# Service difficulty reports: Cessna T182T

A list on [Cessna T182T](https://openairdocs.org/model/cessna-t182t.md).

Newest first. General aviation reporting is voluntary.

- [SDR 2025FA0000198](https://openairdocs.org/sdr/2025FA0000198.md): Actuator · faulted · Mar 21, 2025 · N65927 · Cessna T182T · Elevator Tab Control System
  > PILOT REPORTED: WHILE ON DESCENT INTO KPWG I DISCONNECTED THE AUTOPILOT AT 500 FT AGL. I WENT TO MAKE A MANUAL ADJUST OF THE TRIM USING THE HAND TRIM WHEEL AND FOUND IT DIFFICULT TO MOVE. I ALSO ATTEMPTED TO USE THE ELECTRIC TRIM BUT FOUND IT TO BE INEFFECTIVE
- [SDR 2024FA0000740](https://openairdocs.org/sdr/2024FA0000740.md): Intake Pipe · loose · Sep 26, 2024 · N2155J · Cessna T182T · Reciprocating Engine Cylinder Section
  > MY SHOP HAS SEEN TWO OF THESE ISSUES IN A VERY SHORT TIME ON TWO DIFFERENT AIRCRAFT. THE FIRST WAS THE LISTED AIRCRAFT (N2155J), THE SECOND IS ON N406CV. SAME ENGINES (TIO-540-AK1A) WITH APPROXIMATELY THE SAME TIME SINCE OVERHAUL (1200 HOURS) FROM TWO DIFFEREN
- [SDR 2023FA0000017](https://openairdocs.org/sdr/2023FA0000017.md): Tube · punctured · Dec 18, 2022 · N1552S · Cessna T182T · Tire Tube
  > ON DEC 18 I WAS NOTIFIED BY THE OWNER THAT HE HAD EXPERIENCED AND FLAT NOSE LANDING GEAR TIRE AFTER LANDING. HE REPORTED TO ME THE TIRE WAS FLAT WHILE WHEN WE WAS TAXIING HE AIRCRAFT BACK TO THE HANGAR. I REMOVED THE NOSE LANDING GEAR WHEEL ASSEMBLY AND INSPE
- [SDR 2019FA0000107](https://openairdocs.org/sdr/2019FA0000107.md): Tailpipe · cracked · Apr 5, 2019 · N723D · Cessna T182T · Engine Collector/Tailpipe/Nozzle
  > OWNER STATED TAIL PIPE CLAMP WAS REPLACED AT ANNUAL INSPECTION 5-25-18 AS WELL AS 3 OTHER CLAMPS ON THE WASTE GATE AND EXHAUST. OWNER FOUND ON PREFLIGHT THAT THE TAIL PIPE WAS LOOSE. UPON FURTHER INSPECTION AT THE MAINTENANCE SHOP FOUND TAIL PIPE CLAMP TO BE I
- [SDR 2018FA0000337](https://openairdocs.org/sdr/2018FA0000337.md): Cylinder Head · bypassing · Aug 9, 2018 · N92VB · Cessna T182T · Reciprocating Engine Cylinder Section
  > PILOT REPORTED NO START CONDITION AFTER 2 HOUR FLIGHT. COMPRESSION CHECK COMPLETED AND FOUND CYLINDER NR 1, 72, ALL OTHER CYLINDERS BELOW 16 PSI, WITH CYLINDERS 4 & 5 AT 0. BORESCOPE FOUND EXHAUST VALVES STUCK OPEN ON CYLINDERS 4 & 5. ALL OTHER PERIMETERS NOR
- [SDR BQVD2018081300001](https://openairdocs.org/sdr/BQVD2018081300001.md): Flex Hose · disintegrated · Aug 9, 2018 · N4839T · Cessna T182T · Aircraft Fuel System
  > ON RAMP, AFTER FLIGHT, PILOT NOTICED A PUDDLE OF FUEL UNDER THE ENGINE COWL. FOUND THE ENGINE DRIVEN FUEL PUMP SEAL WAS LEAKING. THE LEAKING FUEL PUMP PROBLEM WAS COMPOUNDING WITH ANOTHER SERIOUS PROBLEM. MAINTENANCE DISCOVERED THE DRAIN HOSE MATERIAL IS NOT
- [SDR 2018FA0000417](https://openairdocs.org/sdr/2018FA0000417.md): Cylinder Head · bypassing · Jun 25, 2018 · N92VB · Cessna T182T · Reciprocating Engine Cylinder Section
  > ENGINE EXTREMELY HARD TO START AND KEEP RUNNING SMOOTHLY. FLEW TO KPNE WITHOUT INCIDENT. ENGINE PERFORMED WITHIN PARAMETERS. DELIVERED AIRPLANE TO MAINTENANCE AND STARTING PROBLEM DIAGNOSIS. MECHANIC DETERMINED 5 OUT OF THE 6 CYLINDERS HAD VERY LOW COMPRESSION
- [SDR 2018FA0000416](https://openairdocs.org/sdr/2018FA0000416.md): Cylinder Head · bypassing · Jun 25, 2018 · N92VB · Cessna T182T · Reciprocating Engine Cylinder Section
  > ENGINE EXTREMELY HARD TO START AND KEEP RUNNING SMOOTHLY. FLEW TO KPNE WITHOUT INCIDENT. ENGINE PERFORMED WITHIN PARAMETERS. DELIVERED AIRPLANE TO MAINTENANCE AND STARTING PROBLEM DIAGNOSIS. MECHANIC DETERMINED 5 OUT OF THE 6 CYLINDERS HAD VERY LOW COMPRESSION
- [SDR 2018FA0000415](https://openairdocs.org/sdr/2018FA0000415.md): Cylinder Head · bypassing · Jun 25, 2018 · N92VB · Cessna T182T · Reciprocating Engine Cylinder Section
  > ENGINE EXTREMELY HARD TO START AND KEEP RUNNING SMOOTHLY. FLEW TO KPNE WITHOUT INCIDENT. ENGINE PERFORMED WITHIN PARAMETERS. DELIVERED AIRPLANE TO MAINTENANCE AND STARTING PROBLEM DIAGNOSIS. MECHANIC DETERMINED 5 OUT OF THE 6 CYLINDERS HAD VERY LOW COMPRESSION
- [SDR CA180510005](https://openairdocs.org/sdr/CA180510005.md): Bearing · out of adjust · May 10, 2018 · Cessna T182T · Engine (Reciprocating)
  > (CAN) BEARING ALIGNMENT HOLES INCORRECTLY INDEXED RESULTING IN MISALIGNED BEARING HALVES. (TC# 20180510005)
- [SDR 2017FA0000360](https://openairdocs.org/sdr/2017FA0000360.md): Exhaust Pipe · cracked · Aug 19, 2017 · N915CR · Cessna T182T · Engine Collector/Tailpipe/Nozzle
  > DURING ANNUAL INSPECTION, OVERBOARD EXHAUST PIPE WAS DISCOVERED CRACKED AND LEAKING AT THE WASTE GATE ATTACH FLANGE.
- [SDR 2016FA0000591](https://openairdocs.org/sdr/2016FA0000591.md): Pushrod · scored · Dec 6, 2016 · N102BR · Cessna T182T · Reciprocating Engine Cylinder Section
  > PUSHRODS INSPECTED PER SA-167A AND 6 PUSHRODS SHOW SIGNS OF SCORING.
- [SDR 2016FA0000268](https://openairdocs.org/sdr/2016FA0000268.md): Spline · sheared · Jan 6, 2016 · N941T · Cessna T182T · Engine Fuel Pump
  > SHAFT SHEARED ON TAKEOFF. PUMP SEIZED. DRIVE SHAFT SPLINE SHEARED.
- [SDR 2015FA0000264](https://openairdocs.org/sdr/2015FA0000264.md): Exhaust Stack · cracked · Jun 9, 2015 · N621D · Cessna T182T · Engine Collector/Tailpipe/Nozzle
  > DURING AN OIL CHANGE THE TECH WAS DOING A VISUAL INSPECTION OF THE ENGINE AND NOTICED SOME EXHAUST SOOT/STAINING ON THE HEAT SHIELD FOR THE J BOX. DISCOVERED THE SOURCE TO BE THE CRACKED EXHAUST ELBOW.
- [SDR CA141117005](https://openairdocs.org/sdr/CA141117005.md): Breather · cracked · Nov 13, 2014 · Cessna T182T · Reciprocating Engine Oil System
  > (CAN) THE OIL BREATHER/SEPARATOR TAKES BLOWBY GASES FROM THE ENGINE CRANKCASE AND CENTRIFUGALLY SEPARATES OIL MISTS FROM THEM BEFORE DUMPING THE GASES OVERBOARD THROUGH THE BREATHER TUBE. OIL IS RETURNED TO THE ENGINE SUMP. OIL WAS NOTED SEEPING FROM A CRACK
- [SDR LC1R20140613001](https://openairdocs.org/sdr/LC1R20140613001.md): Wastegate Valve · eroded · Jun 13, 2014 · N875DE · Cessna T182T · Exhaust Turbocharger
  > TROUBLE SHOT A LOW MANIFOLD PRESS PROBLEM, FOUND WASTE GATE BUTTERFLY OVER 80% ERODED AWAY. THERE WAS NO OTHER DAMAGE TO THE INDUCTION SYS OR TO THE TURBOCHARGER.
- [SDR CA140516002](https://openairdocs.org/sdr/CA140516002.md): Bolt · interference · May 13, 2014 · Cessna T182T · Aileron Control System
  > (CAN) BALANCE CABLE TO LT AILERON BELLCRANK ATTACH BOLT FOUND TO BE INTERFERING WITH AILERON PUSHROD AT FULL TRAVEL.
- [SDR 2014FA0000111](https://openairdocs.org/sdr/2014FA0000111.md): Screw · loose · Mar 7, 2014 · N5918G · Cessna T182T · Control Column Section
  > COMPLIED WITH SB SEB-27-01. SEVERAL DAYS LATER, ACFT WAS FLOWN AND THE ELEVATOR CONTROL BECAME INCREASINGLY STIFF DURING THE FLIGHT TO THE POINT OF LOCKING UP. THE ACFT RETURNED AIRPORT AND MADE AN UNEVENTFUL LANDING. DURING INSPECTION, TENSION WAS RESET ON
- [SDR YWYR201209159368](https://openairdocs.org/sdr/YWYR201209159368.md): Master Switch · damaged · Sep 7, 2012 · N931JP · Cessna T182T · AC Power Distribution System
  > PILOT REPORTED THAT ACFT MASTER SWITCH WOULD NOT ACTUATE ACFT POWER ON SEVERAL OCCASIONS. IF THE MASTER SWITCH WAS CYCLED ON AND OFF SEVERAL TIMES IT WOULD EVENTUALLY TURN ACFT POWER ON. NEW MASTER SWITCH INSTALLED AND OPERATION WAS NORMAL.
- [SDR 2012FA0000542](https://openairdocs.org/sdr/2012FA0000542.md): Bracket · missing · Jul 26, 2012 · N6046R · Cessna T182T · Fuselage Main, Attach Fittings
  > DURING A SCHEDULED INSPECTION, IT WAS NOTED THAT THE RIVETS ATTACHING HORIZONTAL STABILIZER LT AND RT ATTACH BRACKETS TO THE TAILCONE BULKHEAD WERE NOT INSTALLED. FURTHER INSPECTION REVEALED THAT THE BRACKET CLIPS HAD PILOT HOLES BUT WERE NOT DRILLED TO MATC
- [SDR CA120509009](https://openairdocs.org/sdr/CA120509009.md): Bulkhead · dented · Apr 20, 2012 · Cessna T182T · Fuselage Main, Bulkhead
  > (CAN) ACFT WAS OPEN FOR INSPECTION. NOTICED THAT BULKHEAD WAS DENTED. ALSO FOUND OUT THAT DEALER HAS NOTED THAT THIS IS A COMMON PROBLEM IN MANY OF THE NEWER MODEL. THIS DAMAGE IS NOT NEGLIGABLE IAW SRM. SUGGEST THAT MFR IS CONTACTED TO MODIFY THE SRM TO ALLO
- [SDR YN8R2012041013834](https://openairdocs.org/sdr/YN8R2012041013834.md): Hose · leaking · Apr 10, 2012 · N82YA · Cessna T182T · Engine Fuel Distribution
  > ON COMPLIANCE WITH SB 599, FUEL PUMP REPLACEMENT, IT WAS DISCOVERED THAT THE ENGINE DRIVEN FUEL PUMP INLET HOSE HAD INDICATIONS OF OUTER FIRESLEEVE DETERIORATION AND BULGING INDICATIVE OF THE FUEL HOSE LEAKING FUEL FROM CRIMPED AREA OF FITTING/HOSE. REPLACED
- [SDR CA120316003](https://openairdocs.org/sdr/CA120316003.md): Bulkhead · dented · Mar 15, 2012 · Cessna T182T · Fuselage Main, Bulkhead
  > (CAN) DURING IMPORT INTO CANADA NOTICED FS 207 BULKHEAD DAMAGE. LOWER PORTION OF BULKHEAD HAS 3 SMALL DENTS. DAMAGE APPEARS TO HAVE OCCURRED DURING THE MFG PROCESS. THERE IS EVIDENCE OF RUB MARKS ON THE PEAKS OF THE DENTS PRESUMABLY CAUSED BY A BUCKING BAR.
- [SDR ESMR2012022801](https://openairdocs.org/sdr/ESMR2012022801.md): Pump · leaking · Feb 24, 2012 · N356CS · Cessna T182T · Engine Fuel Pump
  > ACFT WAS INBOUND WHEN THE ENGINE BEGAN TO LOOSE POWER. THE PILOT USED THE FUEL BOOST PUMP TO KEEP THE ENGINE RUNNING AND LANDED WITHOUT INCIDENT. THE ENGINE RAN FINE AT IDLE ON THE GROUND. WITH THE ENGINE OFF AND THE FUEL SELECTOR TURNED ON, FUEL WAS RUNNING
- [SDR TRBA2012013001](https://openairdocs.org/sdr/TRBA2012013001.md): Switch · faulty · Jan 7, 2012 · N525MJ · Cessna T182T · Emergency Lighting
  > THE CREW REPORTED TE EMERGENCY LIGHTS ABOVE THE F/A JUMP SEATS ON AT ALL TIMES. THE ACFT WAS REMOVED FROM SERVICE. REPLACED 2 MIN LIGHT PUSH BUTTON SWITCH NEAR PASSENGER ENTRANCE DOOR, PERFORMED OPS CHECK AND FOUND WORKING PROPERLY IAW MM 20-27-17. THE OPS C
- [SDR CA100805004](https://openairdocs.org/sdr/CA100805004.md): Antenna · failed · May 31, 2010 · Cessna T182T · Global Positioning System
  > WAAS/GPS/COMM COMBINATION ANTENNA NO LONGER ABLE TO RECEIVE GPS SATELLITE INFORMATION. COMM FUNCTIONALITY UNAFFECTED.
- [SDR 2010FA0000232](https://openairdocs.org/sdr/2010FA0000232.md): Circuit Breaker · defective · Mar 17, 2010 · N2252Z · Cessna T182T · Flight Control System Wiring
  > ON GROUND ROLL AFTER LANDING FLAPS STOPPED RETRACTING AT 10 DEGREES. FLUSH TYPE CIRCUT BREAKER DID NOT POP OUT BUT WAS TRIED NUMEROUS TIMES. ALL SWITCHES AND MOTOR CHECKED GOOD. REINVESTIGATING CIRCUT BREAKER, CAUSED CIRCUT BREAKER TO CLICK AND SYSTEM TO RUN
- [SDR 2008FA0000291](https://openairdocs.org/sdr/2008FA0000291.md): Unknown · malfunctioned · Apr 24, 2008 · N488PJ · Cessna T182T · Integrated Flight System
  > WHEN TURNING THE (CRS) COURSE KNOB, THE INNER KNOB (BARO) BAROMETRIC PRESSURE KNOB WOULD TURN ALSO. CHANGING THE ALTITUDE INDICATED.
- [SDR O7TR200800001](https://openairdocs.org/sdr/O7TR200800001.md): Turbocharger · failed · Mar 11, 2008 · Cessna T182T · Exhaust Turbocharger
  > MAJOR TURBO FAILURE DUE TO SEPARATION OF TURBINE WHEEL HEAD FROM SHAFT.
- [SDR 2007FA0000562](https://openairdocs.org/sdr/2007FA0000562.md): Line · cracked · Jun 29, 2007 · N1328N · Cessna T182T · Reciprocating Engine Oil System
  > 30 DEGREE FITTING HAS CRACK ON WRENCH FLAT. (K)
- [SDR 2007FA0000233](https://openairdocs.org/sdr/2007FA0000233.md): Spring · broken · Mar 12, 2007 · N5198G · Cessna T182T · Magneto/Distributor
  > NEW POINTS (PN M3081) WERE INSTALLED IN BOTH MAGNETOS AT THE ANNUAL INSPECTION ON 2/22/07, TT 649.2. ON 3/10/07, TT 658.2, PART TT - 9.0 HOURS, THE PILOT/OWNER PERFORMED MAG CHECK AND THE ENGINE QUIT. A MECHANIC REMOVED THE RT MAG AND FOUND THAT THE SPRING T
- [SDR FAA1012001](https://openairdocs.org/sdr/FAA1012001.md): Fuel · leaking · Oct 7, 2006 · N6004S · Cessna T182T · Aircraft Fuel System
  > AFTER AN APPROXIMATELY 30 MILE UNEVENTFUL FLIGHT WITH A LANDING AND TAXIBACK FOR DEPARTURE AT HVN THE AIRCRAFT WAS CLEARED FOR TAKEOFF BY THE TOWER. THERE WAS A FEW MINUTES OF HOLDING PRIOR TO BEING RELEASED. ON TAKEOFF FROM HVN RWY 2, THE AIRCRAFT FUNCTIONE
- [SDR 2006FA0000944](https://openairdocs.org/sdr/2006FA0000944.md): Relief Valve · failed · Sep 11, 2006 · N182GA · Cessna T182T · Exhaust Turbocharger
  > PILOT REPORTED, ON TAKEOFF ROLL, THE MANIFOLD PRESSURE WENT TO GREATER THAN 40 MP FOR 3 TO 4 SECONDS. THE PILOT WENT BACK TO RUNUP AREA AND CONFIRMED THAT MP COULD GO ABOUT 40 MP, PILOT TAXIED BACK TO RAMP AND GROUNDED AIRCRAFT. TROUBLESHOT TURBO CHARGER SYS
- [SDR 2006FA0000727](https://openairdocs.org/sdr/2006FA0000727.md): Guard · out of rig · Jul 14, 2006 · N1568W · Cessna T182T · Aircraft Fuel System
  > PROTECTIVE GUARDS ARE CALLED OUT BY IPL ORIGINALLY, IPL REV 7 DOES, REV 8 DOES NOT. CURRENT REVISION 12, CALLS FOR THE GUARDS TO BE INSTALLED REV 13 IS IN TRANSIT BUT SHOULD INCLUDE THE CALL OUT. THIS AIRCRAFT HAS INDICATIONS THAT ELEVATOR CONTROL LINES HAVE
- [SDR 2006FA0000089](https://openairdocs.org/sdr/2006FA0000089.md): Fuel Line · worn · Dec 30, 2005 · N542LB · Cessna T182T · Engine Fuel Distribution
  > FOUND FUEL INJECTION LINE RUBBING CYLINDER COOLING FINS. CAUSING WEAR TO THE LINE. IF WORN CAN CAUSE FUEL LEAK ON TO THE TURBO CHARGER. AD WAS IN COMPLIANCE BUT THE CLAMP WAS LOOSE ALLOWING FUEL LINE TO ROTATE. (SW01200603311) (K)
- [SDR 2005FA0000309](https://openairdocs.org/sdr/2005FA0000309.md): Switch · inoperative · Mar 7, 2005 · N66139 · Cessna T182T · Stall Warning System
  > STALL WARNING INOP FOUND STALL WARNING SWITCH TERMINAL SCREW LAYING INSIDE WING, SCREW BACKED OUT IN FLIGHT.
- [SDR 2005FA0000303](https://openairdocs.org/sdr/2005FA0000303.md): Terminal · loose · Mar 7, 2005 · N66139 · Cessna T182T · Stall Warning System
  > STALL WARNING INOP, FOUND STALL WARNING SWITCH TERMINAL SCREW LAYING INSIDE WING, SCREW BACKED OUT IN FLIGHT.
- [SDR 2006FA0000181](https://openairdocs.org/sdr/2006FA0000181.md): Connector · disconnected · Feb 13, 2005 · N36TP · Cessna T182T · Engine Indicating System Wiring
  > PLASTIC CONNECTOR THAT CONNECTS TO TACHOMETER TRANSDUCER HAS NO LOCKING DEVICE, THIS TYPE OF CONNECTOR SHOULD HAVE A SNAP LOCK AT THE END OF IT THREAD TRAVEL. FOUND THIS SAME SIMILAR PROBLEM ON 2 OTHER SINGLE ENGINE AIRCRAFT WITH THE SAME TRANSDUCERE. ALSO H
- [SDR CA041216010](https://openairdocs.org/sdr/CA041216010.md): Wastegate Valve · seized · Dec 14, 2004 · Cessna T182T · Exhaust Turbocharger
  > (CAN) WASTEGATE BUTTERFLY VALVE FOUND SEIZED ON INSPECTION. THIS IS THE SECOND VALVE FOUND SEIZED ON TWO DIFFERENT AIRCRAFT WITH LOW TTSN.
- [SDR 2004FA0000859](https://openairdocs.org/sdr/2004FA0000859.md): Circuit Breaker · misinstalled · Aug 27, 2004 · N5107Y · Cessna T182T · DC Power Distribution System
  > GPS CIRCUIT BREAKER IS PROVIDING POWER TO MULTIPLE UNITS WHICH IS CONTRARY TO AC20-138A. AC20-138 STATES THAT GPS CIRCUIT BREAKER CAN ONLY POWER GPS. REFERENCE ATTACHED DRAWINGS FROM MFG WIRING DIAGRAM MANUAL. PAGES 34-20-00-01 AND 34-52-03-01.
- [SDR CA031217008](https://openairdocs.org/sdr/CA031217008.md): Restraint · inoperative · Dec 9, 2003 · Cessna T182T · Passenger Compartment Equipment
  > (CAN) DURING INSPECTION IT WAS NOTICED THAT BOTH REAR SEAT RESTRAINT SYSTEM INERTIA REELS WOULD INTERMITTENTLY LOCK AND NOT ALLOW BELT TO EXTEND. IT WAS DECIDED THAT IF RESTRAINTS WERE RELEASED IN FLIGHT IT MAY NOT BE POSSIBLE TO REFASTEN THEM SO BOTH UNITS WE
- [SDR 2003FA0001028](https://openairdocs.org/sdr/2003FA0001028.md): Cylinder · wrong part · Sep 30, 2003 · Cessna T182T · Reciprocating Engine Cylinder Section
  > DURING A ANNUAL INSPECTION, FOUND THE NR 1 CYLINDER TO BE INCORRECT FOR THIS INSTALLATION, INCORRECT CYLINDER INSTALLED BY CESSNA OR LYCOMING PRIOR TO INSTALLATION ON AIRCRAFT. CYLINDER WAS FOR SHORT REACH PLUGS, ENGINE USES LONG REACH. CYLINDER FOUND ON 2ND A
- [SDR 2003FA0001027](https://openairdocs.org/sdr/2003FA0001027.md): Cylinder · wrong part · Sep 30, 2003 · Cessna T182T · Reciprocating Engine Cylinder Section
  > DURING A ANNUAL INSPECTION, FOUND THE NR 1 CYLINDER TO BE INCORRECT FOR THIS INSTALLATION, INCORRECT CYLINDER INSTALLED BY MFG PRIOR TO INSTALLATION ON AIRCRAFT. CYLINDER WAS FOR SHORT REACH PLUGS, ENGINE USES LONG REACH. CYLINDER FOUND ON 2ND ANNUAL INSPECTIO
- [SDR 2003FA0001026](https://openairdocs.org/sdr/2003FA0001026.md): Cylinder · wrong part · Sep 30, 2003 · Cessna T182T · Reciprocating Engine Cylinder Section
  > DURING A ANNUAL INSPECTION, FOUND THE NR 1 CYLINDER TO BE INCORRECT FOR THIS INSTALLATION, INCORRECT CYLINDER INSTALLED MFG PRIOR TO INSTALLATION ON AIRCRAFT. CYLINDER WAS FOR SHORT REACH PLUGS, ENGINE USES LONG REACH. CYLINDER FOUND ON 2 ND ANNUAL INSPECTION
- [SDR 2003FA0000598](https://openairdocs.org/sdr/2003FA0000598.md): Connector · improper · May 15, 2003 · N529PT · Cessna T182T · Turn and Bank/Rate of Turn Indicator
  > THE CONNECTOR FROM AIRCRAFT HARNESS THAT MATS TO THE TURN COORDINATOR HAS IMPROPERLY CRIMPED PINS. THIS FAULTY CONNECTION CAUSES AUTOPILOT WING ROCKING AND CAN CAUSE UNDESIRABLE ROLL RATES DURING CLIMBS.
- [SDR 2002FA0001028](https://openairdocs.org/sdr/2002FA0001028.md): Magneto · damaged · Aug 26, 2002 · N24712 · Cessna T182T · Magneto/Distributor
  > OWNER COMPAINED WHEN RT MAGNETO WAS SELECTED ENGINE WOULD QUIT. AFTER REMOVING MAGNETO FOUND MANY INTERNAL PARTS BURNED. REPLACED WITH NEW MAGNETO.

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE aircraft_model_key = 'T182T'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/cessna-t182t/reports

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