Cessna 182M

Service difficulty reports · 25

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "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 = '182M'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR 2022FA0000499Oil Filter · looseAIRCRAFT IS EQUIPPED WITH AN AIRWOLF REMOTE OIL FILTER ADAPTER MOUNTED ON THE FIREWALL. A TEMPEST EZ TURN OIL FILTER PART # AA48109-1 WAS INSTALLED AT THE LAST OIL CHANGE AND INSTALLED WITHOUT THE USE OF DOW CORNING DC4 LUBRICANT ON THE SEAL AS DIRECTED BY THESep 10, 2022 · N71033 · Cessna 182M · Oil ServicingSDR 2021FA0000164Control Cable · intermittentFLAP OPERATION INTERMITTENT. FOUND PREVIOUSLY INSTALLED CONTROL CABLE (P/N S1244-20) BINDING AT CABLE CLAMP, AT FLAP ACTUATOR. FOUND CABLE IN OTHER AIRFRAMES HAVE CABLE PROTECTION FOR CLAMP, ELIMINATING INNER CABLE RESTRICTION. SOLICITED TO MANUFACTURE A CABLEApr 6, 2021 · N71752 · Cessna 182M · Trailing Edge Flap Control SystemSDR 2021FA0000093Control Cable · bindingFLAP OPERATION INTERMITTENT. FOUND PREVIOUSLY INSTALLED CONTROL CABLE (P/N S1244-20) BINDING AT CABLE CLAMP, AT FLAP ACTUATOR. FOUND CABLE IN OTHER AIRFRAMES HAVE CABLE PROTECTION FOR CLAMP, ELIMINATING INNER CABLE RESTRICTION. SOLICITED MCFARLAND AVIATION TO Apr 6, 2021 · N71752 · Cessna 182M · Trailing Edge Flap Control SystemSDR 2017FA0000397Bulkhead · crackedCRACKS WERE FOUND IN THE AFT BULKHEAD AND ALL FIVE VERTICAL FIN ATTACHMENT BOLTS WERE FOUND LOOSE. THIS WAS CAUSED BY THE AFT BULKHEAD BEING UNDER DESIGNED.May 18, 2017 · N71551 · Cessna 182M · Fuselage Main, BulkheadSDR 2017FA0000270Battery · leakingELT FAILED OPS CHECK. REMOVAL AND INSPECTION REVEALED 2 D CELL BATTERIES LEAKING PROFUSELY. UNIT WAS CLEANED AND INSPECTED AND ALL CELLS WERE REPLACED, EXPIRATION DATES WERE 2017. BATTERY EXPIRATION DATES WERE ALL 2019. 6 (SIX) MONTHS LATER THE ELT WAS AGAMar 27, 2014 · N1904F · Cessna 182M · Emergency Locator BeaconSDR 2012FA0000124Piston · failedNUMBER 5 CYLINDER ON O-470 ENGINE WITH APPROXIMATELY 300 HOURS EXPERIENCED PISTON FAILURE DUE TO WHAT APPEARS AT FIRST IMPRESSION DETONATION. HOWEVER, PISTON IS BELIEVE TO HAVE FAILED DUE TO FLAW IN MANUFACTURE OR EXPERIENCE DAMAGE SUCH AS DROPPING PRIOR TO INFeb 20, 2012 · N71890 · Cessna 182M · Reciprocating Engine Cylinder SectionSDR 2011FA0000561Bulkhead · crackedWHILE PERFORMING A VISUAL INSP OF THE AFT FUSELAGE BULKHEAD IAW AD 72-07-09; DISCOVERED CRACKS IN THE AFT BULKHEAD BETWEEN THE RUDDER CABLE CUTOUT AND THE BULKHEAD FLANGE (BOTH SIDES). FOLLOWING THE INSTRUCTIONS IN THE AD, PERFORMED A TORQUE CHECK OF THE BOLJul 28, 2011 · N91568 · Cessna 182M · Fuselage Main, BulkheadSDR 2008FA0000223Skin · crackedON INSPECTION BOTH FLAPS RT AND LT TOP AND BOTTOM FLAP SKINS WERE CRACKED 6 TO 8 INCHES ALONG THE T/E, ON THE RIVET LINE. ALSO SHEERED RIVETS ON (3) OF THE (4) FLAP TRACK LOWER TRACK TO RIBS. RESKINNED FLAPS AND INSTALLED MS21042 STEEL SCREWS IN REPLACEMENT Mar 8, 2008 · N71784 · Cessna 182M · Trailing Edge FlapsSDR 2006FA0000018Seal · deformedRESEALED FUEL SELECTOR VALVE PN 0716613-1 AND DURING A LEAK TEST LEAKAGE WAS FOUND FROM ONE OF THE PN 1216107-4 SEALS. INVESTIGATION FOUND THAT THE SEAL FACE WAS DEFORMED AND THAT MOLD LINES FROM THE INJECTION MOLDING PROCESS CAUSED VOIDS IN THE SEALING SURFACJan 11, 2006 · Cessna 182M · Aircraft Fuel Distribution SystemSDR 2002FA0000024Control Cable · brokenPILOT COMPLAINED THAT THE PROPELLER CONTROL WAS HARD TO MOVE. WHEN TECHNICIAN INVESTIGATED, THE CONTROL CABLE BROKE AND CAME OFF IN TECHNICIAN`S HAND. REMOVED AND REPLACED CONTROL WITH NEW PART.Dec 14, 2001 · N71398 · Cessna 182M · Propeller Controlling SystemSDR 2002FA0000267Piston · failedCASTROSPHOIC ENGINE FAILURE AFTER TAKEOFF. EMERGENCY LANDING WAS EXECUTED WITHOUT INCIDENT. ENGINE WAS DISASSEMBLED, REVEALING NR 5 PISTON DISINTEGRATED. ENGINE HAD BEEN OVERHAULED APPROXIMATELY 280 HOURS AND 3.5 YEARS PRIOR TO FAILURE. ALL PISTONS HAD BEEDec 1, 2001 · N71298 · Cessna 182M · Reciprocating Engine Power SectionSDR 20010424CW009Bulkhead · crackedWHILE PERFORMING 100 HOUR INSPECTION, FOUND A CRACK IN THE UPPER RADIUS ABOVE THE RIGHT RUDDER STOP BOLT. PROBABLE CAUSE WOULD BE FROM THE RUDDER CONTACTING TOO HARD, POSSIBLE WIND DAMAGE. RECOMMED A SOFT HEADED STOP BOLT.Sep 28, 2000 · N182AZ · Cessna 182M · Fuselage Main, BulkheadSDR 99ZZZX1640Valve Guide · wornEXHAUST VALVE GUIDES WORN OUT SEVERELY ON ALL 6 CYLINDERS. 133.0 HOURS SINCE NEW.Mar 29, 1999 · N91767 · Cessna 182M · Reciprocating Engine Cylinder SectionSDR 99ZZZX1639Valve Guide · wornEXHAUST VALVE GUIDES WORN OUT SEVERELY ON ALL 6 CYLINDERS. 210.3 HOURS SINCE NEW.Mar 29, 1999 · N91767 · Cessna 182M · Reciprocating Engine Cylinder SectionSDR 99ZZZX1032Stop · bentFOUND RUDDER STOP BENT AND NO LONGER LIMITING RUDDER TRAVEL. FOUND IMPROPER HARDWARE INSTALLED. TRUSS HEAD SCREW INSTEAD OF BOLT DID NOT ALLOW FOR PROPER CONTACT AREA. COULD NOT TELL FROM LOGS WHEN THIS WAS INSTALLED.Feb 11, 1999 · N71886 · Cessna 182M · Rudder StructureSDR CA990203001Lifter · broken(CAN) AFTER DEPARTURE DURING CLIMB-OUT, THE ENGINE BEGAN TO LOSE POWER. THE PILOT TURNED BACK TO THE POINT OF DEPARTURE, THE AIRCRAFT MADE A FORCED LANDING 38 MILES EAST OF THE BASE. THE AIRCRAFT WAS RECOVERED AND THE CAUSE OF THE POWER LOSS WAS DETERMINED TJan 15, 1999 · Cessna 182M · Reciprocating Engine Power SectionSDR AU970559Crankcase · out of limits(AUS) ENGINE CRANKCASE OUT OF LIMITS - FOUND DURING BULK STRIP DUE TO METAL CONTAMINATION - OTHER DEFECTS FOUND INCLUDED:-1. CAMSHAFT LOBE CASE HARDENING WORN AND LOBE CRACKED 2. THREE CYLINDERS UNSERVICEABLE WITH ONE CYLINDER WORN THROUGH THE HARD CHROME3. IMay 22, 1997 · Cessna 182M · Reciprocating Engine Power SectionSDR 97ZZZX803Bulkhead · crackedAFT BULKHEAD CRACKED BETWEEN RUDDER CABLE CUTOUT AND THE BULKHEAD FLANGE. INSTALLED NEW BULKHEAD ASSY C/W AD 72-07-09 AMDT 39-1988, PARA A,B,C,D,E, 123 F,G,I.Feb 2, 1997 · N71766 · Cessna 182M · Fuselage Main, BulkheadSDR 96ZZZX5303Cylinder · out of specCYLINDER CLASS 68-1 RECEIVED WITH INTAKE ROCKER SHAFT END-PLAY IN EXCESS OF (SIDE CLEARANCE). .040 INCH RECEIVED FROM EC SW, 8-13-96.Sep 10, 1996 · N71136 · Cessna 182M · Reciprocating Engine Cylinder SectionSDR AU961190Bulkhead · cracked(AUS) RH FORWARD DOORPOST BULKHEAD CRACKED IN BEND RELIEF NOTCH - FOUND DURING INSPECTION IAW AD/CESSNA180/75Aug 1, 1996 · Cessna 182M · Fuselage Main, BulkheadSDR AU960776Nlg · separated(AUS) NOSE LANDING GEAR SEPARATED FROM AIRCRAFT DURING LANDING (TORN OFF) - SUSPECT CAUSED BY HEAVY LANDING AND/OR INCORRECT LANDINGTECHNIQUE - PILOT ERRORJun 3, 1996 · Cessna 182M · Nose/Tail Landing Gear Strut/AxleSDR AU960665Battery · leaking(AUS) REMOTE ELT BATTERIES LEAKING CAUSING CORROSION DAMAGE TO THE ENTIRE UNITMay 3, 1996 · Cessna 182M · Emergency Locator BeaconSDR 96ZZZX2392Bulkhead · crackedDURING ANNUAL INSPECTION, FOUND AFT BULKHEAD AT FS 230.18 CRACKED AT LEFT RUDDER CABLE CUT OUT. THIS BULKHEAD HAD PREVIOUSLY CRACKED AT THE RIGHT RUDDER CABLE CUT OUT AND WAS REPAIRED. AD 72-07-09 AND CESSNA SB SE72-3 BOTH PERTAIN TO THIS AREA AND DO NOT ALLMar 8, 1996 · N70802 · Cessna 182M · Fuselage Main, BulkheadSDR AU960202Bulkhead · cracked(AUS) LH AND RH SIDE FORWARD DOORPOST BULKHEAD CRACKED - FOUND DURING INSPECTION IAW AD/C180/75 AMDT1Feb 21, 1996 · Cessna 182M · Fuselage Main, BulkheadSDR 95ZZZX964Cap · seal failedOLD STYLE CESSNA PLASTIC FUEL CAPS - SEALS ARE NOT AVAILABLE ANYMORE.Feb 12, 1995 · N70920 · Cessna 182M · Fuel Storage
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