N593FE
Service difficulty reports · 318
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 = 'N593FE' 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 = 'N593FE' 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 04FDEA02710Frame · dentedFUSELAGE FRAME AT STA 1601, LT L12, FOUND DENTED. DENTED AREA TRIMMED OUT AT CABIN-FUSELAGE FRAME STA 1601, LEFT HAND LONGERON 12 AND REPAIR CARRIED OUT AS PER SRM 53-30-00 VOL I AND INSTALLED AS PER SRM 51-33- 01 VOL II. REFER TO EA 1-5310-79743.SDR 04FDEA02688Track · crackedENGINE NR 2, RT, T/R COWL AT UPPER SLIDER TRACK END FOUND WITH CRACK. T/R COWL REMOVED AS PER AMM 78-33-01-4. REPAIR CARRIED OUT, REFER TO FAA 8130-3, FORM TRACKING NO. 5479 RIGHT HAND THRUST REVERSER COWL RE-INSTALLED AS PER AMM 78-33-01-4. ADJUSTMENT ASDR 04FDEA02687Track · crackedENGINE NR 3 LT T/R COWL UPPER SLIDER TRACK END FOUND WITH CRACK. REMOVED AND REPLACED AS PER AMM 78-33-01-4 AND REPAIR CARRIED OUT, PLS REFER TO FAA 8130-3 FORM TRACKING NR 5480 FOR FURTHER WORK DETAILS AND INSTALLED AS PER AMM 78-33-01-04 AND FUNCTIOSDR 04FDEA02666Longeron · corrodedCENTER CARGO COMPARTMENT AT BETWEEN STATION 5-73 TO 5-113, LONGERON 52 FOUND CORRODED. CORRODED LONGERON AT CENTER CARGO COMPARTMENT, BETWEEN STATION 5-73 TO STATION 5-113 LONGERON 52 TRIMMED OUT AND CARRIED OUT REPAIR AS PER SRM 53-10-00 FIG 2 VOL I.SDR 04FDEA02661Panel · corrodedRIGHT HAND HORIZONTAL STABILIZER NR 22 BARREL NUT BORE CORROSION EXCEEDED CONDITION 3 LIMITS. RIGHT HAND HORIZONTAL STABILIZER NR 22 BARREL NUT BORE REPAIRED AS PER EA NR 1-5510-80309 TITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 22R. REWORKED BEYOND S/B MSDR 04FDEA02656Stop Fitting · crackedLT WING OUTBOARD FLAP INBOARD STOP FITTING FOUND CRACKED. REMOVED CRACKED FITTING AS PER SRM 51-31-01 VOL II AND INSTALLED NEW FITTING AT LEFT HAND WING OUTBOARD FLAP INBOARD AS PER SRM 51-33-01 VOL II.SDR 04FDEA02655Stop Fitting · crackedRT WING OUTBOARD FLAP INBOARD STOP FITTING FOUND CRACKED. REMOVED STOP FITTING AS PER SRM 51-31-01 VOL II AND INSTALLED NEW FITTING AT RIGHT HAND WING OUTBOARD FLAP INBOARD AS PER SRM 51-33-01 VOL II.SDR 04FDEA02579Frame · dentedCABIN, FUSELAGE FRAME AT STA 1681, LEFT HAND, L12, FOUND DENTED. DENTED AREA TRIMMED OUT AT CABIN, FUSELAGE FRAME STA 1681, LEFT HAND LONGERON 12 AND REPAIR CARRIED OUT AS PER SRM 53-30-00 VOLUME I AND INSTALLED AS PER SRM 51-33-01 VOLUME II. FEDEX EA NR 1-5SDR 04FDEA02578Frame · dentedCABIN, FUSELAGE FRAME AT STA 1701, LEFT HAND, L12, FOUND DENTED. DENTED AREA TRIMMED OUT AT CABIN, FUSELAGE FRAME STA 1701, LEFT HAND LONGERON 12 AND REPAIR CARRIED OUT AS PER SRM 53-30-00 VOLUME I AND INSTALLED AS PER SRM 51-33-01 VOLUME II. FEDEX EA NR 1-SDR 04FDEA02577Frame · dentedCABIN - FUSELAGE FRAME AT STA 1721, LEFT HAND, S12, FOUND DENTED. DENTED AREA TRIMMED OUT AT CABIN-FUSELAGE FRAME STA 1721, LEFT HAND LONGERON 12 AND REPAIR CARRIED OUT AS PER SRM 53-30-00 VOLUME I AND INSTALLED AS PER SRM 53- 30-00 VOLUME II. FEDEX EA 1-53SDR 04FDEA02576Splice · crackedCENTER CARGO COMPARTMENT AT STA 5-113 TO 1542 LONGERON 41L SPLICE FITTING FOUND CRACKED. REMOVED AND REPLACED WITH NEW SPLICE FITTING AS PER SRM 51-33-01 VOL II.SDR 04FDEA02575Splice · crackedCENTER CARGO COMPARTMENT AT STA 5-113 TO 1542 LONGERON 34L SPLICE FITTING FOUND CRACKED. REMOVED AND REPLACED WITH NEW FABRICATED SPLICE FITTING AND INSTALLED AS PER SRM 51-33-01 VOL II.SDR 04FDEA02574Splice · crackedCENTER CARGO COMPARTMENT AT STA 5-113 TO 1542 LONGERON 38R SPLICE FITTING FOUND CRACKED. REMOVED AND REPLACED WITH NEW FABRICATED SPLICE FITTING AS PER DWG A5A7114 AND INSTALLED AS PER SRM 51-33-01 VOL II.SDR 04FDEA02556Rib · crackedLEFT HAND WING LEADING EDGE NR 16 SLAT TRACK RIB FOUND CRACK. REMOVED CRACKED RIB AS PER SRM 51-31-01 VOL II AND INSTALLED NEW RIB AT LEFT HAND WING LEADING EDGE NR 16 SLAT TRACK AREA AS PER SRM 51-33-01 VOL II.SDR 04FDEA02555Rib · crackedRIGHT HAND WING LEADING EDGE NR 16 SLAT TRACK RIB FOUND CRACK. REMOVED CRACKED RIB AS PER SRM 51-31-01 VOL II AND INSTALLED NEW RIB AT RIGHT HAND WING LEADING EDGE NR 16 SLAT TRACK AS PER DRAWING ARB7565 AND SRM 51-33-01 VOL II.SDR 03FDEA00949Windshield · damagedAT FL 330 .84 MACH, OBJECT HIT WINDSCREEN IN 2 PLACES AND FRACTURED R1 FROM BOTTOM UPWARDS. CONT TO FRACTURE SPREAD ACROSS WINDSHIELD. SPIDER WEB AT LOWER PORTION OF R1 THROUGH TO UPPER PORTION. FACT R/R R1 WINDSHIELD ASSY PER MD-11M/M 56-11-01-4. AFTESDR 03FDEA00348Fitting · crackedLT OB FLAP TRACK FITTING IS CRACKED AT THE UP STOP MOUNT BARREL NUT HOLE. REPAIRED PER EA 1-5750-67543. THIS EA REMOVES THE 3D0011 BARREL NUT ASSY. AND NAS578-8B RETAINER AND INSTALLS A ZERO CLEARANCE FIT PLUG IN PLACE OF THE REMOVED PARTS AND PROVIDES FOSDR 02FDEA00677Actuator · malfunctionedAFTER TAKEOFF, BOTH PRIMARY (LIGHT BY HANDLE) AND SECONDARY (SYNOPTIC) SHOWED UNSAFE FOR LEFT MAIN LANDING GEAR WITH GEAR HANDLE UP. CYCLED GEAR, NO HELP. INDICATIONS OK WITH HANDLE DOWN. DUMPED FUEL, RETURNED FOR NORMAL LANDING. REMOVED AND REPLACED LEFT
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