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 FDEA201005041432Seat Track · crackedCRACKED (APPROX 3 INCH) - SEAT TRACK STA635, X =27.5 AT MAIN DECK CARGO FLOOR. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 625 TO STA 665 X= 27.5 IAW SRM 53-00-52, FIG 201 REPAIR 1, REV 43. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.SDR FDEA201005011422Seat Track · corrodedCORROSION - CABIN FLOOR SEAT TRACK, STA 2007, X = 47", IN AFT CARGO WASTE TANK COMPARTMENT CEILING. REPAIRED IAW SRM 53-00-52 FIG. 201 REPAIR 1, REV 43 AND EA 1-5310-138498. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.SDR FDEA201005011421Seat Track · corrodedCORROSION - CABIN FLOOR SEAT TRACK, STA 2007, X = -47", IN AFT CARGO WASTE TANK COMPARTMENT CEILING. REPAIRED AS IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 43 AND EA 1-5310-138498. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.SDR FDEA200909163311Valve · failedWHEN WING AND TAIL ANTI-ICE SELECTED RECEIVED BLEED AIR 1 OFF, BLEED AIR 2 OFF, PACK 1 OFF, PACK 2 OFF ALERTS. THEY TRIED ESC IN MAN AND SWAPPING CONTROLLERS - NO HELP. NR 2 BLEED AIR WOULD SHUT DOWN FIRST FOLLOWED BY NR 1 BLEED APPROX 30 SEC LATER. SELECTSDR 08FDEA04895Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE) SIDE LOAD MOUNT SURFACE FOUND CORROSION. CORROSIONS REMOVED ON SIDE LOAD MOUNT AT LT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) AND FOUND WITHIN LIMIT AS PER EA 1-5750-122634, REPAIR CLASSIFIED AS MINOR RESDR 08FDEA04894Hinge Bracket · corrodedRIGHT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE) SIDE LOAD MOUNTING SURFACE FOUND CORRODED. CORROSION REMOVED ON SIDE LOAD MOUNTING SURFACE AT RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) AND FOUND WITHIN LIMIT AS PER CMM 57-44-08. EXISTING THICKNESSDR 08FDEA04827Seat Track · corrodedUPON REMOVAL OF FLOOR PANEL FOR AUX TANK UPPER SURFACE CORROSION REMOVAL ACCESS FOUND SEAT TRACK AT STATION 1184, X=-75 CORRODED.SDR 08FDEA04826Seat Track · corrodedUPON REMOVAL OF FLOOR PANEL FOR AUX TANK UPPER SURFACE CORROSION REMOVAL ACCESS FOUND SEAT TRACK ATTACHMENT HOLE AT STATION 1219, X=-75 CORRODED.SDR 08FDEA04781Support Fitting · crackedEMPENNAGE, AFT FUSELAGE COMPARTMENT PRESSURE BULKHEAD UPPER AFT SURFACE QUANTITY 01 SUPPORT FITTING AT STATION 2007, X=-31.930 FOUND CRACKED.SDR 08FDEA04780Skin · chafedRIGHT WING, NR 3 LEADING EDGE SLAT TELESCOPIC DUCT CUTOUT REPAIR DOUBLER INBOARD AND OUTBOARD SIDE LEADING EDGE SURFACE FOUND CHAFING. CHAFE MARK SMOOTHED AS PER SRM 51-21-01, VOLUME II AND REPAIR CARRIED OUT AS PER EA 1-5740-122632. REPAIR CLASSIFIED AS MSDR 08FDEA04779Skin · chafedLEFT WING, NR 3 LEADING EDGE SLAT TELESCOPIC DUCT CUTOUT REPAIR DOUBLER INBOARD AND OUTBOARD SIDE LEADING EDGE SURFACE FOUND CHAFING. CHAFE MARK SMOOTHED AS PER SRM 51-21-01, VOLUME II AND REPAIR CARRIED OUT AS PER EA 1-5740-122631. REPAIR CLASSIFIED AS SDR 08FDEA04778Stiffener · crackedEMPENNAGE, AFT FUSELAGE COMPARTMENT PRESSURE BULKHEAD AFT SURFACE VERTICAL STIFFENER AT STATION 2007, X=-15.250 FOUND CRACKED AT UPPER CORNER AREA.SDR 08FDEA04726Support 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 A, B AND D. REMOVED AND REPLACED AS PER SRM 51-33-01, VOLUME II. BUSHING REPAIR AT BOLT HOLES CARRIED OUT AS SDR 08FDEA04725Support 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 B AND D. CARRIED OUT BUSHING REPAIR AS PER SRM 53-50- 00, FIGURE 10, VOLUME I. REPAIR CLASSIFIED MAJOR AS PSDR 08FDEA04723Support Fitting · crackedDURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 5 FOUND WITH CRACK INDICATION AT HOLE D. CARRIED OUT BUSHING REPAIR AS PER SRM 53-50- 00, FIGURE 10, VOLUME I. REAPIR CLASSIFIED MAJOR AS PER GMM 6SDR 08FDEA04722Support Fitting · crackedDURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 4 FOUND WITH CRACK INDICATION AT HOLE C. CARRIED OUT BUSHING REPAIR AS PER SRM 53- 50-00, FIGURE 10, VOLUME I. REPAIR CLASSIFIED MAJOR AS PER GMM 6SDR 08FDEA04720Support Fitting · crackedDURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 FOUND WITH CRACK INDICATIONS AT HOLES C AND D. CARRIED OUT REPAIR AS PER SRM 53-50-00, VOLUME I, FIGURE 10. REPAIR CLASSIFIED MAJOR AS PER GMM 6-SDR 08FDEA04719Support Fitting · crackedDURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 2 FOUND WITH CRACK INDICATIONS AT HOLES A, B, C AND D. REMOVED AND REPLACED AS PER SRM 51-33-01, VOLUME II. BUSHING REPAIR CARRIED OUT AT BOLT HOLESSDR 08FDEA04717Fitting · crackedDURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 1 FOUND WITH CRACK INDICATIONS AT HOLES A, B AND D. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. BUSHING REPAIR CARRIED OUT AT BOLT HOLES AS SDR 07FDEA03057Unknown · unknownAT CRUISE FL340 MOMENTARY ENGINE FIRE INDICATION ON ENGINE ONE. NO OTHER ENGINE INDICATIONS OF FIRE. RETARDED THROTTLE TO IDLE. REMAINED AT IDLE FOR DIVERT TO LAX. CHECKED RESISTANCE FOR LOOP B AND WAS GOOD, IAW FIM 26-11. FOUND SEVERAL CLAMPS WITH OUTSDR 07FDEA02371Skin · dentedRIGHT WING I/B FLAP LOWER SURFACE FOUND DENT. REPAIR CARRIED OUT AT RIGHT HAND WING I/B FLAP LOWER SURFACE AS PER SRM 57-10-00 FIGURE 38 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 07FDEA02345Frame · dentedMAIN DECK CARGO, RIGHT FRAME 1701 AT STRINGER L12 FOUND DENT. REPAIR CARRIED OUT AT MAIN DECK CARGO, RIGHT FRAME 1701 AT STRINGER L12 AS PER SRM 53-30-00 FIGURE I VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 07FDEA02344Frame · dentedMAIN DECK CARGO, RIGHT FRAME 1681 AT STRINGER L12 FOUND DENT. REPAIR CARRIED OUT AT MAIN DECK CARGO, RIGHT FRAME 1681 AT STRINGER L12 AS PER SRM 53-30-00 FIGURE I VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 07FDEA02343Frame · dentedMAIN DECK CARGO, RIGHT FRAME 1661 AT STRINGER L12 FOUND DENT. REPAIR CARRIED OUT AT MAIN DECK CARGO, RIGHT FRAME 1661 AT STRINGER L12 AS PER SRM 53-30-00 FIGURE I VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 07FDEA02342Frame · dentedMAIN DECK CARGO, RIGHT FRAME 1641 AT STRINGER L12 FOUND DENT. REPAIR CARRIED OUT AT MAIN DECK CARGO, RIGHT FRAME 1641 AT STRINGER L12 AS PER SRM 53-30-00 FIGURE I VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 07FDEA02322Trunnion · corrodedCTR LANDING GEAR, RT TRUNNION FITTING FWD HOLE FOUND CORRODED. [07-10-07] COMPLIED WITH FEDEX E.A. 1-5310-112350, CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.SDR 07FDEA02321Trunnion · corrodedCTR LANDING GEAR, RT TRUNNION FITTING AFT HOLE FOUND CORRODED. [07-10-07] COMPLIED WITH FEDEX E.A. 1-5310-112350, CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.SDR 07FDEA02320Trunnion · corrodedCTR LANDING GEAR, RT TRUNNION FITTING ALIGNMENT HOLE FOUND CORRODED. [07-10-07] REMOVED AND FOUND WITHIN LIMITS AS PER SRM 53-40-00 FIG. 16 VOL.I. ORIGINAL HOLE DIAMETER: 1.500"; REWORKED HOLE TO 1.6664". MAXIMUM HOLE DIAMETER: 1.680". BUSHING FABRISDR 07FDEA02319Trunnion · corrodedCTR LANDING GEAR, RT TRUNNION FITTING MATING SURFACE FOUND CORRODED. [07-10-07] REMOVED AND FOUND WITHIN LIMITS AS PER SRM 53-40-00 FIG. 16 VOL.I. FWD LUG - ORIGINAL THICKNESS: 2.505"; MATERIAL REMOVED: 0.040" REMAINING THICKNESS: 2.465"; MIN. ALLOWABSDR 07FDEA02318Trunnion · corrodedCTR LANDING GEAR, LT TRUNNION FITTING ALIGNMENT HOLE FOUND CORRODED AFTER PILLOW BLOCK REMOVAL. [07-10-07] REMOVED AND FOUND WITHIN LIMITS AS PER SRM 53-40-00 FIG. 16 VOL I. ORIGINAL HOLE DIAMETER: 1.500"; REWORKED HOLE TO 1.666". MAXIMUM HOLE DIAMETERSDR 07FDEA02317Trunnion · corrodedCTR LANDING GEAR, LT TRUNNION FITTING MATING SURFACE FOUND CORRODED AFTER PILLOW BLOCK REMOVAL. [07-10-07] REMOVED AND FOUND WITHIN LIMITS AS PER SRM 53-40-00 FIG. 16 VOL.I. FWD SIDE - ORIGINAL THICKNESS: 2.536"; MATERIAL REMOVED: 0.044" REMAINING THICSDR 07FDEA02316Trunnion · corrodedCTR LANDING GEAR, LT TRUNNION FITTING FWD HOLE FOUND CORRODED. [07-10-07] REMOVED AND FOUND WITHIN LIMITS AS PER SRM 53-40-00 FIG. 16 VOL.I. ORIGINAL HOLE DIAMETER: 1.341"; REWORKED HOLE TO 1.379". MAXIMUM HOLE DIAMETER: 1.385". BUSHING FABRICATED AND INSTSDR 07FDEA02315Trunnion · corrodedCTR LANDING GEAR, LT TRUNNION FITTING AFT HOLE FOUND CORRODED. [07-10-07] COMPLIED WITH FEDEX E.A. 1-5310-112351. CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.SDR 07FDEA02270Duct · crackedRIGHT WING LEADING EDGE PANEL NEAR TELESCOPING DUCT AREA FOUND CRACKED.SDR 07FDEA02269Hinge · crackedLANDING GEAR, FLIPPER DOOR OUTBOARD EDGE ADJACENT TO FORWARD HINGE FOUND CRACKED. [07-16-07] REPAIR CARRIED OUT AT LANDING GEAR - RT FLIPPER DOOR OUTBOARD EDGE ADJACENT TO FORWARD HINGE AS PER SRM 52-10-00 FIGURE 18 VOLUME I. REPAIR CLASSIFIED AS MINOR AS SDR 07FDEA02268Structure · crackedLANDING GEAR, LT MLG FLIPPER DOOR, FWD EDGE FOUND CRACKED. [07-13-07] REPAIR CARRIED OUT AT MLG - LT MLG FLIPPER DOOR, FWD EDGE AS PER SRM 52-10-00 FIGURE 18 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR 07FDEA02267Trunnion · crackedLANDING GEAR, NOSE GEAR LT TRUNNION FITTING FOUND CRACKED. [07-06-07] REPAIR CARRIED OUT AT NOSE LANDING GEAR LT TRUNNION FITTING AS PER SRM 53- 40-00 FIGURE 23 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 07FDEA02266Duct · crackedLEFT WING ANTI-ICE TELESCOPING DUCT CUT OUT CORNER FOUND CRACKED. [07-13-07] REPAIR CARRIED OUT AT LEFT HAND WING ANTI ICE TELESCOPING DUCT CUT OUT CORNER AS PER FEDEX EA 1-5710-111133, REPAIR CLASSIFIED AS MIN0R AS PER GMM 6-2-100.SDR 07FDEA00528Buss · malfunctionedWHILE EXPERIENCING DU4,5 &6 INTERMITTENT BLANKING RECIEVED 'BUS R EMER AC OFF' LVL 1 ALERT,THEN 'IRU 2 ON BAT' LVL 1,FINALLY 'IRU2 FAIL' LVL 2 ALERT.LATER RECEIVED 'SELECT FADEC ALTN' LVL 2 ALERT ON ALL ENGINES,'ATC XPNR 1 & 2 'FAIL ALERTS,ETC. DIVERTED SDR 06FDEA2391Control Handle · dirtyLOWERED GEAR AT 1200 FT FOR LANDING, UNSAFE INDICATIONS ALL 4 GEAR BOTH PRIMARY AND SECONDARY. RECYCLED GEAR, GOT SAFE DOWN INDICATIONS. FOUND GEAR HANDLE AND CONTROL MECHANISIM STICKING CAUSING FOUR GEAR UNSAFE INDICATIONS PRIMARY AND SECONDARY. CLEANED ANSDR 06FDEA0621Structure · corrodedMAIN DECK COMPARTMENT, DURING SLANT PANEL DRAIN INSPECTION FOUND CORROSION, NEAR DRAIN AREA AT LT STA 1361. REMOVED AND FOUND EXCEEDED LIMITS PER SRM 57-20-00 VOLUME I, FIGURE 12. COMPLIED WITH FEDEX EA 1-5710-90740.SDR 06FDEA0620None · noneUNABLE TO PERFORM EA 1-5740-90695A PT3, WINGS LEADING EDGE SLATS, LT NR 2 SLAT TRACK WEB AND SUPPORT REPAIR DUE TO LONG LEAD TIME OF NEW WEB PN: ARB2981-5. COMPLIED WITH FEDEX EA 1-5740-90695ASDR 06FDEA0347Frame · dentedSNRM N00737: CABIN COMPARTMENT LEFT HAND FRAME AT STATION 1681 FOUND WITH DENT BETWEEN STRINGER 10-11. CORRECTIVE ACTION: SNRM N00737: CABIN COMP'T LH FRAME STA 1661 STR 10-11 CARRIED OUT REPAIR AS PER SRM 53-30 -00 FIG. 1 VOL. I. REPAIR CLASSIFIED ASSDR 06FDEA0290Fuel Tank · crackedLEFT HAND WING TANK, CRACK FOUND DURING HFEC INSPECTION AT THE END OF STRINGER 42 (LOWER STRINGER).SDR 06FDEA0291Fuel Tank · crackedLEFT HAND WING TANK, CRACK FOUND DURING HFEC INSPECTION AT THE END OF STRINGER 43 (LOWER STRINGER). REPAIR CARRIED OUT AS PER SRM 57-20-00.SDR 06FDEA0289Fuel Tank · crackedLEFT HAND WING TANK, CRACK FOUND DURING HFEC INSPECTION AT THE END OF STRINGER 12 (UPPER STRINGER).SDR 06FDEA0288Fuel Tank · crackedRIGHT HAND WING TANK, CRACK FOUND DURING HFEC INSPECTION AT THE END OF STRINGER 9 (UPPER STRINGER). SLOTTED OUT AND REPAIR CARRIED OUT AS PER SRM 57-20-00 VOLUME I, FIGURE 10. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA0287Floorbeam · crackedCENTER CARGO, DOOR ENTRANCE AFT CORNER AT STA 1781 LATERAL FLOORBEAM CHORD FOUND CRACK APPROXIMATELY TWO INCHES LONG. REPAIR CARRIED OUT IAW FEDEX EA 1-5310-90734.SDR 05FDEA04189Structure · crackedSLAT DISAGREE AFTER T/O PRIOR TO SLAT RETRACT. NO ROLL MOVEMENT. INDICATION STOPPED AT SLAT RETRACTION ON ARRIVAL SFS SLAT DISAGREE AGAIN. FOLLOWED CHECK LIST. NO SLAT LANDING WAS NORMAL. FOUND DAMAGED L/E STRUCTURE WHERE PULLY FOR NR 1 SLAT EXTEND CABLE SDR 05FDEA03960Relief Valve · leakingAFTER T/O GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. GROUND SENSOR WAS NOT A FACTOR SINCE PRESSURIZATION WAS NORMAL AND A/P ENGAGED. CONSULTED QRH BUT DID NOT USE THE HANDLE RELEASE BUTTON PER MOCC. RETURNED TO DEL. INSPECTION FOUND FLUID DRIPPING FROM
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