N594FE
Service difficulty reports · 342
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 = 'N594FE' 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 = 'N594FE' 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 08FDEA03657Support Fitting · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 2 SUPPORT FITTING AT HOLES A AND B. MAIN CARGO DOOR LOWER JAMB, CRACKED NR 2 SUPPORT FITTING R & R AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MSDR 08FDEA03656Support Fitting · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 1 SUPPORT FITTING AT HOLES A, C AND D. MAIN CARGO DOOR LOWER JAMB, CRACKED NR 1 SUPPORT FITTING R & R AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIEDSDR 08FDEA03654Vane · delaminatedRT WING INBOARD FLAP VANE LOWER SURFACE INBOARD OF MID WAY TO LEADING EDGE AREA FOUND DELAMINATED. REPAIRED IAW EA 1-5750-124362, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 08FDEA03653Vane · delaminatedLT WING INBOARD FLAP VANE INBOARD OF MID WAY TO TRAILING EDGE AREA FOUND DELAMINATED. REMOVED AND REPLACED AS PER AMM 27-50-22-4. ADJUSTMENT AND TEST CARRIED OUT FOUND SATISFACTORY AS PER AMM 27-50-22-5. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR 08FDEA03652Skin · crackedLT WING - LEADING EDGE AT SLAT NR 3, NR 8 TRACK AREA, 01 EA EDGE CRACK. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100.SDR 08FDEA01877Landing Gear · malfunctionedAFTER TAKEOFF RIGHT MAIN LANDING GEAR INDICATED UNSAFE AFTER RETRACTION ON BOTH THE LANDING GEAR INDICATOR AND ON THE SYNOPTIC DISPLAY. COMPLIED WITH QRH WHICH CALLED FOR ONE RECYCLING OF THE LANDING GEAR. IT WAS SUCCESSFUL ,SDR 07FDEA01248Skin · puncturedLT WING I/B FLAP LOWER SEGMENT UPPER SKIN FOUND PUNCTURED. LT WING I/B FLAP LOWER SEGMENT REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG 35, VOL I AND FEDEX EA 1-5750-106610, WINGS TRAILING EDGE AND TRAILING EDGE DEVICES, LT INBD FLAP UPPER SKIN REPAIR. CLASSISDR 07FDEA00986Frame · dentedMAIN DECK CARGO FRAME, FOUND DENT AT STA 1661 L12 LT. REPAIR CARRIED OUT AT MAIN DECK CARGO FRAME AT STA 1661 L12 LT AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 07FDEA00985Frame · dentedMAIN DECK CARGO, FRAME FOUND DENT AT STA 1721 L12 LT. REPAIR CARRIED OUT AT MAIN DECK CARGO FRAME AT STA 1721 L12 LT AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 07FDEA00922Door · crackedRIGHT MLG FLAPPER DOOR FWD CORNER FOUND CRACKED. REPAIR CARRIED OUT AT RIGHT HAND MLG FLAPPER DOOR FWD CORNER AS PER SRM 52-10-00 FIGURE 18 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR 07FDEA00921Duct · crackedLT WING FIXED L/E COMPT FOUND TELESCOPING DUCT PASSAGE CUTOUT ON EXTERNAL UPPER SURFACE CORNER CRACKED. REPAIR CARRIED OUT ON PASSAGE CUTOUT EXTERNAL UPPER SURFACE CORNER OF THE LT WING FIXED L/E COMPT TELESCOPING DUCT AS PER SRM 57-10-00 FIGURE 42 VOLUME ISDR 06FDEA1274Adc · malfunctionedCRUISE 340 ALL AI ON. AP AND AT DISCONNECTED, FOLLOWING ALERTS SEL ELEV MAN, SEL FLAP LIMIT OVERRIDE, IAS COMPL, WIND SHEAR DET FAIL, NO FD PITCH BAR. RAN AIRSPEED LOST. SUSPECT OR ERRATIC CK LIST, INDICATES NR 1 CADC PROBLEM. DIVERTED TO KSEA ON CADC 2. SDR 06FDEA0403Valve · unknownPDIS: HAD UNSAFE GEAR INDICATION ON ALL 4 GEAR ON BOTH PRIMARY AND SECONDARY INDICATORS. EXECUTED MISSED APPROACH AND COMPLIED W/QRH. GEAR RECYCLED ON OUTSIDE DOWNWIND IAW/QRH AND WE RECEIVED 4 DOWN AND LOCKED INDICATIONS ON PRIMARY AND SECONDARY INDICATORS.SDR 06FDEA0189Fire Warning · false indicationON T/O GOT NR 1 ENG FIRE INDICATION. REJECTED 60KTS/FIRED NR 1 BOTTLE. INDICATION WENT OUT WHEN THROTTLES WERE RETARDED TO IDLE OPENED NR 1 ENG COWLING FOUND SEVERAL COUPLINGS MISSING FOIL. NR 1 FIRE BOTTLE REPLACED, SEE WRI 26-20/4535. FOUND SEVERAL CLAMSDR 05FDEA03111Skin · damagedRIGHT WING UPPER SURFACE AFT OF NR 7 SLAT, 2 EACH LOCKBOLT HEAD FOUND FUEL LEAK, SKIN PLANK FOUND TO HAVE AN ELONGATED BORE. CARRIED OUT REPAIR AS PER FEDEX EA 1-5710-90018.SDR 05FDEA03079Bushing · wornNOSE LANDING GEAR, GROUND SENSING CRANK ASSY, FOUND WITH PLAY. CARRIED OUT BUSHING REPAIR AS PER FEDEX EA 1-3220-90020.SDR 05FDEA03026Fitting · corrodedRIGHT WING, OUTBOARD FLAP INBOARD AFT HINGE FITTING AFT MOUNT AFT HOLE (FLAP SIDE) CORRODED. REMOVED AS PER EO 1-5750-7-5008.SDR 05FDEA03025Fitting · corrodedLEFT WING, OUTBOARD FLAP INBOARD AFT HINGE FITTING FORWARD MOUNT OUTBOARD AFT HOLE (FLAP SIDE) CORRODED. REMOVED AND REPLACED AS PER AMM 27- 50-30-4. ADJUSTMENT AND OPERATION TEST CARRIED OUT FOUND SATISFACTORY AS PER AMM 27-50-00.SDR 05FDEA03024Fitting · corrodedRIGHT WING, OUTBOARD FLAP INBOARD AFT HINGE FITTING OUTBOARD MOUNT HOLE (HINGE SIDE) CORRODED. CARRIED OUT BUSHING REPAIR AS PER FEDEX EA #1-5750- 90023.SDR 05FDEA02936Stringer · crackedCRACK INDICATION AT END OF STRINGER-12 WAS FOUND DURING HFEC INSPECTION AT RIGHT SIDE WING TANK. SLOTTED OUT AND REPAIR CARRIED OUT AS PER SRM 57-20-00, FIG 10, VOL I. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 05FDEA02935Stringer · crackedCRACK INDICATION AT END OF STRINGER-13 WAS FOUND DURING HFEC INSPECTION AT RIGHT SIDE WING TANK. SLOTTED OUT AND REPAIR CARRIED OUT AS PER SRM 57-20-00, FIG 10, VOL I. NEW STRINGER CLIP FABRICATED AS PER FEDEX EA 1-5720-90027, THIS REPAIR IS CLASSIFIED AS MASDR 05FDEA02934Stringer · crackedCRACK INDICATION AT END OF STRINGER-14 WAS FOUND DURING HFEC INSPECTION AT RIGHT SIDE WING TANK. SLOTTED OUT AND REPAIR CARRIED OUT AS PER SRM 57-20-00, FIG 10, VOL I. NEW STRINGER CLIP FABRICATED AS PER FEDEX EA 1-5720-90025, THIS REPAIR IS CLASSIFIED AS MASDR 05FDEA02927Longeron · crackedCENTER CARGO, LONGERON SPLICE AT BILGE AREA ADJACENT TO STATION 5-113 TO STATION 1541 LONGERON -51 LT BRIM AREA FOUND CRACK. CRACK LONGERON SPLICE REMOVED AS PER SRM 51-33-01 VOLUME II. NEW LONGERON SPLICE MACHINED AS PER DWG A5A7114. NEW LONGERON SPLICE SDR 05FDEA02926Longeron · crackedCENTER CARGO, LONGERON SPLICE AT BILGE AREA ADJACENT TO STATION 5-113 TO STATION 1541 LONGERON-52 LEFT BRIM AREA FOUND CRACK. CRACK LONGERON SPLICE AT CENTER CARGO - LONGERON STATION 5-113 TO STATION 1541 LONGERON 52 REMOVED AND REPLACED WITH NEW LONGERON ASSDR 05FDEA02925Longeron · crackedCENTER CARGO, LONGERON SPLICE AT BILGE AREA ADJACENT TO STATION 5-113 TO STATION 1541 LONGERON-49 RIGHT BRIM AREA FOUND CRACK. LONGERON SPLICE REMOVED AT BILGE AREA ADJACENT TO STATION 5-113 TO STATION 1541 LONGERON-49 RT AS PER SRM 51-33-01 VOLUME II. NEW LSDR 05FDEA02924Stringer · crackedCRACK INDICATION AT END OF STRINGER 09 WAS FOUND DURING HFEC INSPECTION AT LEFT SIDE WING TANK. REPAIR CARRIED OUT AT LT WING TANK AT STRINGER 9 AS PER SRM 57-20-00 FIG 10 VOL I. FABRICATED REPAIR ANGLES AS PER SRM 57-20-00 FIG 10 VOL I AND INSTALLED REPAIR SDR 05FDEA02923Stringer · crackedCRACK INDICATION AT END OF STRINGER 10 WAS FOUND DURING HFEC INSPECTION AT LEFT SIDE WING TANK. CRACKED AREA REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 05FDEA02922Stringer · crackedCRACK INDICATION AT END OF STRINGER 14 WAS FOUND DURING HFEC INSPECTION AT LEFT SIDE WING TANK. SLOTTED OUT AND REPAIR CARRIED OUT AS PER SRM 57-20-00, FIGURE 10 VOLUME I. STRINGER REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. THIS REPAIR IS CLASSIFSDR 05FDEA02921Stringer · crackedCRACK INDICATION AT END OF STRINGER-43 WAS FOUND DURING HFEC INSPECTION AT LEFT SIDE WING TANK. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 05FDEA02849Splice · crackedCENTER CARGO - LONGERON SPLICE ADJACENT TO STA 1541 L-40 LEFT HAND BRIM AREA FOUND CRACK. LONGERON SPLICE ADJACENT TO STA 1541 LLONGERON 40 LEFT HAND BRIM AREA REMOVED AS PER SRM 51-33-01 VOL II. NEW LONGERON SPLICE FABRICATED AS PER DRAWING A5A7114 AND SDR 05FDEA02848Splice · crackedCENTER CARGO - LONGERON SPLICE ADJACENT TO STA 1541 L-38 RIGHT BRIM AREA FOUND CRACK. STA 1541 LONGERON 38 RT CRACK LONGERON SPLICE REMOVED AS PER SRM 51-33-01 VOL II. NEW LONGERON SPLICE MACHINED AS PER DWG A5A7114. NEW LONGERON SPLICE INSTALLED AS PER SRSDR 05FDEA02847Frame · nickedMAIN DECK - DVI CARRIED OUT ON INTERIOR FUSELAGE, NICK FOUND ON FRAME 535 LEFT HAND AT G-NET CAUSED BY SUPPORT YOKES. MAIN DECK STATION 535 LEFT HAND FRAME REPAIRED AS PER DWG SRZ-53-503. THIS REPAIR CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100.SDR 05FDEA02846Splice · crackedCENTER CARGO LONGERON SPLICE BRIM AREA SUSPECT CRACK AT STA 1541 ADJACENT TO LONGERON 37 RIGHT HAND. SPLICE REMOVED AS PER SRM 51-33-01 VOL II. NEW LONGERON SPLICE MACHINED AS PER DWG A5A7114. NEW LONGERON SPLICE INSTALLED AS PER SRM 51-33-01 VOL II. THIS SDR 05FDEA02845Splice · crackedCENTER CARGO LONGERON SPLICE FOUND CRACK AT STA 1541 L-32 LEFT HAND. NEW LONGERON SPLICE FABRICATED AS PER DRAWING A5A7112. CRACKED LONGERON SPLICE ON STA 1541 LONGERON 32 REMOVED AND REPLACED AS PER SRM 51-33- 01 VOL II. THIS REPAIR CLASSIFIED AS MAJOSDR 05FDEA02844Doubler · chippedCENTER CARGO - DOOR AFT CUTOUT EDGES EXTERIOR EXISTING REPAIR DOUBLER PATCH CHIPPED EDGES. DAMAGED EXISTING REPAIR DOUBLERS ON CENTER CARGO, DOOR AFT CUTOUT AREA REMOVED AS PER SRM 51-33-01 VOLUME II. AND NEW REPAIR DOUBLERS FABRICATED AS PER SRM 53-50- SDR 05FDEA02843Seat Track · crackedCABIN - SEAT TRACK ADJACENT TO STA 635 X-11 LOWER FLANGE FOUND CRACKED. CARRIED OUT REPAIR AS PER SRM 53-70-00 FIG 1 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 04FDEA02943Rod End · damagedON T/O, THE ACFT ROTATED EXTREMELY SLOW DUE TO ABNORMALLY HEAVY NOSE. CONTACTED GOC TO VERIFY LOAD. AFTER DISCUSSION WITH MX IT WAS DETERMINED THAT PAST HISTORY OF JET SUGGESTED FLT CONTROL PROBLEM. EMERGENCY DECLARED, FUEL DUMPED TO LANDING WEIGHT, CONTROSDR 04FDEA02813Pneumatic System · malfunctionedON CLIMB OUT FROM ZSPD GOT LEVEL 3 ALERT AIR MANF 2 FAIL. COMPLIED /W QRH, DUMPED FUEL, LANDED RJBB. ACN RELEASED FOR SERVICE IAW MEL/CDL: 36-10-02-A CATEGORY: C EXPIRATION: 03OCT04) MEL 36-10-02-A: PNEUMATIC SUPPLY SYS NR 2 INOPERATIVE.**** S/D COMING***SDR 04FDEA01650Frame · dentedMAIN CABIN RIGHT SIDE, TRANSVERSE FRAME DAMAGED AT FS Y= 1621 ALONG LONGERON 12L. COMPLIED WITH FEDEX EA 1-5310-76735, FUSELAGE MAINFRAME REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO (NR: 1-2520-7-3308) PART I.SDR 04FDEA01649Frame · dentedMAIN CABIN RIGHT SIDE, TRANSVERSE FRAME DAMAGED AT FS Y= 1661 ALONG LONGERON 12L. COMPLIED WITH FEDEX EA 1-5310-76735, FUSELAGE MAINFRAME REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO (NR: 1-2520-7-3308) PART I.SDR 04FDEA01648Frame · dentedMAIN CABIN RIGHT SIDE, TRANSVERSE FRAME DAMAGED AT FS Y= 1681 ALONG LONGERON 12L. COMPLIED WITH FEDEX EA 1-5310-76735, FUSELAGE MAINFRAME REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO NR: 1-2520-7-3308 PART I.SDR 04FDEA01647Frame · dentedMAIN CABIN LT SIDE, TRANSVERSE FRAME DAMAGED AT FS Y= 1701 ALONG LONGERON 12L. COMPLIED WITH FEDEX EA 1-5310-76734, FUSELAGE MAINFRAME REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO NR: 1-2520-7-3308 PART I.SDR 04FDEA01646Frame · dentedMAIN CABIN LEFT SIDE, TRANSVERSE FRAME DAMAGED AT FS Y= 1741 ALONG LONGERON 12L. COMPLIED WITH FEDEX EA 1-5310-76734, FUSELAGE MAINFRAME REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO (NR: 1-2520-7-3308) PART I.SDR 04FDEA01645Frame · dentedMAIN CABIN LT SIDE, TRANSVERSE FRAME DAMAGED AT FS Y= 1681 ALONG LONGERON 12L. COMPLIED WITH FEDEX EA 1-5310-76734, FUSELAGE MAINFRAME REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO (NR: 1-2520-7-3308) PART I.SDR 04FDEA01600Pressure Panel · canningRIGHT HAND WHEEL WELL - OIL CANNING FOUND AT STA: Y= 1395-1401, Z= -90 TO -100, DEPTH= 0.0549 INCH Y= 1401-1411, Z= -90 TO -100, DEPTH= 0.0941 INCH Y= 1411-1421, Z= -90 TO -100, DEPTH= 0.0921 INCH Y= 1421-1431, Z= -90 TO -100, DEPTH= 0.0976 INCH Y= 1431-14SDR 04FDEA01598Hinge · corrodedLEFT WING - OUTBOARD FLAP FORWARD OUTBOARD HINGE, FOUND OUTBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09 PG. 402-407. ORIG. DIAM.: 1.187, FINAL DIAM.: 1.222, REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76724 - WINGSDR 04FDEA01597Hinge · corrodedLEFT WING - OUTBOARD FLAP FORWARD OUTBOARD HINGE, FOUND INBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09 PG. 402-407 ORIG. DIAM.:1.187 FINAL DIAM.: 1.222. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76724 WINGS - TRSDR 04FDEA01596Hinge · corrodedLT WING - OUTBOARD FLAP FORWARD OUTBOARD HINGE, FOUND SIDE LINK MATING SURFACE CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 - 407. ORIGINAL THICKNESS =0.446, MATERIAL REMOVED =0.003, REMAINING THICKNESS =0.443, WITHIN LIMIT AS PER DWG NR ARC0503.SDR 04FDEA01595Hinge · corrodedRIGHT WING - OUTBOARD FLAP FORWARD INBOARD HINGE, FOUND INBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44-08 PAGES 402 - 407. ORIGINAL DIAMETER= 1.187, FINAL DIAMETER= 1.221. COMPLIED WITH FEDEX EA 1-5750-76725, WISDR 04FDEA01594Hinge · corrodedRIGHT WING - OUTBOARD FLAP FORWARD INBOARD HINGE, FOUND OUTBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44-08 PAGES 402 - 407. ORIGINAL DIAMETER= 1.187, FINAL DIAMETER= 1.220. COMPLIED WITH FEDEX EA 1-5750-76725, WI
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