N575FE
Service difficulty reports · 416
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 = 'N575FE' 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 = 'N575FE' 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 05FDEA01895Splice · damagedCENTER CARGO BAY RT STA 5-113, LONGERON 44 SPLICE FITTING FOUND WITH EXISTING ENLONGATED HOLE AFTER REMOVAL SPLICE FITTING. REMOVED AND REPLACED NEW SPLICE FITTING AS PER SRM 51-33-01 VOL. II. MINOR REPAIR AS GMM 6-2-100.SDR 05FDEA01894Hinge · corrodedLT WING O/B FLAP O/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PG 402-407. REPAIR CARRIED OUT AS PER CMM 57-44-09.SDR 05FDEA01890Hinge · corrodedLT WING, O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. REPAIRED AS PER CMM 57-44-09 P402-407 AND EA 1-5750-87592A.SDR 05FDEA01889Hinge · corrodedLT WING, O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. REPAIRED AS PER EA1-5750-87592A.SDR 05FDEA01888Stringer · damagedAFT CARGO BAY AT STA 1967, AFT CENTER CEILING TOP STRINGER ASSY FOUND DAMAGED AS MARKED. DAMAGED FLOOR SUPPORT REMOVED. NEW FLOOR SUPPORT REWORKED FROM S2922781- 1X2024T42 AS PER DWG ACA 7149 AND INSTALLED AS PER SRM 51-31-01 VOL.II. CLASSIFIED MINOR REPAISDR 05FDEA01887Bracket · corrodedAFT CARGO BAY STA 1841 LOWER FRAME FWD FLOOR PANEL SUPPORTING BRACKET FOUND CORRODED AS MARKED. AFT CARGO COMPARTMENT, STA 1841 LOWER FRAME FWD FLOOR PANEL SUPPORTING BRACKET REMOVED AS PER SRM 51-33-01 VOL II. NEW STIFFENER FABRICATED AS PER DRAWING AGA SDR 05FDEA01886Hinge · corrodedRT WING, O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. REPAIRED AS PER EA1-5750-87591.SDR 05FDEA01885Hinge · corrodedRT WING, O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. REMOVED IAW CMM 20-11-02. FABRICATED BUSHING AND INSTALLED IAW EA1-5750-87591.SDR 05FDEA01884Hinge · corrodedRT WING, O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT ASPER EA1-5750-87591.SDR 05FDEA01883Hinge · corrodedRT WING, O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. REPAIRED AS PER EA1-5750-87591.SDR 05FDEA01882Hinge · corrodedRT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. REPAIRED AS PER EA1-5750-87591.SDR 05FDEA01881Hinge · corrodedRT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. REPAIRED AS PER EA1-5750-87591.SDR 05FDEA01880Hinge · corrodedRT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. REPAIRED AS PER EA1-5750-87591.SDR 05FDEA01879Hinge · corrodedRT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. REPAIRED AS PER EA1-5750-87591.SDR 05FDEA01878Hinge · corrodedRT WING, O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. REPAIRED AS PER EA1-5750-87590.SDR 05FDEA01877Hinge · corrodedRT WING, O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. REPAIRED AS PER EA1-5750-87590.SDR 05FDEA01876Hinge · corrodedRT WIN, O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. REPAIRED AS PER EA1-5750-87590.SDR 05FDEA01875Hinge · corrodedRT WING, O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. REPAIRED AS PER EA1-5750-87590. SDR 05FDEA01874Hinge · corrodedRT WING, O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. REPAIRED AS PER EA1-5750-87590.SDR 05FDEA01873Hinge · corrodedRT WING, O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED IAW CMM 20-11-02. FABRICATED BUSHING AND INSTALLED AS PER EA1-5750-87590.SDR 05FDEA01872Hinge · corrodedRT WING, O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. REPAIR CARRIED OUT AS PER EA1-5750-87590.SDR 05FDEA01871Hinge · corrodedRT WING, O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT I/B BORE FOUND CORRODED.SDR 05FDEA01841Skin · damagedRT WING I/B AILERON BOTTOM SURFACE HAS MULTIPLE SHARP ABRASIONS. SDR 05FDEA01840Hinge · corrodedLT WING - O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. REPAIR CARRIED OUT AS PER EA 1-5750-87588.SDR 05FDEA01839Hinge · corrodedLT WING - O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87588.SDR 05FDEA01838Hinge · corrodedLT WING - O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. CORROSION REPAIRED AS PER CMM 20-11-02 AND EA 1-5750- 87588.SDR 05FDEA01837Hinge · corrodedLT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. REPAIR CARRIED OUT AS PER EA 1-5750-87588.SDR 05FDEA01836Structure · corrodedLT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED.SDR 05FDEA01835Structure · corrodedLT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87588.SDR 05FDEA01834Structure · corrodedLT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED.SDR 05FDEA01833Structure · corrodedLT WING, O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. FABRICATED BUSHING AND INSTALLED A PER EA 1-5750-87588.SDR 05FDEA01831Structure · corrodedLT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. REPAIRED AS PER EA1-5750-87587.SDR 05FDEA01829Structure · corrodedLT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. REPAIRED AS PER EA1-5750-87587.SDR 05FDEA01827Structure · corrodedLT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. SUPPORT BRACKET REPAIRED AS PER EA1-5750-87587 LT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.SDR 05FDEA01825Structure · corrodedLT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. SUPPORT BRACKET REPAIRED AS PER EA1-5750-87587 LT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.SDR 05FDEA01823Structure · corrodedLT WING, O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. REPAIR CARRIED OUT AS PER EA1-5750-87587.SDR 05FDEA01821Structure · corrodedLT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. FABRICATED BUSHING AND INSTALLED AS PER EA1-5750-87587.SDR 05FDEA01820Structure · corrodedLT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. REPAIR CARRIED OUT AS PER EA1-5750-87587.SDR 05FDEA01819Structure · corrodedLT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. FABRICATED BUSHING AND INSTALLED AS PER EA1-5750-87587.SDR 05FDEA01816Stiffener · corrodedCABIN OVERWING EXTERIOR STIFFENER FOR UPPER AUX TANK FOUND CORRODED AT STA 1339 RBL 98 AS MARKED. REMOVED AS PER SRM 51-31-01 VOL.II AND NEW STIFFENER INSTALLED AS PER DRAWING APB 7242.NEW STIFFENER REWORKED PER DWG 7242. REPAIR CLASSIFIED AS MAJOR PER GMM 6SDR 05FDEA01815Stiffener · corrodedOVERWING EXTERIOR STIFFENER FOR UPPER AUX TANK FOUND CORRODED AT STA 1332 RBL 98 AS MARKED. CORRODED STIFFENER REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II.SDR 05FDEA01814Stiffener · corrodedOVERWING STIFFENER FOR UPPER AUX TANK FOUND CORRODED AT STA 1352 RBL 98 AS MARKED. REMOVED AS PER SRM 51-31-01 VOL.II AND NEW STIFFENER REPLACED PER DWG APB7242. NEW STIFFENER REWORKED PER DWG APB7242. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. [CLOSED]SDR 05FDEA01813Stiffener · corrodedOVERWING EXTERIOR STIFFENER FOR UPPER AUX TANK FOUND CORRODED AT STA 1345 RBL 98 AS MARKED. REMOVED AND INSTALLED AS PER SRM 52-57-12.SDR 05FDEA01812Seat Track · corrodedSTA 912 RBL 8.5 SEAT TRACK BASE FOUND CORRODED. (OPEN)SDR 05FDEA01811Support · corrodedCABIN AT STA 1834 LBL 36.25 LAVATORY MOUNTING SUPPORT STRUCTURE AT TOP FOUND CORRODED. (OPEN)SDR 05FDEA01810Longeron · corrodedCENTER CARGO BAY, RT STA 1641 AFT LONGERON 44 FOUND WITH CORROSION AS MARKED. FABRICATED AS PER DWG AFA7127 AND SPICED REPAIR AS PER SRM 53-10-00 VOL1 FIG1. [CLOSED]SDR 05FDEA01809Skin · canningVERTICAL STABILIZER HAS OIL CANNING ON SKIN JUST ABOVE 373BR. RIGHT I/B FLAP UPPER SKIN BETWEEN 140.6 TO 147.3, 03 EACH EXISTING DENTS SMOOTHENED OUT AND REPROTECTED AS PER SRM 51-21-01 VOL II, DEEPEST DENT IS 0.025", DIAMETER: 1/2" FOUND WITHIN LIMIT AS SDR 05FDEA01808Skin · canningVERTICAL STABILIZER HAS OIL CANNING ON SKIN JUST ABOVE 373BL. REPAIR DOUBLER INSTALLED IAW SRM 51-35-01. [CLOSED]SDR 05FDEA01790Floor Support · corrodedSTA 1909 TO STA 2007 LBL 60 ALONG FLOOR SUPPORT STRUCTURE FOUND CORRODED. FLOOR SUPPORT REWORKED IAW DWG AGA7496 AND INSTALLED IAW SRM 51-31-01.SDR 05FDEA01789Floor Support · crackedFLOOR SUPPORT FOUND CRACKED AT STA 5-11 AT RBL 69 AS MARKED. CORRECTIVE ACTION: SNRM N1342: DISPREPANT FLOOR SUPPORT REMOVED AS PER SRM 51-31-01 VOL II. NEW FLOOR SUPPORT REWORKED FROM S2932222T12000 AS PER DRAWING ACA 3762 AND INSTALLLED AS PER SRM 51-
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