Piper PA-42-1000
Service difficulty reports · 21
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 = 'PA421000' 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 = 'PA421000' 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 2020F00118Brace · crackedDURING A ROUTINE EVENT INSPECTION ON N411BG , 42-5527004 THE RIGHT
MAIN LANDING GEAR SIDE BRACE P/N 75245-015 WAS FOUND CRACKED, SEE PHOTOS
ATTACHED.
THIS PART HAS A LIFE LIMIT OF 3,000 HOURS , THE TIME IN SERVICE ON
THIS PART IS 2,601.6 THE PARTSDR 2013FA0000694Brace · crackedDURING ROUTINE MAINTENANCE, INSPECTOR OBSERVED CRACK IN RT MLG FWD SIDE BRACE, PN 75245-015, SECOND FINDING.SDR GW1R20120427181Brace · crackedDURING ROUTINE INSPECTION, RT MLG SIDE BRACE WAS FOUND CRACKED. THIS IS A POST SB 0817C PART. PART LIFE-LIMIT IS 3,000 HRS PART TTSN:1876.7 HRS. PART WAS REPLACED WITH NEW UNIT. NOTE: THIS IS THE SECOND OCCASION THAT THIS PART HAS BEEN FOUND CRACKED ON THISSDR 2010FA0001093Link Assy · cracked(GW1R) DURING ROUTINE INSPECTION, THE NLG IDLER-LINK ASSY. INDICATED CRACKS IN 3 LOCATIONS BY FLOURESCENT PENETRANT INSP (FPI).SDR 2010FA0000835Link Assy · crackedDURING ROUTINE INSP, MX OF THE NLG THE LINK ASSY, NLG IDLER WAS FOUND CRACKED IN THREE (3) AREAS. THERE IS NO LIFE LIMIT ON THIS PART AND NO SPECIAL INSP REQUIREMENTS. SUGGEST 500 HR REPETIVE IN CONJUNCTION WITH SL1088 NLG SIDE BRACE INSP.SDR 2010FA0000272Bolt · shearedBOLT PN 400-159 WAS FOUND SHEARED. SB 885 SPECIFIES BOLT REPLACEMENT AT 500 HR INTERVALS. FAILED BOTH TTSN WAS 414.1 HRS. REPLACEMENT BOLT PN 400-159, RIB PN 50377-011, BRACKET PN 73524-003, ACTUATORS AND MISC. HARDWARE.SDR 2009FA0000450Brace · crackedDURING ROUTINE INSP, PART WAS FOUND CRACKED. THIS IS A POST SB817C UNIT. PART LIFE LIMIT IS 3,000 HRS.SDR 2007FA0000657Roll Pin · shearedPILOTS RT RUDDER PEDAL ROLL PINS SHEARED. REFERENCE IPC PN 761792, FIG. 103, INDEX 14, PN 480572. FAILURE MAY CAUSE LOSS OF DIRECTIONAL CONTROL OR BRAKING ACTION DURING GROUND OPERATION. (K)SDR 2006FA0000678Fork · crackedPILOT REPORTED A LEAKING LT MAIN GEAR STRUT, BUT WAS LEAKING FROM JOINT BETWEEN ALUMINUM FORK ASSY AND CHROMED STEEL STRUT TUBE. STRUT DISASSEMBLED AND A RADIAL CRACK WAS FOUND, 2 INCH LOGN AND .5 INCH. BELOW TOP OF ALUMINUM FORK ASSY. A SERIOUS ACCIDENT COSDR 2005FA0001211O-Ring · cutAT THE OUTER MARKER ON APPROACH, THE PILOT NOTICED AN OIL ODOR IN THE ENVIRONMENTAL SYSTEM. THE AIRCRAFT LANDED WITHOUT INCIDENT. POST FLIGHT WALK AROUND REVEALED OIL LEAK AT THE RT PROPELLER. MAINTENANCE WAS DISPATCHED AND INVESTIGATION REVEALED THE RT PROSDR 20000711SH006Rod End · brokenRIGHT MAIN LANDING GEAR ACTUATOR ROD END BROKE IN HALF WHERE PIVOT BALL IS RETAINED. NOT SURE WHETHER IT BROKE ON UP OR DOWN CYCLE. AFTER FAILURE, GEAR WOULD NOT COMPLETELY LOCK. BLOW DOWN SYSTEM AND HAND PUMP WERE NOT ABLE TO WORK WITH ROD END BROKEN. GEASDR 20000412SH001Trunnion · damagedPART IS MAIN LANDING GEAR REAR SIDE BRACE TRUNNION. A SMALL CRACK WAS FOUND IN THE WEB NEXT TO THE INBOARD LOWER BOLT HOLE ON BOTH RT AND LT MAIN GEAR. CRACK WAS DETECTED BY SMALL CRACK IN PAINT AND VERIFIED BY DYE PENETRANT. (X)SDR 20000407SH032Trunnion · damagedPART IS MAIN LANDING GEAR REAR SIDE BRACE TRUNNION. A SMALL ERODE WAS FOUND IN THE WEB NEXT TO THE INBOARD LOWER BOLT HOLE ON BOTH RT AND LT MAIN GEAR. CRACK WAS DETECTED BY SMALL CRACK IN PAINT. CRACK WAS VERIFIED BY DYE PENETRANT. (X)SDR 20000407SH020Trunnion · crackedPART IS MAIN LANDING GEAR REAR SIDE BRACE TRUNNION. A SMALL CRACK WAS FOUND IN THE WEB NEAR TO THE INBOARD LOWER BOLT HOLE ON BOTH RT AND LT MAIN GEAR. CRACK DETECTED FROM PREVIOUS EXPERIENCE. CRACK WAS VERIFIED BY DYE PENETRANT. (X)SDR 20000407SH016Trunnion · crackedPART IS MAIN LANDING GEAR REAR SIDE BRACE TRUNNION. A SMALL CRACK WAS FOUND IN THE WEB NEXT TO THE INBOARD LOWER BOLT HOLE ON BOTH RT AND LT MAIN GEAR. CRACK WAS DETECTED BY PREVIOUS EXPERIENCE. CRACK WAS VERIFIED BY DYE PENETRANT. (X)SDR 98ZZZX4531Fork Bolt · failedLEFT MAIN LANDING GEAR WOULD NOT RETRACT. FORK BOLT WHICH ATTACHES HYDRAULIC ACTUATOR TO FORWARD SIDE BRACES HAD SHEARED. INSTALLED NEW FORK BOLT, OPERATIONAL CHECK SATISFACTORY. PIPER HAS A 500-HOUR LIFE LIMIT ON THE MLG ACTUATOR ATTACH BOLT WHICH SECURES SDR 97ZZZX17Elevator · crackedAFTER PAINT WAS CHEMICALLY REMOVED, 3 CRACKS WERE FOUND IN THE SKIN AT THE COUNTERWEIGHT CHANNEL RUNNING AFT. 2 MORE CRACKS WERE FOUND IN THE STRINGER AFT OF THAT CHANNEL. LOOKING THROUGH THE ACCESS PANEL, IT WAS ALSO FOUND THAT THE STRINGER WAS BROKEN.SDR 96ZZZX4760Deice Boot · shortedWHILE IN-FLIGHT, THE CREW NOTICED A SUDDEN SHOWER OF SPARKS FROM THE LEFT PROPELLER. A QUICK CHECK OF THE AMMETER SHOWED NO UNUSUAL CURRENT DRAW. THE PROPELLER DEICE SYSTEM SHUT ITSELF OFF BEFORE THE CREW COULD TURN IT OFF. AFTER LANDING, THE PROPELLER WAS SDR 96ZZZX578Housing · failedAIRCRAFT WAS MODIFIED WITH LONG RANGE FUEL TANKS FOR FLIGHT TO AUKLAND, NEW ZEALAND FROM OAKLAND, CALIFORNIA. AIRCRAFT WAS APPROVED FOR OVERWEIGHT TAKEOFF. DURING TAKEOFF ROLL, LEFT MLG COLLAPSED CAUSING EXTENSIVE DAMAGE TO AIRCRAFT. MLG HOUSING WAS INSPECTSDR 95ZZZX3223Strut · splitAIRCRAFT HAS EXTRA TANKS INSTALLED AND WAS FULLY FUELED FOR FLIGHT TO NEW ZEALAND. AIRCRAFT AUTHORIZED 125 PERCENT CTOW BY DIRECTORATE, BUT WAS LOADED TO 118 PERCENT CTOW. AIRCRAFT BEGAN TAKEOFF ROLL AND WAS TRAVELLING APPROXIMTELY 40 KNOTS WHEN TAKEOFF WAS SDR 95ZZZX2409Shaft Assy · flange crackedMLG PIVOT SHAFT ASSY CONTAINS PIVOT SHAFT AND FWD ATTACH FLANGE. FWD ATTACH FLANGE MOUNTED TO MAIN WING SPAR. THIS ATTACH FLANGE FOUND CRACKED AND BROKEN OUT ALLOWING PIVOT SHAFT (WHICH IS BOLTED TO IT) TO MOVE AFT TOWARD WW. PILOT REPORTED CLUNK NOISE AT G
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