N587FE
Service difficulty reports · 399
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 = 'N587FE' 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 = 'N587FE' 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 08FDEA03369Seat Track · corrodedMAIN DECK CARGO COMPARTMENT AT APPROXIMATELY STATION 1541, X = -8.5 FOUND SEAT TRACK FLANGE CORROSION. CABIN MAIN DECK CARGO COMPARTMENT SEAT TRACK REPAIRED FROM STA 1531 TO STA 1551, X = -8.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJSDR 08FDEA03368Stanchion · corrodedFORWARD CARGO COMPARTMENT FOUND AFT BULKHEAD LOCATION WITH LINERS SUPPORTING STANCHION X = -9 INCHES WITH CORROSION. FORWARD CARGO COMPARTMENT AFT BULKHEAD LOCATION WITH LINERS SUPPORTING STANCHION X = -9 INCHES CARRIED OUT REPAIR AS PER EA NR 1-5310-12241SDR 08FDEA03367Seat Track · corrodedMAIN DECK CARGO AT APPROXIMATELY STA 1641, X = 27.5 FOUND SEAT TRACK CORROSION. CABIN MAIN DECK CARGO SEAT TRACK REPAIRED FROM STA 1631 TO STA 1651, X = 27.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA03366Seat Track · corrodedMAIN DECK CARGO AT APPROXIMATELY STATION 5-73 TO 5-93, X = -27.5 FOUND SEAT TRACK CORROSION. CABIN MAIN DECK CARGO SEAT TRACK REPAIRED FROM STA 5-00 TO STA 5-123, X = -27.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA03365Seat Track · corrodedCABIN, MAIN DECK CARGO COMPARTMENT AT APPROXIMATELY STATION 1761 TO 1821, X = -8.50 FOUND SEAT TRACK CORROSION. CABIN MAIN DECK CARGO COMPARTMENT SEAT TRACK REPAIRED FROM STA 1761 TO STA 1831, X = -8.50 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIESDR 08FDEA03363Support Fitting · crackedDURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 FOUND WITH CRACK INDICATIONS AT HOLES NR A, NR B , NR C AND NR D. MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 FABRICATED AS PER FEDEX EA NR 1-530SDR 08FDEA03362Support Fitting · crackedDURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 5 FOUND WITH CRACK INDICATIONS AT HOLES NR A, NR B AND NR C. MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 5 FABRICATED AS PER FEDEX EA NR 1-5300-12240SDR 08FDEA03364Support Fitting · crackedDURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 FOUND WITH CRACK INDICATIONS AT HOLES NR A, NR B , NR C AND NR D. MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 FABRICATED AS PER EA NR 1-5300-122SDR 08FDEA03312Support Fitting · crackedDURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 4 FOUND WITH CRACK INDICATIONS AT HOLES A, C AND D. MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 4 FABRICATED AS PER FEDEX EA NR 1-5300-122409A. SUPPSDR 08FDEA03311Support Fitting · crackedDURING OPEN-HOLE INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 FOUND WITH CRACK INDICATIONS AT HOLES A, B, C AND D. MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 FABRICATED AS PER FEDEX EA NR 1-5300-122409A, SUPPORSDR 08FDEA03293Skin · chafedLEFT WING, FIXED LEADING EDGE TELESCOPE DUCT CUTOUT REPAIR DOUBLER AT XOS 467 FOUND CHAFFED. REMOVED DAMAGED REPAIR DOUBLER AS PER SRM 51-31-01 VOLUME II. FABRICATED NEW DOUBLER AND INSTALLED AT LEFT WING FIXED LEADING EDGE TELESCOPE DUCT CUTOUT AS PER SRM 5SDR 08FDEA03274Doubler · crackedCENTER LANDING GEAR WHEEL WELL RIGHT BULKHEAD FORWARD LOWER DOUBLER FOUND CRACKED. CRACKED DOUBLER REMOVED AND REPLACED WITH NEW PART AT CENTER LANDING GEAR WHEEL WELL RIGHT BULKHEAD FORWARD LOWER AREA AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MISDR 08FDEA03273Doubler · crackedCENTER LANDING GEAR WHEEL WELL LEFT BULKHEAD FORWARD LOWER DOUBLER FOUND CRACKED. CRACKED DOUBLER REMOVED AND REPLACED WITH NEW PART AT CENTER LANDING GEAR WHEEL WELL LEFT BULKHEAD FORWARD LOWER AREA AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOSDR 07FDEA05065Unknown · malfunctionedNR 2 ENG RPM LO ON CLIMB-OUT (FLAMEOUT). CREW REPORTED DURING CLIMB-OUT NR 2 ENG N1 WENT TO 11 PERCENT WITH N2 ALMOST 0 PERCENT, LOW EGT, AND FF APPROX 600 PPM. INSP NR 2 ENG INLET AND EXH FOR METAL PARTICLES AND FOD. NO DEFECTS NOTED. CHKD NR 2 ECU, NO SDR 07FDEA01508Seat Track · damagedCABIN SEAT TRACK CROWN AREA FOUND CHIPPED OFF AT STA 899 X = -47. CABIN SEAT TRACK AT STA 899 X= -47 CARRIED OUT REPAIR AS PER SRM 53-70-00 VOL I FIG 1. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.SDR 07FDEA01357Angle · crackedCABIN, RT WEB ANGLE FOUND CRACKED AT STA 1219 LONGERON 27. REPAIRED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA01356Longeron · crackedCABIN, RIGHT LONGERON 17 FOUND CRACKED AT STA 1239. [SUP 4-18-07] REMOVED AND REPLACED AS PER SRM 51-33- 01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA01355Longeron · crackedCABIN LEFT LONGERON 17 FOUND CRACKED AT STA 1239. 4-18-07, REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA01354Skin · dentedFORWARD CARGO DOOR AFT CUTOUT LOWER SKIN FOUND DENT AND CHAFED. CARRIED OUT REPAIR AS PER SRM 53-50-00 FIGURE 16 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA01353Skin · crackedLEFT WING DROOPED LEADING EDGE UPPER SURFACE FOUND CRACKED. [SUP 4-19-07] REMOVED AND REPLACED AS PER AMM 27-80-10. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA01299Seat Track · deformedCABIN SEAT TRACK AT STA 1485, X = 47 FOUND DEFORMED. 4-18-07, CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA01297Seat Track · crackedCABIN, SEAT TRACK CROWN AREA AT STA 755, X = -8 FOUND CRACKED. 4-18-07, CARRIED OUT REPAIR AS PER SRM 53-70- 00 VOLUME I. FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA01231Skin · corrodedRIGHT WING TIP LOWER SURFACE FOUND CORROSION. [SUP 4-19-07] REPAIRED AS PER FEDEX E.A. 1-5710-107829. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA01230Slat Track · crackedRIGHT WING FIXED LEADING EDGE NR 14 SLAT TRACK CUTOUT FOUND CRACKED. 4-18-07, REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA01214Trunnion · crackedNOSE LANDING GEAR RIGHT TRUNNION FITTING FOUND CRACKED. [SUP 4-18-07] REPAIRED AS PER SRM 53-40-00 FIGURE 22 VOLUME I AND FEDEX EA 1-5310-107815, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA01213Trunnion · crackedNOSE LANDING GEAR LEFT TRUNNION FITTING FOUND CRACKED. REPAIRED AS PER SRM 53-40- 00 FIGURE 22 VOLUME I AND FEDEX EA 1-5310-107816, REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.SDR 07FDEA01212Duct · crackedLEFT WING TOPSIDE FIXED LEADING EDGE AT TELESCOPING DUCT CUTOUT FOUND 2 SKIN CRACKS AT AFT CORNERS. [SUP 4-19-07] CRACKS AT LT WING TOPSIDE FIXED LEADING EDGE AT TELESCOPIC DUCT CUTOUT CORNERS REPAIRED AS PER SRM 57-10-00 FIGURE 42 VOLUME I. REPAIR CLASSIFIESDR 07FDEA01211Duct · crackedRIGHT WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT FOUND CRACKED. [SUP 4-19-07] CRACKED AT RIGHT HAND WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT REPAIRED AS PER SRM 57-10-00 FIGURE 42 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA2963Wire · burnedPDIS: LEVEL ONE CAC AIR FLO OFF ALERT DURING ENGINE START. MAINT FOUND SIGNIFICANT AMOUNT OF WIRES BURNED IN LWR FWD CARGO COMPARTMENT AFT RT CORNER IN CAC BLOWER AREA. FOUND SEVERAL BREAKERS POPPED IN THE COCKPIT. R&R 57 WIRES DESIGNATED C901.WRAPPED 19 WIRSDR 05FDEA03112Frame · dentedUPPER CARGO RIGHT SIDEWALL, FRAME AT STA 1561 INNER CHORD FOUND DENT AT LONGERON 12R TO LONGERON 13R. CARRIED OUT REPAIR AS PER SRM 53-30-00 FIGURE 1 VOLUME I DUE TO CAT B REPAIR. REFER TO FEDEX EA 1-5330-90040.SDR 05FDEA03110Access Panel · damagedRIGHT WING, LOWER FUEL TANK PANEL 638CB CUTOUT FASTENER HOLE FOUND ELONGATED. REPAIRED AS PER FEDEX EA 1-5710-90029.SDR 05FDEA03109Access Panel · damagedLEFT WING, UPPER FUEL TANK ACCESS PANEL 534BT CUTOUT FASTENER HOLE FOUND ELONGATED. REPAIRED AS PER FEDEX E.A. 1-5710-90037.SDR 05FDEA03108Floor Support · corrodedAFT CARGO, 02 CORROSION FOUND AT RIGHT CEILING FLOOR STRUCTURE AT STA 1921 TO STA 1941 X= -40.SDR 05FDEA03107Stringer · crackedCRACK INDICATION FOUND AT STRINGER END OF STRINGER 13, UPPER STRINGER, LEFT SIDE WING TANK. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I.SDR 05FDEA03106Stringer · crackedCRACK INDICATION FOUND AT STRINGER END OF STRINGER 14 (UPPER STRINGER), APPROXIMATE LENGTH 7 INCHES, RIGHT SIDE WING TANK. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I .SDR 05FDEA03105Stringer · crackedCRACK INDICATION FOUND AT STRINGER END OF STRINGER 12 (UPPER STRINGER), APPROXIMATE LENGTH 7 INCHES, RIGHT SIDE WING TANK. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I.SDR 05FDEA03068Stringer · crackedCRACK INDICATION FOUND AT STRINGER END OF STRINGER 16 (UPPER STRINGER), APPROXIMATE LENGTH 17 INCHES, RIGHT SIDE WING TANK. CRACK PROPAGATES TOWARDS INBOARD TO THE NEAREST WEB. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I AND CLIP REMOVED AND REPLACSDR 05FDEA03067Stringer · crackedCRACK INDICATION FOUND AT STRINGER END OF STRINGER 10 (UPPER STRINGER), APPROXIMATE LENGTH 11.5 INCHES, LEFT SIDE WING TANK. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I.SDR 05FDEA03043Longeron · corrodedCENTER CARGO, LONGERON CORROSION FOUND AT STA 1701 R50. REMOVED AS PER SRM 51-21-01 VOLUME II.SDR 05FDEA03042Longeron · corrodedCENTER CARGO, LONGERON CORROSION FOUND AT STA 1701 L50. REPAIR AS PER SRM 53-10-00 FIGURE 2 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 05FDEA03041Seat Track · corrodedUPPER CARGO, SEAT TRACK LBL 8 CORRODED AT STA 1551. SEAT TRACK REPAIRED AS PER SRM 53-70-00 VOLUME I FIGURE 1. CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100.SDR 05FDEA03022Seat Track · corrodedUPPER CARGO, SEAT TRACK RBL 77 CORRODED AT STATION 1350. SEAT TRACK REPAIRED AS PER SRM 53-70-00 VOLUME I FIGURE 1. CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100.SDR 04FDEA02046Bracket · corrodedCOMPLY EA 1-5750-78010 OUTBOARD TRAILING EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) CORROSION REPAIR. OUTBOARD TRAILING EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) CORROSION REPAIR HAS BEEN COMPLIED.SDR 04FDEA02045Structure · damagedCOMPLY WITH EA 1-5510-76669 HORIZONTAL STABILIZER BARREL NUTS REWORK PER SB MD11 55-023 REV 1 AND FEDEX EO 1-5510-7-5000. HORIZONTAL STABILIZER BARREL NUTS REWORK PER SB MD11 55-023 REV 1 AND FEDEX EO 1-5510-7-5000' HAS BEEN COMPLIED.SDR 04FDEA01971Wire · burnedMAIN DECK CABIN AT STA 775 (RT) WIRE NR`S. C029-1-6AL, C029-2-6AL AND C029-3-6AL FND BURNT. GVI ON THE BURNT WIRES SURROUNDING AREAS,CONDUCTIVITY INSP PER DAC NDT SPM PART 06-10-01-001 REV11 ON M/D STA 775R FRAME/SKIN FND ACCEPTABLE RANGE. BURNT CABLES, REPASDR 04FDEA01868Stop Fitting · crackedLEFT HAND WING OUTBOARD FLAP STOP FITTING CRACKED. LEFT HAND WING - OUTBOARD FLAP REMOVED AND REPLACED AS PER AMM 27-50-30 AND ADJUSTMENT CARRIED OUT AS PER AMM 27-50-00, FOUND SATISFACTORY.SDR 04FDEA01867Stop Fitting · crackedRIGHT HAND WING OUTBOARD FLAP STOP FITTING CRACKED. RIGHT HAND WING - OUTBOARD FLAP CRACKED STOP FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL I.SDR 04FDEA01856Structure · corrodedEMPENNAGE HORIZONTAL STABILIZER RIGHT HAND BARREL NUT NR 35R SIDEWALL CORROSION BLENDED OUT FOUND EXCEEDED LIMIT. EMPENNAGE HORIZONTAL STABILIZER RIGHT HAND NR 35R BARREL NUT BORE REPAIRED AS PER FEDEX EA 1-5510-78027. HORIZONTAL STABILIZER BARREL NUT BORE NSDR 04FDEA01855Spar Cap · corrodedLEFT HAND HORIZONTAL STABILIZER NR 36L FOUND WITH CORROSION BEARING, SIDEWALL AND BOTTOM. CORROSION CLEAN-UP AND FOUND EXCEEDED LIMIT AS PER SB MD11 55-023. HORIZONTAL STABILIZER NR 36L BARREL NUT BORE REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-78026. HORIZOSDR 04FDEA01850Fitting · wornRIGHT HAND WING - INBOARD FLAP VANE, OUTBOARD TEE FITTING MID AND AFT HOLES FOUND WORN. RIGHT HAND WING - INBOARD FLAP VANE, OUTBOARD TEE FITTING REMOVED & REPLACED AS PER EO 1-5750-7-5005 PT2 TITLE : WINGS - TRAILING EDGE DEVICES - INSPECT/MODIFY I/B FLAP VA
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