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 04FDEA01792Frame · dentedMAIN DECK FRAME FOUND DENT AT STA 535 LONGERON L19-24.SDR 04FDEA01791Seat Track · wornMAIN DECK SEAT TRACK FOUND WORN AT STA 699 LBL 47 INCHES.SDR 04FDEA01790Hinge · corrodedRIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK SPOTFACE FOUND CORRODED.SDR 04FDEA01789Hinge · corrodedRIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), LOWER MOUNTING INBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PG 402-407 ORIG THK 0.52 MATERIAL REMOVED 0.033 REMAINING THICKNESS 0.487 & FOUND WITHIN LIMITS AS PER DWG TOLERASDR 04FDEA01788Hinge · corrodedRIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER =1.187, FINAL DIAMETER=1.221 AND REPAIRED AS PER FSDR 04FDEA01787Hinge · corrodedRIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.221 AND REPAIRED AS PER FEDESDR 04FDEA01786Hinge · corrodedRIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK SPOTFACE FOUND CORRODED.SDR 04FDEA01785Hinge · corrodedRIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), LOWER MOUNTING OUTBOARD BOLT HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=0.516, FINAL DIAMETER=0.596 AND REPAIRED AS PER SDR 04FDEA01784Hinge · corrodedRIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), LOWER MOUNTING INBOARD BOLT HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=0.516, FINAL DIAMETER=0.596 AND REPAIRED AS PER FESDR 04FDEA01783Hinge · corrodedRIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.221 AND REPAIRED AS PER FESDR 04FDEA01782Hinge · corrodedRIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.225 AND REPAIRED AS PER FEDSDR 04FDEA01778Structure · corrodedLEFT HAND WING LOWER WINGLET WING SIDE - AFT INTERNAL MOUNT BOLT HOLE AREAS HAVE MINOR SURFACE CORROSION.SDR 04FDEA01777Seat Track · crackedMAIN DECK SEAT TRACK FOUND CRACKED AT STA 905 RT 28. REMOVED AND REPAIRED IAW SRM 53-70-00 FIG 1 VOL I.SDR 04FDEA01769Seat Track · wornMAIN DECK SEAT TRACK FOUND WORN AT STA 792 RIGHT 48 INCHES.SDR 04FDEA01763Fitting · crackedCENTER CARGO COMPARTMENT BILGE AREA, RIGHT HAND LONGERON 49 SPLICE FITTING BETWEEN STA 5-113 AND STA 1541 FOUND CRACKED.SDR 04FDEA01762Fitting · crackedCENTER CARGO COMPARTMENT BILGE AREA, RIGHT HAND LONGERON 45 SPLICE FITTING BETWEEN STA 5-113 AND STA 1541 FOUND CRACKED.SDR 04FDEA01761Fitting · crackedCENTER CARGO COMPARTMENT BILGE AREA, RIGHT HAND LONGERON 44 SPLICE FITTING BETWEEN STA 5-113 AND STA 1541 FOUND CRACKED.SDR 04FDEA01760Fitting · crackedCENTER CARGO COMPARTMENT BILGE AREA, LEFT HAND LONGERON 51 SPLICE FITTING BETWEEN STA 5-113 AND STA 1541 SUSPECT CRACKED.SDR 04FDEA01759Seat Track · corrodedMAIN DECK SEAT TRACK AT R1 DOOR WAY FOUND CORRODED.SDR 04FDEA01758Seat Track · wornMAIN DECK - SEAT TRACK FOUND WORN AT STA 492 RT 63.SDR 04FDEA01757Seat Track · wornMAIN DECK SEAT TRACK FOUND WORN AT STA 492 RIGHT 63.SDR 04FDEA01756Hinge · corrodedLT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-52-03 PAGES 442 TO 443 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.328 AND REPAIRED AS PER FEDEX EA 1-5750- 7677SDR 04FDEA01754Hinge · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR OUTBOARD HOLE SPOTFACE FOUND CORRODED.SDR 04FDEA01753Hinge · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR INBOARD SPOTFACE FOUND CORRODED.SDR 04FDEA01752Hinge · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR OUTBOARD BORE FOUND CORRODED.SDR 04FDEA01751Hinge · corrodedLEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR INBOARD BORE FOUND CORRODED.SDR 04FDEA01750Hinge · corrodedLEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE SPOTFACE FOUND CORRODED.SDR 04FDEA01749Hinge · corrodedLEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE BORE FOUND CORRODED.SDR 04FDEA01748Hinge · corrodedLEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE FOUND CORRODED.SDR 04FDEA01747Hinge · corrodedLEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE BORE FOUND CORRODED.SDR 04FDEA01755Hinge · corrodedLT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-52-03 PAGES 442 TO 443 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187", FINAL DIAMETER=1.255 AND REPAIRED AS PER FEDEX EA 1-5750- 76775SDR 04FDEA01735Seat Track · corrodedFOUND MAIN DECK SEAT TRACK CORROSION AT STA 460 LEFT HAND MOST OUTBOARD. MAIN DECK SEAT TRACK FOUND CORROSION AT STA 460 LEFT HAND MOST OUTBOARD REMOVED AS PER SRM 51-31-01 VOL 2 AND SRM 51-33-01 VOL 2. THE CORROSION REMOVED AS PER SRM 51-21-01 VOL 2 AND FSDR 04FDEA01736Seat Track · corrodedMAIN DECK SEAT TRACK FOUND CORROSION AT STA 5-113 LEFT HAND 8 INCHES.SDR 04FDEA01708Seat Track · crackedSEAT TRACK FOUND CRACKED AT STA 792 RIGHT 28 INCHES. REPAIRED AS PER SRM 53-70-00 FIG 1 VOL 1 AND CRACK FREE ON CUT OUT AREA BY NDT INAPECTION.SDR 04FDEA00914Smoke Detector · malfunctionedAT 200 FT AGL ON LANDING GOT CABIN SMOKE LEVEL 3 ALERT, WENT OUT SHORTLY. ALERT ON DURING LANDING ROLL THEN WENT OUT. EMERGENCY DECLARED. ON TAXI, CABIN SMOKE LEVEL 3 ALERT, STEADY. APU RUNNING, ENGINE SHUTDOWN. F/O WENT BACK TO OPEN DOOR, SMELLED SMOKE. SDR 04FDEA00886Smoke · detectedAT 200 FT AGL ON LANDING IN SFS, GOT A CABIN SMOKE LVL 3 ALERT, IT WENT OUT SHORTLY. ALERT ON AGAIN DURING LANDING ROLL, THEN OUT. EMERGENCY DECLARED. ON TAXI IN, CABIN SMOKE LEVEL 3 ALERT ON STEADY. APU RUNNING. ENGINE SHUTDOWN. F/O SMELLED SMOKE. EMERSDR 03FDEA01047Trim Motor · contaminatedUPON APPLICATION OF POWER UP FOR TAKEOFF THE STABILIZER MOVED FROM 7.3 TO 5.4. AFTER REJECTED TAKEOFF WHILE ON TAXIWAY STABILIZER, RESET TO 7.3. UPON SUBSEQUENCY TAXI THE STAB MOVED BY ITSELF TO 9.2 AND THEN BACK TO ABOUT 5. T/S AND FOUND NR 2 TRIM MOTOR C/SDR 02FDEA00904Support · crackedRT WING LE SUPPORT LOCATED ON NR 16 SLAT TRACK AT XOS 1005.124. FOUND WITH CRACK APPROX. 1 INCH IN LENGTH. CRACKED SUPPORT RIB ON RT WING LE LOCATED ON NR 16 SLAT TRACK AT XOS 1005.124 REMOVED AND REPLACED AS PER SRM 51-31-01, VOL. II.SDR 02FDEA00875Support · crackedLT WING L/E WING SUPPORT FOUND CRACKED AT NR 16 SLAT TRACK.SDR 02FDEA00074Tailpipe · fireAFTER BLOCK IN & ENGINE SHUTDOWN, NR 2 ENGINE TAILPIPE ON FIRE. R&R APU NR 1 FIRE BOTTLE PER MM 26-21-01-4.SDR 01FDEA00894Support · corrodedCORROSION ON FLOORBOARD HAT SECTION SUPPORT AT BS 457 X=+76 IN AT FWD CABIN. REMOVED AND REPLACED FLOORBOARD PER SRM 51-31-01 VOL II.SDR 01FDEA00459Actuator · out of adjA/C MADE AIR TURNBACK DUE DEFLECT AILERON DISAGREE ALERT. LT O/B ACTUATOR ADJUSTED AND SAFETIED PER MXP 27-2 METHOD "D".SDR 00FDEA00665Seat Track · crackedMAIN DECK (BALL MAT AREA) RIGHT BS 635, RBL 8.5 SEAT TRACK FOUND CRACKED. *S/D* REMOVED PER 53-70-00 FIG 1, VOL I & 51-33-01 VOL II. FLOOR PNL 232FF & 233EF REMOVED FOR ACCESS AND REINSTALL PER MM 53-21-04-4.SDR 00FDEA00664Seat Track · crackedMAIN DECK (BALL MAT AREA) - LEFT BS 635, LBL 8.K, SEAT TRACK FOUND CRACKED. *S/D* REMOVED AND REPLACED PER SRM 53-70-00 FIG 1, VOL I & 51-33-01 VOL II. FLOOR PANEL 233EF & 233FF REMOVED FOR ACCESS AND REINSTALLED PER 53-21-04-4.SDR 00FDEA00557Flap · malfunctionedDURING T/O, FLAP RETRACT AIL DEFLECT DISAG LEVEL 2 ALERT SHOW BOTH DEFLECTED.SDR 99FDEA00261Seat Track · crackedMAIN DECK AREA - CRACK FOUND ON SEAT TRACK AT STA 635 X = 47.5 LT. CRACK LENGTH APPROX 3.85 IN. *S/D* CRACK AREA TRIMMED OUT AT STA 625 & 645. NEW TRACK REWORKED PER DWG NR NCA 6792. SPLICE HATS REWORK AND SPLICE PLATES FAB AND WEB INSTALLED PER SRM 53-70SDR 98FDEA00431Line · leaking98-0169 - STA-HKG - APPROX 1.5 HR INTO FLT HYD 1 OFF LEVEL 2 ALERT ILLUMINATED WITH HYD 1 RESERVOIR INDICATING 2.8 GAL RESERVOIR QTY CONT TO DROP UNTIL HYD 1 FAIL LEVEL 2 ALERT ILLUM WITH QUAN INDICATING 1 GAL RESERVOIR CONT DECREASE UNTIL REACH ZERO. ON ARRSDR 97FDEA00233Valve Controller · malfunctionAT FLIGHT LEVEL OF 24,000 FEET AND DESCENDING A LEVEL 2 ALERT TANK 2 PUMPS OFF ILLUMINATED. THE FUEL SYSTEM CONTROLLER WAS IN AUTO AT THE TIME. SWITCHED THE SYSTEM TO MANUAL TO TRY TO TURN THE PUMPS ON AND AT THIS TIME THE NR 2 ENGINE FLAMED OUT. ACCOMPLISHSDR 97FDEA00232Control Unit · failedLEVEL 2 FUEL QUANTITY USED CHECK ALERT ILLUMINATED APPROXIMATELY 25 MINUTES INTO FLIGHT. ACCOMPLISHED THE CHECK LIST, THEN RAN FUEL SYSTEM IN MANUAL WITH NO APPARENT LOSS OF FUEL FOR APPROXIMATELY 30 MINUTES. RETURNED SYSTEM TO AUTO AND OBSERVED ABNORMAL DE
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