N487MC
Service difficulty reports · 181
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N487MC' AND registry_match = 'registration' 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 n_number = 'N487MC' AND registry_match = 'registration' 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 P5CA2020070100217Splice · crackedM/D RT SUBSTITUTE TRACK SPLICE FOUND CRACKED. M/D RT SUBSTITUTE TRACK REPAIRED AS PER SRM 53-00-52 REPAIR 13.SDR P5CA2020070100218Depressor · crackedNR 2 ENG RT FIRE WALL SUPPORT DEPRESSOR FWD END FOUND CRACKED. DEPRESSOR REPLACED WITH NEW PART 311U2680-438 IAW DWG 311U2680.SDR P5CA2020070100219Seat Track · crackedM/D LT SUBSTITUTE TRACK AT STA 2183 FOUND CRACKED. M/D LT SUBSTITUTE TRACK REPAIRED AS PER SRM 53-00-52 REPAIR 13.SDR P5CA2020070100220Shear Web · crackedM/D RT FLOOR SHEAR WEB AT STA 472 RBL 88-94 FOUND CRACKED. M/D RT FLOOR SHEAR WEB REPLACED, REFER TO DWG 65B14804.SDR P5CA2020070100221Support Angle · crackedM/D LT FLOOR O/B SUPPORT ANGLE AT STA 1358 LBL 116 FOUND CRACKED. M/D LT FLOOR O/B SUPPORT ANGLE REPAIRED IAW RI-53-60-14100 REV A.SDR P5CA2020070100222Support Angle · crackedM/D LT FLOOR O/B SUPPORT ANGLE AT STA 1941 LBL 116 FOUND CRACKED. M/D LT FLOOR O/B SUPPORT ANGLE REPAIRED IAW RI-53-60-14092.SDR P5CA2020070100223Floorbeam · corrodedM/D LT FLOORBEAM AT STA 800 LBL 85 FOUND CORRODED. M/D LT FLOORBEAM AT STA 800 LBL 85 REPAIRED IAW SRM 53-00-51 REPAIR 3 FIG 201.SDR P5CA2020070100224Floorbeam · corrodedM/D FLOORBEAM STA 620 LBL 90 FOUND CORROSION. CORROSION REMOVED IAW SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101.SDR P5CA2020070100225Floorbeam · corrodedM/D FLOORBEAM 980 LBL 11- RBL 11 FOUND CORROSION. CORROSION REMOVED IAW SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101.SDR P5CA2020070100226Floorbeam · corrodedM/D FLOORBEAM STA 400 LBL 80 FOUND CORROSION. CORROSION REMOVED IAW SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101.SDR P5CA2020070100227Floorbeam · corrodedM/D FLOORBEAM STA 520 LBL 78 FOUND CORROSION. CORROSION REMOVED IAW SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101.SDR P5CA2020070100228Floorbeam · corrodedM/D FLOOR BEAM STA 761 RBL 22 FOUND CORROSION. CORROSION REMOVED IAW SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101.SDR P5CA2020070100229Seat Track · corrodedM/D SEAT TRACK STA 640-660 LBL 90 I/B FLANGE FOUND CORROSION. CORROSION REMOVED IAW SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101.SDR P5CA2020070100230Seat Track · corrodedM/D SEAT TRACK STA 1780-1800 LBL 99 FOUND CORROSION. CORROSION REMOVED IAW SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101.SDR P5CA2020070100231Stiffener · crackedRT HORIZ STAB 420 T/E O/B RIB VERTICAL STIFFENER FOUND CRACKED. VERTICAL STIFFENER REPLACED AS PER DWG 65B03651.SDR P5CA2020070100232Bulkhead · crackedAPU COMPT FWD BULKHEAD STA 2658 LT LOWER FOUND CRACKED. STA 2658 BULKHEAD REPAIRED IAW RI-53-83-14095 REV A.SDR P5CA2020070100233Structure · corrodedLT WLG WW CENTER TANK JETTISON PUMP BOLT HOLE FOUND CORROSION. CORROSION REMOVED IAW RI-57-12-14097 REV A.SDR P5CA2020070100234Structure · corrodedRT WLG WW CENTER TANK JETTISON PUMP BOLT HOLE FOUND CORROSION. CORROSION REMOVED IAW RI-57-12-14098 REV A.SDR P5CA2020070100235Fairing · delaminatedLT WING O/B MID FLAP L/E FAIRING (587PT) FOUND DELAMINATION. PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A REV 88.SDR P5CA2020070100236Fairing · delaminatedLT WING O/B MID FLAP L/E FAIRING (587QT) FOUND DELAMINATION. PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A REV 88.SDR P5CA2020070100237Fairing · delaminatedRT WING I/B MID FLAP L/E FAIRING FOUND DELAMINATION. PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A REV 88.SDR P5CA2020070100238Fairing · delaminatedRT WING O/B MID FLAP L/E FAIRING FOUND DELAMINATION. PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A REV 88.SDR P5CA2020070100239Fairing · delaminatedLT WING O/B MID FLAP L/E FAIRING FOUND DELAMINATION (FROM I/B 58"). PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A REV 88.SDR P5CA2020070100240Skin · corrodedM/D SIDE CARGO DOOR INNER SKIN STA 1860-1870 SPOT LIGHT FOUND CORROSION. CORROSION REMOVED IAW SRM 52-30-01 ALLOWABLE DAMAGE 1 FIG 101.SDR P5CA2020070100241Skin · corrodedM/D SIDE CARGO DOOR INNER SKIN STA 1790-1800 SPOT LIGHT FOUND CORROSION. CORROSION REMOVED IAW SRM 52-30-01 ALLOWABLE DAMAGE 1 FIG 101.SDR P5CA2020070100242Washer · tornNR 1 PYLON, BOTH LT AND RT UNDERWING MIDSPAR FITTING KARON WASHERS FOUND TORN. NR 1 PYLON BOTH LT AND RT UNDERWING MIDSPAR FITTING KARON WASHERS REPLACED AS PER HX RI NO RI-57-20-14099 REV A.SDR P5CA2020070100243Washer · unknownNR 4 PYLON, BOTH LT AND RT UNDERWING MIDSPAR FITTING KARON WASHERS FOUND TORN OR DETACHED. NR 4 PYLON BOTH LT AND RT UNDERWING MIDSPAR FITTING KARON WASHERS REPLACED AS PER HX RI NO RI-57-20-14099 REV A.SDR P5CA2020070100244Frame · crackedFX STA 880 BODY FRAME UPPER FOUND CRACKED. BODY FRAME REPAIRED IAW SRM 53-00-71 REPAIR 4 FIG 201.SDR P5CA2019102540214Pitot Head · inoperativeREJECTED T/O AT 70 KTS DUE TO NO AIRSPEED INDICATION ON CAPTAINS PFD.(<P>REMOVED AND REPLACED PITOT STATIC PROBE IAW AMM 34-11-01/401. PERFORMED CAPTAIN'S PITOT SYSTEM LEAK TEST IAW AMM 34-11-00-795-019, SYSTEM CHECKS OK. AIRCRAFT OK FOR SERVICE. <BR /></P>)SDR P5CA2019012200017Warning System · false activationAIRCRAFT PERFORMED AIR RETURN TO ICN DUE TO ENG 1 FUEL FILT MESSAGE.(<P>ONCE BACK IN BLOCKS, DEBRIEFED CREW AND DETERMINED ALL ENGINE PARAMETERS WERE NORMAL AND NO ERRATIC ENGINE CONDITIONS. ENGINE OPERATION WAS NORMAL.<BR /></P><P>MAINTENANCE INSPECTED AND RSDR P5CA2018102200326Pdu · malfunctionedFLAPS PRIMARY AND FLAPS DRIVE EICAS DURING FLAP EXTENSION.(<P>FLIGHT CREW REPORTED THAT LEFT INBOARD LEADING EDGE FLAP GROUP DID NOT EXTEND. CMC INDICATED LEADING EDGE FLAP DRIVE PDU L4 FAULTED. REPLACED PDU L4 AND ALL OPS CHECKS SATISFACTORY.<BR /></P>)
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