Cessna 182J

Service difficulty reports · 29

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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 = '182J'
  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 CA150930012Bulkhead · cracked(CAN) DURING MFG PROGRESSIVE CARE INSPECTION THE SPINNER DOME WAS FOUND TO BE LOOSE. UPON FURTHER INSPECTION THE SPINNER BULKHEAD WAS FOUND TO BE CRACKED ALL THE WAY AROUND CRANKSHAFT FLANGE. SPINNER AND PROPELLER RE & RE AND NEW BULKHEAD INSTALLED, PN D-752Sep 28, 2015 · Cessna 182J · Propeller Spinner SectionSDR CA131128009Casting · cracked(CAN) DURING A PROGRESSIVE CARE OPERATION INSPECTION, A CRACK WAS FOUND IN THE RT MLG OTBD SUPPORT CASTING, APPROXIMATELY 1" IN LENGTH AT THE AFT ATTACHMENT POINT ON LOWER RADIUS.Nov 25, 2013 · Cessna 182J · Wing, Landing Gear Attach FittingsSDR CA131128008Casting · cracked(CAN) DURING A PROGRESSIVE CARE OPERATION INSPECTION, A CRACK WAS FOUND IN THE LT MLG OTBD SUPPORT CASTING, APPROXIMATELY 1" IN LENGTH AT THE AFT ATTACHMENT POINT ON LOWER RADIUS.Nov 25, 2013 · Cessna 182J · Wing, Landing Gear Attach FittingsSDR 2013FA0000459Battery Pack · failedPURCHASED 406/121.5/243 ELT PN 451-23 TSO C126 APPROVED SN 11624 WITH GPS POSITIONS ON 04/08/2011. THE UNIT WAS INSTALLED. DURING ACFT ANNUAL THIS YEAR, MECHANIC NOTIFIED ME THAT MY BATTERIES IN MY ELT UNIT WERE DEAD. VERIFIED THAT NO CORROSION WAS PRESENT.May 10, 2013 · N2942F · Cessna 182J · Emergency Locator BeaconSDR CA130124008Bulkhead · cracked(CAN) DURING ANNUAL INSPECTION,THE REAR BULKHEAD WAS FOUND CRACKED AT TOP RT AND LT CORNERS WHERE THE RUDDER CABLES PASS THROUGH. A NEW REAR BULKHEAD WAS ORDERED AND WILL BE REPLACED BEFORE ACFT WILL BE RETUNED TO SERVICE.Jan 23, 2013 · Cessna 182J · Fuselage Main, BulkheadSDR CA120913002Propeller · misoverhauled(CAN) PROPELLER SENT TO MY SHOP WITH POSSIBLE INTERNAL OIL LEAK. NO INTERNAL OIL LEAK, BUT AFTER A VISUAL INSPECTION, DISCOVERED MAJOR ISSUES OF NON-COMPLIANCE FROM LAST O/H. THE O/H WAS DONE IN 2010. I HAVE BEEN IN CONTACT WITH ABOUT THIS, AND COURSE OF ASep 12, 2012 · Cessna 182J · Propeller AssemblySDR CA120604003Support · cracked(CAN) DURING A PROGRESSIVE CARE INSPECTION, A CRACK WAS FOUND ON THE RT MLG SUPPORT BRACKET. THE CRACK WAS APPROX .7500 LONG. THE CRACK WAS LOCATED WHERE BOLT GOES THROUGH THE BRACKET TO THE ATTACHMENT POINT.May 31, 2012 · Cessna 182J · Fuselage, Landing Gear Attach FittingsSDR CA090622003Support Bracket · cracked(CAN) ACFT STEERING AND RELATED SYS WERE INSPECTED DUE TO COMPLAINT REGARDING ACFT BEING HARD TO TURN TO THE RT. AN OPEN CRACK WAS FOUND ON LWR OLEO SUPPORT BRACKET DESCRIBED ABOVE. CONDITION MAY HAVE CAUSED FAILURE OF OLEO SUPPORT, POSSIBLY RESULTING IN OLEJun 12, 2009 · Cessna 182J · Main Landing GearSDR CA081107003Seat Track · cracked(CAN) 3 CRACKS LT PAS RAIL, 1 CRACK LT PILOTS RAIL, SEAT RAILS SOME WEAR, WEAR WITHIN LIMITS.Nov 3, 2008 · Cessna 182J · Fuselage, Seat/Cargo Attach FittingsSDR K2Z2005F00000Bulkhead · crackedCRACKS FOUND IN BOTH SIDES, UPPER CORNER OF RUDDER CABLE CUTOUT BETWEEN COUTOUT AND FLANGE. DYE PENETRANT INSPECTION OF FRONT FLANGE REVEALED NO DEFECTS. INSPECTION OF THIS BULKHEAD PREVIOUSLY ACCOMPLISHED AT 3607. NOT REQUIRED FOR INSPECTION IAW AD. RECOMMay 31, 2005 · N3474F · Cessna 182J · Fuselage Main, BulkheadSDR CA050519001Leg Assy · cracked(CAN) DUE TO A BROKEN MLG LEG ON ONE OF OUR AIRCRAFT LAST SEASON IT WAS DECIDED TO HAVE ALL MLG LEGS MAGNAFLUXED TO DETERMINE IF ANY OTHERS IN THE FLEET WERE CRACKED. EACH INSPECTION SINCE THEN, NDTD LEGS HAVE BEEN INSTALLED AND THE LEGS REMOVED FROM SERVICE May 17, 2005 · Cessna 182J · Main Landing GearSDR CA030627003Mount · cracked(CAN) ENGINE MOUNT CRACKED AT SUPPORT PADS. REINFORCED TO CARRY 10520 ENGINE AS PER P-PONK STC SA461NW ON JULY 96. MOUNT REPLACED WITH NEW MOUNT PN 4402. NO VIBRATION TO DATE.Jun 20, 2003 · Cessna 182J · Engine Mount SectionSDR 2002FA0000825Nut · crackedDURING CYLINDER INSTALLATION P/N 652541 NUT CRACKED DURING TORQUEING OPERATION. FAILURE AT ABOUT 60 FT/LBSMay 23, 2002 · N3090F · Cessna 182J · Reciprocating Engine Cylinder SectionSDR CA040622004Crankcase · cracked(CAN) WHILE CONDUCTING PRE-FLIGHT CHECK, OIL DRIPS WHERE NOTICED. AFTER VERIFICATION BY AN AMO, IT WAS DETERMINED THAT THERE WAS A SMALL CRACK IN THE CRANKCASE. ENGINE DISASSEMBLED AND CRANKCASE WAS REPLACED.May 6, 2002 · Cessna 182J · Reciprocating Engine Power SectionSDR 20001012SH012Bulkhead · crackedAFT BULKHEAD AT BS 230.187 WAS FOUND CRACKED DURING VISUAL INSPECTION IN THE AREA OF THE LEFT RUDDER CABLE CUT-OUT RADIUS AND THE BULKHEAD FLANGE. THESE CRACKS CAN BE VERY FINE AND HARD TO SEE. THEY USUALLY CAN BE VERIFIED BY VIEWING THE BULKHEAD FROM THE FRSep 22, 2000 · N3120F · Cessna 182J · Rudder StructureSDR 20000816SH031Hub · crackedHUB, SN 697045, CRACKED IN NR 2 HUB SOCKET ON BACK SIDE. RED DYE LEAKING FROM PROPELLER. CAUSE OF CRACK UNKNOWN. REPLACED HUB WITH SN 725308. (X)Jul 31, 2000 · Cessna 182J · Propeller Hub SectionSDR AU981384Tappet · misinstalled(AUS) ENGINE TAPPETS FITTED IN THE INCORRECT LOCATIONS. SUBMITTER SUSPECTED ALSO UNAPPROVED PARTS. PART TC: 740.Oct 4, 1998 · Cessna 182J · Reciprocating Engine Cylinder SectionSDR 98ZZZX3434Bulkhead · crackedDURING ROUTINE INSPECTION, CRACK IN BULKHEAD FOUND. RECOMMEND CLOSE INSPECTION DURING ANNUAL INSPECTIONS.Sep 10, 1998 · N3304F · Cessna 182J · Fuselage Main, BulkheadSDR 98ZZZX4228Alternator · failedCUSTOMER COMPLAINED OF 'NO ALTERNATOR OUTPUT - AMMETER SHOWS DISCHARGE'. MECHANIC FOUND THE ALTERNATOR IN 3 PIECES. THE DRIVE END WAS STILL ATTACHED TO THE MOUNT AND WAS STILL CAPABLE OF ROTATING. THE STATOR WAS FOUND IN THE BOTTOM OF THE COWL, THE HEAD ENDSep 4, 1998 · N3388F · Cessna 182J · Alternator-Generator DriveSDR 98ZZZX3012Cylinder Assy · misoverhauledTHIS ENGINE WAS OVERHAULED AND INSTALLED ON 3-25-92, NR 1 AND NR 3 CYLINDERS WERE REMOVED AT 536.7 HOURS DUE TO LOW COMPRESSION. CYLINDERS WERE SENT BACK FOR REPAIR BOTH INTAKE AND EXHAUST SEATS AND EXHAUST GUIDES WERE BAD, CYLINDERS RE-INSTALLED AT 621.6 HOJul 1, 1998 · N3090F · Cessna 182J · Reciprocating Engine Cylinder SectionSDR 98ZZZX897Blade · crackedPROPELLER WAS SHOWING SIGNS OF ERRATIC PITCH CHANGE AND STICKING. BLADE SHOWS EVIDENCE OF PREVIOUS IMPACT STRIKE. THIS AIRCRAFT HAD PREVIOUSLY HAD A STUCK PRESSURE RELIEF VALVE IN THE GOVERNOR WHICH, AFTER DISCUSSION WITH THE PILOT, MAY HAVE CAUSED AN OVERSPFeb 10, 1998 · N979ND · Cessna 182J · Propeller Blade SectionSDR 98ZZZX189Yoke Shaft · fouledDURING ANNUAL INSPECTION, FOUND UP ELEVATOR TRAVEL BELOW LIMIT BY 30 PERCENT - 18 DEGREES UP - 26 DEGREES PLUS 1 MINUS ZERO DEG. INSPECTION FOUND 'TINNERMAN' TYPE HOSE CLAMP CAUGHT INBETWEEN LT YOKE SHAFT P/N 0713667-1, AND LT CONTROL WHEEL SUPPORT ASSY STOPPDec 1, 1997 · N3546F · Cessna 182J · Control Column SectionSDR 97ZZZX3485Bulkhead · crackedPILOTS HAD COMMENTED ON A 'CLICKING' SOUND SOMEWHERE IN THE CABIN FOR SOME TIME. DURING AN ANNUAL INSPECTION, THE STARBOARD TUNNEL BULKHEAD WAS FOUND CRACKED IN AREA OF THE FUEL LINE (TO FIREWALL BULKHEAD FITTING). POSSIBLE CAUSE OF DAMAGE MAY BE FROM SEVEREJul 1, 1997 · N2787F · Cessna 182J · Fuselage Miscellaneous StructureSDR 96ZZZX4374Pump · drive shearedVACUUM PUMP DRIVESHAFT SHEARED AND SPLINES EXTREMELY WORN. IT STILL MADE VACUUM PRESSURE. SUBMITTER RECOMMENDS MORE FREQUENT INSPECTIONS OF DRIVE SPLINE ASSY (NOTE: WET DRIVE VACUUM PUMP).Aug 22, 1996 · N2714F · Cessna 182J · Vacuum Distribution SystemSDR 96ZZZX5216Hose · splitAFTER EACH FLIGHT, PILOT REPORTED HAD TO WIPE FUEL STAIN FROM TRAILING EDGE OF LT WING. INSPECTION OF LT FUEL BLADDER MADE AND FOUND HOSE CONNECTING TANK VENT LINE TO THE LT FUEL TANK WAS SPLIT AND ALLOWING FUEL TO VENT INTO THE WING BAY OUTBOARD OF LT TANK. Aug 5, 1996 · N3119F · Cessna 182J · Fuel StorageSDR EY2R9600200Blade · corrodedBLADE ASSY SN C37703 IS CORRODEDJan 1, 1996 · Cessna 182J · Propeller Blade SectionSDR 95ZZZX3801Rib · bentHORIZONTAL STABILIZER LEADING EDGE RIBS FOUND BENT. DISCOVERED BY PINCHING THE LEADING EDGE AT EACH RIB. SUBMITTER SUGGESTS POOR GROUND HANDLING MAY BE THE CAUSE OF THIS DAMAGE.Apr 14, 1995 · N2687F · Cessna 182J · Horizontal Stabilizer, Spar/RibSDR 95ZZZX3800Rib · bentHORIZONTAL STABILIZER LEADING EDGE RIBS FOUND BENT. DISCOVERED BY PINCHING THE LEADING EDGE AT EACH RIB. SUBMITTER SUGGESTS POOR GROUND HANDLING MAY BE THE CAUSE OF THIS DAMAGE.Apr 14, 1995 · N2687F · Cessna 182J · Horizontal Stabilizer, Spar/RibSDR 95ZZZX2623Mount · pittedDURING ANNUAL INSPECTION, FOUND ENGINE MOUNT PITTED MORE THAN 10 PERCENT OF TUBE THICKNESS IN AREA OF CLOSE PROXIMITY TO THE EXHAUST SYSTEM. CESSNA PARTS MANUAL DOES NOT LIST EXHAUST DEFLECTOR, HEAT SHIELDS, FOR THIS SERIAL NUMBERED AIRCRAFT. SUBMITTER SUGGEMar 28, 1995 · N3063F · Cessna 182J · Engine Mount Section
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