061LA): Installation of JPI digital tachometer.. J P Instruments - [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 SA00215NY](https://openairdocs.org/stc/SA00215NY): Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system.. CAVU Products Limited - [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 SA00272WI](https://openairdocs.org/stc/SA00272WI): Replacement of hydraulic system pressure switch.. APPH Wichita Inc. - [STC SA00281BO](https://openairdocs.org/stc/SA00281BO): Installation of Avidyne Corporation MLX770 MultiLink Broadcast Transceiver P/N 700-00163-( ), Sensor Systems Inc. Antenna P/N S67-1575-109, or equivalent, and optional Avidyne Mounting Tray P/N 700-00165-000. Avidyne Corporation - [STC SA00290BO](https://openairdocs.org/stc/SA00290BO): Installation of Avidyne Corporation Part Number 700-00167-XXX Multi-Function Display and Mounting Tray Assembly Part Number 700-00168-XXX. Avidyne Corporation - [STC SA00306DE](https://openairdocs.org/stc/SA00306DE): Installation of an external infrared imaging system.. Dart Aerospace USA Inc. - [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 SA00367DE](https://openairdocs.org/stc/SA00367DE): Installation of an Oilamatic Preoiler system.. Oilamatic Inc - [STC SA00368DE](https://openairdocs.org/stc/SA00368DE): Installation of an Aircraft Noise Control System.. Quiet Flight 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 SA00410BO](https://openairdocs.org/stc/SA00410BO): Installation of an AV-30-C Multi-Mode Indicator. uAvionix Corporation - [STC SA00422WI](https://openairdocs.org/stc/SA00422WI): Installation of McCauley Propeller Model D3A34C402/90DFA -8, -10 and associated changes.. Air Plains Services Corporation - [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 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 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 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 SA00796AT](https://openairdocs.org/stc/SA00796AT): Installation of a dual-isolator forward engine mount system. Summit Aviation Inc. - [STC SA00855SE](https://openairdocs.org/stc/SA00855SE): Installation of BAS, Inc. duel belt shoulder harness with inertia reel in accordance with BAS Report 1002, dated April 1, 2000, or later FAA approved revision.. BAS Inc - [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 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 SA01058SE](https://openairdocs.org/stc/SA01058SE): Installation of vortex generators on the wings and tail surfaces of the above model aircraft in accordance with Drawing Package MA2165, Revision IR, dated February 14, 2002, and Installation Manual MA2166, Revision IR, dated February 25, 2002, or later FAA approved revision of either of these documents.. Micro AeroDynamics Inc - [STC SA01077SE](https://openairdocs.org/stc/SA01077SE): Installation of fluoropolymer film.. Columbia Pacific Airlines - [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 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 SA01120SE](https://openairdocs.org/stc/SA01120SE): Installation of Door Steward.. Mountain View Aviation LLC - [STC SA01134DE](https://openairdocs.org/stc/SA01134DE): Installation of EarthX ETX680-24-TSO Lithium Battery. EarthX Inc. - [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 SA01194NY](https://openairdocs.org/stc/SA01194NY): Installation of a Freon-Type electric motor driven Air Conditioning System. Griggs Aircraft Refinishing LLC All 257: https://openairdocs.org/model/cessna-210r/stcs.md ## NTSB investigations (1) 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 DFW08FA061](https://openairdocs.org/ntsb/DFW08FA061), Feb 5, 2008: Cessna 210 (N968CC), Baytown, TX, destroyed, 1 fatal. Probable cause: The pilot's failure to maintain aircraft control after flying into clouds. ## FAA accident and incident reports (2) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Accident 20080204010019A](https://openairdocs.org/incident/20080204010019A), Feb 4, 2008: Cessna 210R (N968CC), Baytown, TX, Destroyed, 1 fatal. (-23) The witness (pilot a) stated that it was extremely foggy and that visibility was less than 1/10 of a mile just before dark. He heard an aircraft fly over… - [Incident 19920226038559I](https://openairdocs.org/incident/19920226038559I), Feb 26, 1992: Cessna 210 (N962CC), Rapid City, MI, Minor damage. Pilot made a forced landing in farm field. Cause of forced landing not stated. Minor damage to propeller on landing ## Service difficulty reports (34) As reported by operators and repair stations, by the model named in the report. - [SDR CA130724006](https://openairdocs.org/sdr/CA130724006), Jul 23, 2013: HOSE. WORN. (CAN) DURING INSPECTION, FOUND ONE OF THE OIL COOLER HOSE RUBBING ON THE RT MUFFLER. HOSE WAS REMOVED AND HAD CHAFED DOWN TO THE METAL BRAIDING. NO LEAKS, NEW H - [SDR CA130522008](https://openairdocs.org/sdr/CA130522008), May 14, 2013: PULLEY. LOOSE. (CAN) DURING TAXI A SQUEEL WAS HEARD FROM THE ENGINE. AFTER SHUTDOWN PILOT OBSERVED THAT PULLY WAS LOOSE ON FRONT ALTERNATOR, 2. THE PULLY HAD BEEN RUBBING ON A - [SDR CA120425001](https://openairdocs.org/sdr/CA120425001), Apr 24, 2012: PISTON. LEAKING. (CAN) ACFT RETURNED AFTER FLIGHT WITH ENGINE OIL SPATTERED ON WINDSCREEN. REMOVED PROPELLER DOME TO DISCOVER ENGINE OIL ON FRONT OF PROPELLOR HUB. PROP SHOP SAY - [SDR CA110620007](https://openairdocs.org/sdr/CA110620007), Jun 20, 2011: GASKET. BROKEN. PILOT REPORTED THAT HE HAD SOME OIL ON RT PART OF WINDSHIELD. DISCOVERED THAT THE OIL COOLER ADAPTER GASKET ON RT FWD OF ENGINE HAD A HAIR LINE OPENING OR SPLIT - [SDR CA090430001](https://openairdocs.org/sdr/CA090430001), Apr 16, 2009: MOTOR. OVERHEATED. (CAN) DURING CRUISE ALTERNATOR NR 1 WENT "OFF LINE", IMMEDIATELY NR 2 WENT OFF AS WELL. LARGE ELEC PWR DRAW ON AMMETER NOTICED, STRONG ODOR & SMOKE NOTED FROM L - [SDR CA080710004](https://openairdocs.org/sdr/CA080710004), Jul 9, 2008: MOUNT. DEFORMED. (CAN) DURING ENGINE INSPECTION NOTED THAT THE LT AND RT FORWARD ENGINE MOUNTS WERE SAGGING TO THE POINT THAT DURING TAKEOFF POWER ON ENGINE AND INTAKE PIPE HOSE - [SDR CA080229004](https://openairdocs.org/sdr/CA080229004), Feb 28, 2008: PULLEY. SEPARATED. (CAN) WHILE IN FLIGHT, NR1 ALTERNATOR FAILED, NR1 ALT AMBER LIGHT CAME ON, ON THE GROUND, INSP REVEALED THAT THE DRIVE PULLEY HAD SEPARATED FROM ALTERNATOR, PUL - [SDR CA070607002](https://openairdocs.org/sdr/CA070607002), Jun 6, 2007: RETAINING NUT. MISSING. (CAN) PILOT HAD CALLED AND REPORTED THAT THE ALTERNATOR THAT WE HAD REPLACED THE NIGHT BEFORE HAD GONE OFFLINE .7 HRS AND A SLIGHT ODOR OF BURNING RUBBER NOTED - [SDR CA051115002](https://openairdocs.org/sdr/CA051115002), Nov 7, 2005: CLUTCH. BROKEN. (CAN) WHILE ATTEMPTING FIRST START OF DAY, PROP ROTATED THEN STOPPED. ON SUBSEQUENT ATTEMPTS THE PROPELLOR FAILED TO ROTATE. IT WAS DETERMINED THAT THE STARTER - [SDR CA050906001](https://openairdocs.org/sdr/CA050906001), Aug 31, 2005: SHAFT. SHEARED. (CAN) DURING ROUTINE MAINTENANCE, SHAFT LOCATION CUTOUT OF RT PUMP HAD AN ODD LOOK TO IT. TURNING PROPELLOR BY HAND VERIFIED SUSPICION, SHAFT WAS SHEARED. PUMP - [SDR AU510002145](https://openairdocs.org/sdr/AU510002145), Mar 11, 2005: IMPULSE COUPLING. DAMAGED. MAGNETO IMPULSE COUPLING CAM FLYWEIGHT TIP BROKEN OFF. RETURN SPRING MISSING FROM UNDER FLYWEIGHT. FOUND DURING INSPECTION IAW AD/ELECT/75. - [SDR CA060301001](https://openairdocs.org/sdr/CA060301001), Feb 25, 2005: CONTACTOR. ARCED. DURING TAXI TO POSITION, PILOT HEARD UNUSUAL STATIC ON HEADSET AND A LARGER THAN NORMAL AMPS DRAW. RETURNED TO CHOCKS; WHILE STILL RUNNING CHECKED SYSTEM AND SU - [SDR AUS20040326](https://openairdocs.org/sdr/AUS20040326), Apr 5, 2004: WEB. CRACKED. (AUS) TAILPLANE ATTACHMENT WEB CRACKED. - [SDR AUS20040168](https://openairdocs.org/sdr/AUS20040168), Mar 9, 2004: TUNNEL WALL. CRACKED. (AUS) RT SIDE NOSE LANDING GEAR TUNNEL WALL CRACKED IN AREA NEAR RT NOSE LANDING GEAR TORQUE TUBE STIFFENER PN 1213801-2. FURTHER INVESTIGATION OF THE STRUCTURE - [SDR CA030317004](https://openairdocs.org/sdr/CA030317004), Mar 13, 2003: MOTOR. WORN. (CAN) PILOT REPORTED DURING CRUISE A ODOUR AND NOISE IN COCKPIT. A SLIGHT AMOUNT OF SMOKE WAS NOTICED IN WINDSHIELD AREA. PILOT PULLED CIRCUIT BREAKER FOR AVION - [SDR AUS20030015](https://openairdocs.org/sdr/AUS20030015), Jan 4, 2003: CABLE. FAILED. (AUS) AIRCRAFT EXPERIENCED AN UNCOMMANDED INCREASE IN PROPELLER RPM AND FAILED TO RESPOND TO FURTHER COMMANDS. INVESTIGATION FOUND THAT THE STAINLESS STEEL SHAF - [SDR AUS20020355](https://openairdocs.org/sdr/AUS20020355), Apr 17, 2002: PISTON. DAMAGED. (AUS) MAIN LANDING GEAR ACTUATOR PISTON AND GEAR TEETH DAMAGED. FOUND DURING INSPECTION IAW SEB 01-2 REV1. SUSPECT DAMAGE OCCURRED DURING A PREVIOUS ACCIDENT. - [SDR CA011220001](https://openairdocs.org/sdr/CA011220001), Dec 19, 2001: NUT. LEAKING. (CAN) DURING ROUTINE GROUND MAINTENCE OIL WAS DISCOVERED EMINATING FROM THE ENGINE COWLING. INVESTIGATION WHICH INCLUDED WASHING DOWN THE AREA AND A RUN UP REVE - [SDR AUS20010721](https://openairdocs.org/sdr/AUS20010721), Jul 2, 2001: HOSE. DETERIORATED. (AUS) INSTRUMENT VACUUM HOSES LOCATED BEHIND THE INSTRUMENT PANEL DETERIORATED. HOSES ARE BRANDED IMPERIAL EASTMAN REDI-SEAL. - [SDR CA010530004](https://openairdocs.org/sdr/CA010530004), May 3, 2001: BRUSHES. WORN. (CAN) PILOT REPORTED HE HAD TO MAKE A FLAPLESS LANDING AS FLAPS WOULD NOT LOWER TO SELECTED POSITION ON APPROACH. NO MOVEMENT OF FLAPS NOTED BY VISUAL CHECK. IN - [SDR CA010508006](https://openairdocs.org/sdr/CA010508006), Apr 20, 2001: ALTERNATOR. FAILED. (CAN) PILOT REPORTED 1 ALTERNATOR OFF LINE LIGHT CAME ON IN FLIGHT. FURTHER INVESTIGATION WHEN AIRCRAFT RETURNED TO BASE, REVEALED THAT THE PULLY/FAN AND RETAIN - [SDR 99ZZZX3168](https://openairdocs.org/sdr/99ZZZX3168), Aug 10, 1999: CYLINDER. WORN. DURING A ROUTINE 100-HOUR COMPRESSION TEST, EXCESSIVE LEAKAGE WAS NOTED GOING PAST THE EXHAUST VALVE. THE EXHAUST VALVE, EXHAUST VALVE GUIDE FOUND TO BE WORN OU - [SDR 99ZZZX2722](https://openairdocs.org/sdr/99ZZZX2722), May 20, 1999: CYLINDER. WORN. DURING A ROUTINE 50-HOUR OIL CHANGE COMPRESSION CHECK, EXCESSIVE LEAKAGE WAS FOUND LEAKING PAST THE INTAKE AND EXHAUST VALVE ON THE NR 1 CYLINDER. THE CYLINDER - [SDR CA980922006](https://openairdocs.org/sdr/CA980922006), Aug 11, 1998: MAGNETO. FAILED. (CAN) AFTER LANDING A MAGNETO CHECK FOUND THE LEFT HAND MAGNETO DEAD. THE MAGNETO WAS REPLACED. THE CAUSE OF THE FAULT WAS NOT DETERMINED. - [SDR 98ZZZX4520](https://openairdocs.org/sdr/98ZZZX4520), Apr 16, 1998: STARTER ADAPTER. WORN. THE ENGINE WOULD NOT CRANK OVER. INVESTIGATION REVEALED THE STARTER MOTOR WAS TURNING. INSPECTION OF THE STARTER ADAPTER, INTERNALLY, INDICATES EXCESSIVE CLEARA - [SDR 98ZZZX4519](https://openairdocs.org/sdr/98ZZZX4519), Feb 16, 1998: FCU. WORN. FUEL PRESSURES ARE UNSTABLE AND FLUCTUATING. THE ENGINE DRIVEN FUEL PUMP AND FUEL CONTROLLER ARE REPLACED AND THE PROBLEM SOLVED. SUBMITTER SUGGESTED POSSIBLE C - [SDR 98ZZZX4518](https://openairdocs.org/sdr/98ZZZX4518), Feb 16, 1998: PUMP. WORN. FUEL PRESSURES ARE UNSTABLE AND FLUCTUATING. THE ENGINE DRIVEN FUEL PUMP AND FUEL CONTROLLER ARE REPLACED AND THE PROBLEM SOLVED. SUBMITTER SUGGESTED POSSIBLE C - [SDR 97ZZZX1233](https://openairdocs.org/sdr/97ZZZX1233), Mar 6, 1997: CYLINDER. CRACKED. WHILE PERFORMING TCM SB 96-12, CONTINUED AIRWORTHINESS INSTRUCTIONS FOR TCM CYLINDERS, BUBBLES WERE FOUND ACCUMULATING AROUND THE NR 2 CYLINDER UPPER SPARK PLUG - [SDR 97ZZZX1232](https://openairdocs.org/sdr/97ZZZX1232), Mar 6, 1997: CYLINDER. CRACKED. NR 3 CYLINDER WAS REMOVED DUE TO LOW COMPRESSION. THE CYLINDER WAS SENT FOR INSPECTION. THE CYLINDER INSPECTION REVEALED A CRACK WHICH BEGAN AT THE SPARK PLUG H - [SDR 98ZZZX4459](https://openairdocs.org/sdr/98ZZZX4459), Feb 17, 1997: VALVE GUIDE. CRACKED. A ROUTINE COMPRESSION CHECK INDICATES LEAKAGE ON THE NR 2 CYLINDER. FURTHER INVESTIGATION REVEALS A CRACK ON THE CYLINDER HEAD THAT EXTENDS FROM THE FUEL INJECT - [SDR CA961203013](https://openairdocs.org/sdr/CA961203013), Nov 21, 1996: RESERVOIR TANK. LEAKING. (CAN) FUEL RESERVOIR TANK FOUND SEEPING FUEL FROM THE FORWARD TOP SEAM WELD. NO CRACK VISIBLE. TANK HAD BEEN PREVIOUSLY REPAIRED AT 3197 HOURS. - [SDR CA960515009](https://openairdocs.org/sdr/CA960515009), May 6, 1996: TIE BOLT. BROKEN. (CAN) ALTERNATOR CASE TIE BOLT BROKEN IN THREADED AREA, 1/2 INCH FROM THE END OF THE BOLT. THIS IS THE 3RD SIMILAR OCCURRENCE ON THIS AIRCRAFT. PREVIOUS CASES W - [SDR CA960507012](https://openairdocs.org/sdr/CA960507012), May 1, 1996: MOTOR. OVERHEATED. (CAN) CREW REPORTED BURNT SMELL AND UNDERCARRIAGE CIRCUIT BREAKER POPPED. GEAR LOWERED BY HAND PUMP. HYDRAULIC POWERPACK MOTOR RUNNING SLOW AND OVERHEATING. MOT - [SDR CA960202015](https://openairdocs.org/sdr/CA960202015), Jan 26, 1996: TIE BOLT. BROKEN. (CAN)PILOT REPORTED AN INCREASING WHINING OVER THE HEADSET FOLLOWED BY THE #2 ALTERNATOR LIGHT ILLUMINATING. #2 ALTERNATOR SHUT DOWN AND THE AIRCRAFT FINISHED F --- 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.