N421UP
Service difficulty reports · 311
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 = 'N421UP' 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 = 'N421UP' 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 UPS08552881Skin · corrodedINSPECTION TYPE:C2 APU INLET DUCT TO FUSELAGE SKIN HAS CORROSION EMINATING FROM NUTPLATE HOLES. REPAIRED AREA IAW ATS ER 08-2389SDR UPS08551668Landing Gear · warning messageAIR/GROUND DISAGREE MESSAGE. ACCOMPLISH FIM 32-09 FIG 106 NO FAULTS AND FIM 32-09-03 FIG 103 PSEU BITE CHECK, NO FAULTS NOTED. PSEU SYSTEM IS OK. STATUS MESSAGE CLEARED.SDR UPS07550352Structure · damagedN/A NR 2 LEADING EDGE SLAT HAS VARIOUS DENTS FROM HAIL DAMAGE. NR 2 SLAT HAS 98 DENTS FROM HAIL DAMAGE. DENTS GREATER THAN .010 INCH ARE DOCUMENTED IN FIG 1 EO B757-5750-27018-A. 10-8-07 ACCOMPLISHED REMOVAL OF NR 1 L/E SLAT UP THROUGH STEP D14 OF MM 27-SDR UPS06547732Angle · wornINSPECTION TYPE:C MAIN DECK FRAME AT BS 1620 LT BETWEEN STR 15-16 HAS WEAR MARK COVER BY CAPSTRIP MOD. FABRICATED REPAIR DOUBLER ANGLE ON MAE TRAVELER NR T6-622527, 7075-0.090 BATCH NR 299181, PO NR MST0008906, HEAT TREAT TO T6 PER AMS 27706, LOT NR 19765.SDR UPS06547731Angle · wornINSPECTION TYPE:C MAIN DECK FRAME AT BS 1500 RT, BETWEEN STR, 15-16 HAS WEAR MARK VO COVERED BY CAP STRIP MOD. FABRICATED REPAIR 'J' ANGLE ON TRAVELER NR T6/622633, MAT'L TYPE 7075-T6 .080, BATCH NR 1051875, PO NR MST 19871, LOT NR 19766 IAW SRM 51-70-11-0G.SDR UPS06547794Fitting · out of limitsINSPECTION TYPE:C RT WING, INBD LUG BORE OUT OF LIMIT. FAB BUSHING ON TRAVELER T6/621746 AND INSTALLED IAW EA 757-5720-27-A1 511 STEP NR 5 ON EA 757-5720-27-A1511 AFTER REWORK LUG DIAMETER IS 1.7 903 STEP NR 6 ON EA 757-5720-27-A1511 MATERIAL THICKNESS BEWTEESDR UPS06547780Bulkhead · chafedINSPECTION TYPE:C NR 1 PYLON AFT BULKHEAD INBD LOWER CORNER CHAFED. FINISHED REPAIR PER SOPM 20-43-03, AND EA NR 757-5453-27-A1509 STEPS 3 3,4,6, AND 7.SDR UPS06547781Frame · dentedINSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1460 BET S26R TO S27R. REPAIR AT FRAME STA: 1460, BET S26R AND S27R HAS BEEN ACCOMPLISHED PER FINAL EA NR 757-5362-27-A1508 WITH NO DEVIATIONS AND UPS EO NR B757-53 10-24958-A, NOTE: ALL WORK STEPS ACCOMPSDR UPS06547700Skin · dentedLT AFT FUSELAGE SKIN DENTED BS 1682, S4L APPROX L .3750 INCH BY W .3125 INCH BY D- .039. BLENDED AND BUFFED OUT GOUGE IN DENTED AREA IAW SRM 53-00-01-1. CUT OUT DAMAGED SKIN IAW SRM 53-00-01, FIG 201. HFEC CUTOUT IAW NTM 51-00-00 PR 6 NO CRACKED NOTED. FABSDR UPS05544998Panel · delaminatedJUST AFT OF RIGHT WING JACK PAD LWR SURFACE PANEL HAS DELAM. PANEL HAS A 3X4 AREA OF DELAM OUT OF LIMITS PER 57-51-01-1A. SECOND, REMOVED PANEL TO S/M SHOP. THIRD, REMOVED DAMAGE, INSTALLED NEW CORE, INSTALLED PLIES & STARTED CURE SRM 51-70-05-06. REMOVED SDR UPS05544416Yaw Damper · leakingINSPECTION TYPE:N/A ATB - EXCESSIVE RUDDER TRIM REQ FOR LEVEL FLIGHT. T/S IN PROGRESS. FOUND BOTH YAW DAMPNERS LEAKING. ORDERED TWO EACH AND TUBE AND LINK ASSY P/N 251N3058-8. AWAITING PARTS.
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