Piper PA-22-150
Service difficulty reports · 30
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 = 'PA22150' 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.
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 = 'PA22150' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 2020FA0000135Terminal · misinstalledWHILE PERFORMING PREFLIGHT MAGNETO CHECK, IT WAS DETERMINED THAT THE LEFT MAGNETO WAS NOT PERFORMING CORRECTLY. THE AIRCRAFT RETURNED TO THE TIE DOWN AREA. ON DISASSEMBLY OF THE MAGNETO THE RING TERMINAL WAS FOUND TO BE INCORRECTLY CRIMPED ONTO THE COIL WIRE, SDR 2017FA0000548Landing Gear · corrodedRIGHT LANDING GEAR RUSTED FROM INSIDE OUT WHERE FORWARD SUPPORT TUBE JOINS THE AXLE. FOUND WHEN SPOTTED A RUST LINE. USING PUNCH AND SMALL HAMMER FOUND THE COMPLETE AREA WAS RUSTED FROM THE INSIDE OUT.SDR BQVR20120204Brake · lockedAT THE BEGINNING OF THE TAKEOFF ROLL, THE NOSE OF THE ACFT SUDDENLY LOWERED AND THE PROPELLER MADE CONTACT WITH THE GROUND. MX ARRIVED AT THE ACFT AND DISCOVERED THE LT BRAKE LOCKED AND THE LT WHEEL UNABLE TO ROLL. THE RT WHEEL WAS FREE TO MOVE. THE LT BRAKSDR CA101209012Compass · inoperative(CAN) WHEN SWINGING THE COMPASS THE EAST WEST ADJUSTMENT WAS NON RESPONSIVE COMPASS REPLACED WITH A NEW UNIT (TC# 20101209012)SDR 2008FA0000376Clamp · looseENGINE DID NOT RESPOND WHEN POWER WAS APPLIED ON A LOW FLY BY OF THE RUNWAY AND CAUSED THE PLANE TO LAND NEXT TO THE RUNWAY IN THE SNOW DAMAGING THE AIRCRAFT. THE FOLLOWING PROBLEM WAS FOUND ON POST INCIDENT INSPECTION OF ENGINE AND EITHER ONE CAN CONTRIBUTE SDR 2008FA0000375Clamp · wornENGINE DID NOT RESPOND WHEN POWER WAS APPLIED ON A LOW FLY BY OF THE RUNWAY AND CAUSED THE PLANE TO LAND NEXT TO THE RUNWAY IN THE SNOW DAMAGING THE AIRCRAFT. THE FOLLOWING TWO PROBLEMS WERE FOUND ON POST INCIDENT INSPECTION OF THE ENGINE AND EITHER ONE CAN COSDR 2008FA0000098Mount · crackedFOUND NOSE GEAR MOUNT CORRODED THIN IN SPOTS ON THE LOWER TUBES FROM THE INSIDE. ORIGINAL THICKNESS .049 INCH AND IN THE THIN SPOTS THE THICKNESS WAS LESS THAN .020 INCH. THE MOUNT HAD BEEN REPAIRED BY WELDING AND ONE WELD WAS A COLD WELD THAT CRACKED AND ALSDR 2008FA0000028Clamp · looseENGINE DID NOT RESPOND WHEN POWER APPLIED ON A LOW FLY BY AND CAUSED THE PLANE TO LAND NEXT TO RUNWAY IN SNOW, DAMAGING ACFT. FOLLOWING PROBLEMS WERE FOUND ON POST INCIDENT INSPECTION OF ENGINE AND EITHER ONE CAN CONTRIBUTE TO LOSS OF LITTLE ALONE BOTH TOGETSDR 2005FA0001473P-Lead · deterioratedDURING RUNUP AFTER ANNUAL INSPECTION, LEFT MAG WAS NOT WORKING. FOUND INSULATION ON P-LEAD WIRE WAS DETERIORATING AND SHORTING TO SHIELDING CAUSING MAG TO BE CONTINUOUSLY GROUNDED NO MATTER WHAT SWITCH POSITION WAS. REPLACED SECTION OF P-LEAD AS REQUIRED. TSDR 2005FA0001472P-Lead · deterioratedDURING RUNUP AFTER ANNUAL INSPECTION, LEFT MAG WAS NOT WORKING. FOUND INSULATION ON P-LEAD WIRE WAS DETERIORATING AND SHORTING TO SHIELDING CAUSING MAG TO BE CONTINUOUSLY GROUNDED NO MATTER WHAT SWITCH POSITION WAS. REPLACED SECTION OF P-LEAD AS REQUIRED. TSDR 2005FA0001471P-Lead · deterioratedDURING RUNUP AFTER ANNUAL INSPECTION, LT MAG WAS NOT WORKING. FOUND INSULATION ON P-LEAD WIRE WAS DETERIORATING AND SHORTING TO SHIELDING CAUSING MAG TO BE CONTINUOUSLY GROUNDED NO MATTER WHAT SWITCH POSITION WAS. REPLACED SECTION OF P-LEAD AS REQUIRED. THSDR 2005FA0001470P-Lead · deterioratedDURING RUNUP AFTER ANNUAL INSPECTION, LT MAG WAS NOT WORKING. FOUND INSULATION ON P-LEAD WIRE WAS DETERIORATING AND SHORTING TO SHIELDING CAUSING MAG TO BE CONTINUOUSLY GROUNDED NO MATTER WHAT SWITCH POSITION WAS. REPLACED SECTION OF P-LEAD AS REQUIRED. THISDR 2005FA0001632Tail Wheel · wornPILOT REPORTED SEVERE TAILWHEEL SHIMMY DURING LANDING ROLLOUT LEADING TO LOSS OF CONTROL AND GROUND LOOP WITH SIGNIFICANT DAMAGE TO AIRCRAFT. POST ACCIDENT INSP FOUND PLAY IN THE ALUMINUM SPACER BETWEEN THE TAILWHEEL ASSY AND THE TAILWHEEL SPRING. ALSO, THERSDR 2003FA0001081Fuel Cap · inadequateFUEL CAP DID NOT VENT. THE FUEL CAP WAS RETURNED TO MFG AND THEY REPORTED THE CAP TO BE VENTING PROPERLY. MFG REPLACED THE CAP AND THE REPLACEMENT REFUSED TO VENT. ON THE GROUND THERE APPEARS TO BE ADEQUATE VENTING CLEARANCE BETWEEN THE FILLER NECK WASHER ASDR 2003FA0001046Fuel Cap · malfunctionedNEW FUEL CAP DID NOT VENT. FUEL TANK WAS PARTIALLY COLLAPSED AND SPEWING SOUND WAS COMING FROM THE CAP. CAP WAS TURNED FOR REMOVAL AND WHEN THE INDENTS RELEASED THE CAP, THE TANK POPPED BACK UP IN PLACE. THE CAP DOES NOT SHOW ANY DEFORMATION OR DAMAGE, IT ASDR 2002FA0001105Fuel Cap · blockedAIRCRAFT WAS AT A CRUISE ALTITUDE OF 1800 FT WHEN ENGINE QUIT RUNNING. MADE AN EMERGENCY LANDING IN A HAY FIELD. FUEL SELECTOR WAS SELECTED ON RT TANK. POST INSPECTION FOUND ORIGINAL TYPE FUEL CAP VENTING WAS BLOCKED (RT TANK). INSPECTION OF FUEL AND OIL SCRESDR 20000913SH017Drum · warpedINNER WHEEL HALF ASSEMBLY CAUSING BRAKE DRUMS TO WARP. FOUND EXCESSIVE BRAKE DRAGGING WHEN PERFORMING ANNUAL INSPECTION. SINCE NO SPECIFIC KEY POSITION, ASSEMBLY CAN BE TAKEN OFF AND RE-ASSEMBLED IN DIFFERENT POSITIONS. WHEN TORQUING, WARPING CAN OCCUR IN BSDR 20000724SH017Fuel Line · deterioratedA MECHANIC PERFORMING ANNUAL INSP, REPORTED THE FUEL SYSTEM WOULD NOT FLOW FOR THE FUEL STRAINER TEST AND CLEANING. T/S FUEL SYS, FOUND BOTH RUBBER FUEL LINES IN BOTH WINGS WHERE THE TANK OUTLET FITTING IS CONNECTED TO THE FUSELAGE ALUMINUM FUEL LINE HAD DETSDR CA000516031Propeller · corroded(CAN) NO TEXTSDR 99ZZZX2286Valve · failedEXHAUST VALVE NR 3 CYLINDER BROKE AT STEM CLOSE TO FACE OF VALVE. COMPLETE HEAD OF VALVE GONE, NOT FOUND. CAUSE UNKNOWN. NOTE: LOG SHOWS PART AS NR 74541. PART NUMBER ON VALVE STEM IS SL 74541 G 58. ALSO, NR 3 CYLINDER WAS OVERHAULED BY CRS 202-87, W.O. SDR 98ZZZX3557Pushrod Spring · brokenPILOT NOTED THE ENGINE WOULD MISS THEN RUN. PILOT MADE PRECAUTIONARY LANDING. THE VALVE COVER ON CYLINDER NR 2 HAD A HOLE IN IT. INVESTIGATION SHOWED THE PUSHROD TUBE SPRING LYC P/N LW14995 BROKE AND SEPARATED AT THE HOLE FOR THE HOLD-DOWN STUD. THE BROKENSDR AU981019Stud · broken(AUS) NR 1 CYLINDER HOLDDOWN STUDS BROKEN OR LOOSE.SDR AU980522Mount · cracked(AUS) TOP RT ENGINE MOUNT TUBE CRACKED IN AREA ADJACENT TO THE WELD.SDR 98ZZZX760Strut · rustedWING STRUTS WERE INSPECTED IAW AD 93-10-06 AND SB 528D IN DEC '96 AND FOUND OK. DURING '97 ANNUAL, OWNER HAD ALL FOUR STRUTS INSPECTED AND MODIFIED. STC SA 4635NM WAS DONE TO STRUTS. OLD FORK BARREL WAS CUT OFF BY TECHNICIANS. FOUND 2 STRUTS RUSTED SEVERELSDR CA970429006Blade · corroded(CAN) PROPELLER RECEIVED FOR REPITCH. INSPECTION FOUND THE PROPELLER BLADES BENT WITH GOUGES AND CORROSION WHICH REQUIRED GRINDING AND FILLING.SDR AU961197Tube · corroded(AUS) FUSELAGE STRUCTURE LH REAR LONGITUDINAL TUBE LOCATED TO THE REAR OF THE LH PASSENGER DOOR CORRODED THROUGH IN THREE PLACES IN A 152.4MM (6IN) LENGTHSDR 96ZZZX3541Gasket · defectiveGASKET SOFT AND CAME APART WHEN TOUCHED. AIRCRAFT USES AUTOGAS AND WHEN MANUFACTURER CALLED, THEY SAID THEY NEVER CHECK THE GASKETS WITH AUTO FUEL AND DID NOT KNOW ANYTHING ABOUT WHAT IT WOULD DO. THIS WAS FOUND WHILE C/W WITH AD 96-09-06. SUBMITTER SUGGESTSDR 96ZZZX3329Tube · crackedCONVERTED FROM TRI-PACER TO PACER CONFIG BY STC 5A45RM, TIME AS PACER, APPROXIMATELY 1,220 HRS. TAIL POST TUBE CRACKED AT .25 INCH HOLE THAT FORMERLY HELD TAIL SKID IN PLACE, NO PROVISION IN STC TO BEEF UP HOLE AREA OF TAIL POST.SDR CA960222018Tubing · cracked(CAN) AIRCRAFT WAS INSPECTED AND FOUND TO HAVE SEVERAL CRACKS AND CORROSION IN STRUCTURAL TUBING, AS PER SKETCH, THAT APPEARS TO BE THE RESULT OF WATER FREEZING. SUBMITTER REPORTS THAT THE INSPECTION WOULD NOT HAVE SHOWN THESE DEFECTS WITH OUT HAVING LIFTED TSDR 95ZZZX1271Switch · defectiveDEFECTIVE BENDIX SWITCH FAILED ON TAKEOFF RESULTING IN ENGINE STOPPAGE AND SUBSTANTIAL DAMAGE TO AIRCRAFT. AD 76-7-12 WAS COMPLIED WITH 80 HOURS (THIS IS TO CORRECT A TYPOGRAPHICAL ERROR OF TIME SINCE ACCOMPLISHED 76-7-12 (80 HRS) PRIOR TO INCIDENT. ALSO, TH
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