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 FDEA202303020377Seat Track · crackedSEAT TRACK AFA7795-11 HAS DAMAGED LOBES AT STA. 1661 AND C/L. INSTALLED SEAT TRACK SPLICE REPAIR AT SEAT TRACK AFA7795-11 STA. 1661 AND C/L. REF. MD-11 SRM 53-00-52- 2R-0 FIGURE 201 REPAIR 1 AND FDX DRAWING SR 10-53-002 REV A.. THIS IS A MAJOR REPAIR.SDR FDEA202303020371Seat Track · crackedSEAT TRACK AFA7795-11 HAS DAMAGED LOBES AT STA. 1539 AND X= -27.50 REF. W/O 85469 SEQ.#14 AND WRI 25506410 REPAIRED PER SRM 53-00-52-2R REPAIR 2SDR FDEA202302040203Engine · damagedMDIS 594 72-21 6359 04FEB23 MEM OPEN U #1 ENG HAS SEVERAL FAN BLADES DAMAGED DUE TO BIRDSTRIKE. COMPLETED FDX WIC 7100000-01-91 INSTALLATION #1 ENG.CHECKS OK.SDR FDEA202204130954Control Valve · failedON FINAL, RECEIVED LEVEL 2 HYD 1 FAIL ALERT. RESERVOIR QUANTITY SHOWED 0.8 GALLONS. ***EMERGENCY DECLARED*** REMOVED STAB TRIM CONTROL MODULE IAW MD11 AMM 27-43-40-4 FOR EVIDENCE OF LEAK. LEAKING ISOLATED TO STAB TRIM CONTROL MODULE FLOW CONTROL VALVE.SDR FDEA202204090908Skin · damagedLEFT HAND WING - INBOARD FLAP ASSEMBLY, INBOARD UPPER MID SEGMENT STATION XIFH 160 FOUND OIL CANNING. LEFT HAND WING INBOARD FLAP ASSEMBLY INBOARD UPPER MID SEGMENT DAMAGE SKIN AT STATION XIFH 160 REPAIRED IN ACCORDANCE WITH SRM 57-00-01-2R REPAIR 1 FIGURESDR FDEA202204090900Bracket · corrodedRIGHT HAND WING - INBOARD FLAP ASSEMBLY . OUTBOARD FORWARD HINGE (WING SIDE) PIVOT LUG BORE CORROSION. CORROSION AT RIGHT HAND WING - INBOARD FLAP ASSEMBLY . OUTBOARD FORWARD HINGE (WING SIDE) PIVOT LUG BORE (#3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS SDR FDEA202204090899Bracket · corrodedLEFT HAND WING - INBOARD FLAP ASSEMBLY . OUTBOARD FORWARD HINGE (WING SIDE) PIVOT LUG BORE CORROSION. CORROSION AT LEFT HAND WING - INBOARD FLAP ASSEMBLY . OUTBOARD FORWARD HINGE (WING SIDE) PIVOT LUG BORE (#3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER SDR FDEA202204090898Spar Cap · corrodedAFTER LEFT HAND OUTBOARD ISLAND REMOVAL FOR ACCESS LEFT HAND WING REAR SPAR UPPER CAP AFT FLANGE XORS = 1069 FOUND CORROSION. AFTER LEFT HAND OUTBOARD ISLAND REMOVAL LEFT HAND WING REAR SPAR UPPER CAP AFT FLANGE XORS = 1069 CORROSION REMOVED AND FOUND EXSDR FDEA202204090897Spar Cap · corrodedAFTER LEFT HAND OUTBOARD ISLAND REMOVAL FOR ACCESS LEFT HAND WING REAR SPAR UPPER CAP AFT FLANGE XORS = 1049 FOUND CORROSION. LEFT HAND WING REAR SPAR UPPER CAP AFT FLANGE XORS = 1049 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 57-00-10-1A ALLOWABLSDR FDEA202204060874Skin · noneAGING AIRCRAFT - EXISTING SKIN SPLICE REPAIR FOUND AT LEFT HAND WING INBOARD FLAP CENTER BOX LOWER SURFACE BETWEEN XIFH 249- XIFH 255. EXISTING SKIN SPLICE REPAIR ON LEFT HAND WING INBOARD FLAP CENTER BOX LOWER SURFACE BETWEEN XIFH 249 - XIFH 255 EVALUATEDSDR FDEA202204030816Lug · corrodedRIGHT HAND WING - INBOARD FLAP ASSEMBLY . OUTBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR LUG BORE CORROSION. REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-07 ANDSDR FDEA202204030815Lug · corrodedRIGHT HAND WING - INBOARD FLAP ASSEMBLY . OUTBOARD FORWARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG BORE CORROSION. REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-07 ANSDR FDEA202204010808Skin · misrepairedAGING AIRCRAFT - EXISTING REPAIR DOUBLER ON EXTERIOR FUSELAGE SKIN BETWEEN STATION 383 TO STATION 399 , LONGERON 25 LEFT HAND TO LONGERON 27 LEFT HAND. EXISTING REPAIR DOUBLER ON EXTERIOR FUSELAGE SKIN BETWEEN STATION 383 TO STATION 399 LONGERON 25 TO LONGSDR FDEA202203310791Skin · noneAGING AIRCRAFT - EXISTING DOUBLER REPAIR AT LEFT HAND WING DROOP LEADING EDGE ASSEMBLY . INBOARD AREA XDLE 309.934. EXISTING DOUBLER REPAIR AT LEFT HAND WING DROOP LEADING EDGE ASSEMBLY INBOARD AREA XDLE 309.934 EVALUATED AND FOUND REPAIRED IN ACCORDANCE WSDR FDEA202203290735Hinge · wornCABIN-UPPER CARGO DOOR FUSELAGE HINGE FITTING PART NUMBER ACA7223-513 FOUND LOBES #1 TO 15 OUT OF LIMIT. LOBE HOLES #1 TO #15 FROM FORWARD AT CABIN-UPPER CARGO DOOR FUSELAGE HINGE FITTING PART NUMBER:ACA7223-513 REWORKED AND FOUND #1 TO #10 HOLES EXCEED SDR FDEA202203290729Support · corrodedLEFT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (D) ECCENTRIC HOLE CORROSION. CORROSION AT LEFT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (D) ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57- 5SDR FDEA202203290730Support · corrodedRIGHT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (B) ECCENTRIC HOLE CORROSION. CORROSION AT RIGHT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (B) ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57- SDR FDEA202203290736Fitting · out of limitsCABIN-MAIN DECK CARGO DOOR HINGE FITTING PART NUMBER ACA7223-523 FOUND LOBES #1 TO 12 FROM FORWARD OUT OF LIMITS. LOBE HOLES #1 TO #12 FROM FORWARD AT CABIN-MAIN DECK CARGO DOOR HINGE FITTING PART NUMBER:ACA7223-523 REWORKED AND FOUND #1 TO #4 HOLES EXCEESDR FDEA202203290733Support · corrodedRIGHT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (D) ECCENTRIC HOLE CORRODED. HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57- 50-02-2R REPAIR 5 FIGURE 201. ECCENTRIC OVERSIZED BUSHING FABRICATED BY MACHINING AS PER MD-SDR FDEA202203290732Support · corrodedRIGHT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (C) ECCENTRIC HOLE CORRODED. HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57- 50-02-2R REPAIR 5 FIGURE 201. ECCENTRIC OVERSIZED BUSHING FABRICATED BY MACHINING AS PER MD-SDR FDEA202203290731Support · corrodedRIGHT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (E) ECCENTRIC HOLE CORRODED. HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57- 50-02-2R REPAIR 5 FIGURE 201. ECCENTRIC OVERSIZED BUSHING FABRICATED BY MACHINING AS PER MDSDR FDEA2022032190730Support · corrodedRIGHT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (B) ECCENTRIC HOLE CORROSION.SDR FDEA202203290728Support · corrodedLEFT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (C) ECCENTRIC HOLE CORROSION. CORROSION AT LEFT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (C) ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-SDR FDEA202203290727Support · corrodedLEFT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (E) ECCENTRIC HOLE CORROSION. CORROSION AT LEFT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (E) ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-SDR FDEA202203290726Support · corrodedLEFT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (B) ECCENTRIC HOLE CORROSION. CORROSION AT LEFT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (B) ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57- SDR FDEA202203280725Bracket · corrodedLEFT HAND WING - OUTBOARD FLAP ASSEMBLY . INBOARD FORWARD HINGE (WING SIDE) BARREL NUT SPOT FACE CORROSION. CORROSION AT LEFT HAND WING - OUTBOARD FLAP ASSEMBLY . INBOARD FORWARD HINGE (WING SIDE) BARREL NUT SPOT FACE REWORKED AS PER MD-11 CMM57-44-08. RESDR FDEA202203280717Support · corrodedLEFT HAND WING - OUTBOARD FLAP ASSEMBLY . INBOARD AFT HINGE (FLAP SIDE) INBOARD PIVOT LUG BORE CORROSION. CORROSION AT LEFT HAND WING - OUTBOARD FLAP ASSEMBLY . INBOARD AFT HINGE (FLAP SIDE) INBOARD PIVOT LUG BORE REWORKED AND FOUND EXCEED LIMIT AS PER MDSDR FDEA202203280715Bracket · corrodedLEFT HAND WING - INBOARD FLAP ASSEMBLY . OUTBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR LUG BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-07. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-07 SDR FDEA202203280714Bracket · corrodedLEFT HAND WING - INBOARD FLAP ASSEMBLY . OUTBOARD FORWARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-07. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-07SDR FDEA202203280713Bracket · corrodedLEFT HAND WING - INBOARD FLAP ASSEMBLY . OUTBOARD AFT HINGE (FLAP SIDE) OUTBOARD PIVOT LUG BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-52-03 AND E.ASDR FDEA202203280712Bracket · corrodedLEFT HAND WING - INBOARD FLAP ASSEMBLY . OUTBOARD AFT HINGE (FLAP SIDE) INBOARD PIVOT LUG BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-52-03 AND E.A.SDR FDEA202203280710Bracket · corrodedRIGHT HAND WING - INBOARD FLAP ASSEMBLY . OUTBOARD AFT HINGE (FLAP SIDE) INBOARD PIVOT LUG BORE CORROSION. CORROSION AT RIGHT HAND WING - INBOARD FLAP ASSEMBLY . OUTBOARD AFT HINGE (FLAP SIDE) INBOARD PIVOT LUG BORE (F AND G HOLE) REWORKED AND FOUND EXCESDR FDEA202203280709Bracket · corrodedRIGHT HAND WING - INBOARD FLAP ASSEMBLY . OUTBOARD AFT HINGE (FLAP SIDE) OUTBOARD PIVOT LUG BORE CORROSION. CORROSION AT RIGHT HAND WING - INBOARD FLAP ASSEMBLY . OUTBOARD AFT HINGE (FLAP SIDE) OUTBOARD PIVOT LUG BORE(A AND B HOLE) REWORKED AND FOUND EXCSDR FDEA202203270702Longeron Splice · crackedLOWER CENTER CARGO COMPARTMENT STATION 5-123 LONGERON 50 RIGHT HAND SPLICE FITTING FOUND WITH CRACK . SPLICE FITTING REMOVED AND REPLACED WITH FABRICATED SPLICE AS PER SRM 51-33-01- OG. SPLICE FABRICATED AS PER DOUGLAS DRAWING A5A7114 REVSION J . REPAIR SDR FDEA202203270701Longeron Splice · crackedLOWER CENTER CARGO COMPARTMENTSTATION 5-123 LONGERON 39 LEFT HAND SLICE FITTINF FOUND WITH CRACK . SPLICE FITTING REMOVED AND REPLACED WITH FABRICATED SPLICE AS PER SRM 51-33-01- OG. SPLICE FABRICATED AS PER DOUGLAS DRAWING A5A7114 REVSION J . REPAIR CLASDR FDEA202203240675Doubler · damagedEXISTING REPAIR FOUND AT LEFT HAND WING TANK STRINGER END 14 (UPPER) BETWEEN XORS 506 TO XORS 538 . EXISTING REPAIR AT LEFT HAND WING TANK STRINGER END 14 BETWEEN XORS 506 AND XORS 538 EVALUATED AND FOUND NOT REPAIRED IN ACCORDANCE WITH SRM 57-00-03-2R REPSDR FDEA202203240673Doubler · damagedEXISTING REPAIR FOUND AT RIGHT HAND WING TANK STRINGER END 14 ( UPPER) BETWEEN XORS 506 TO XORS 538. EXISTING REPAIR AT RIGHT HAND WING TANK STRINGER END 14 BETWEEN XORS 506 TO XORS 538 EVALUATED AND FOUND NOT REPAIRED IN ACCORDANCE WITH SRM 57-00-03-2R RESDR FDEA202203240672Doubler · damagedEXISTING REPAIR FOUND AT RIGHT HAND WING TANK STRINGER END 13 (UPPER) BETWEEN XORS 562 TO XORS 592. EXISTING REPAIR AT RIGHT HAND WING TANK STRINGER END 13 BETWEEN XORS 562 TO XORS 592 EVALUATED AND FOUND NOT REPAIRED IN ACCORDANCE WITH SRM 57-00-03-2R RESDR FDEA202203230654Skin · damagedLEFT HAND WING - INBOARD FLAP ASSEMBLY INBOARD LOWER SEGMENT EXISTING REPAIR INTERNAL DAMAGED. DAMAGE EXISTING REPAIR AT LEFT HAND WING INBOARD FLAP ASSEMBLY INBOARD LOWER SEGMENT BETWEEN XIFH 133.9 AND XIFH 195.3 REMOVED AS PER SRM 51-31-01-0G. REPAIR SDR FDEA202203220630None · noneAGING AIRCRAFT - EXISTING REPAIR DOUBLER FOUND ON WEB AT CENTER CARGO COMPARTMENT AFT BULKHEAD STATION 1841 X = 17 . EXISTING REPAIR DOUBLER ON WEB AT CENTER CARGO COMPARTMENT AFT BULKHEAD STATION 1841 X = 17 EVALUATED AND FOUND WEB WITH DAMAGE AND EXCEESDR FDEA202203220629Former · crackedRIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT AT APPROXIMATELY XOS 584 FORMR FOUND CRACKED. RIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT AT APPROXIMATELY XOS 584 FORMER CRACKED REMOVED AND REPLACED AS PER SRM 51-31-01-OG. FORMER FABRICATED AS PSDR FDEA202203220625Seat Track · damagedAGING AIRCRAFT - EXISTING REPAIR FOUND ON SEAT TRACK AT MAIN DECK CARGO COMPARTMENT BETWEEN STATION 745 TO STATION 783 X = 27.5. EVALUATED AND FOUND SEAT TRACK NOT REPAIRED IN ACCORDANCE WITH SRM 53-00-52-2R REPAIR 1 FIGURE 201 . SEAT TRACK REPAIR CARRIEDSDR FDEA202203220624None · noneAGING AIRCRAFT - EXISTING REPAIR FOUND ON SEAT TRACK AT MAIN DECK CARGO COMPARTMENT BETWEEN STATION 745 TO STATION 785 X = -8.5.SDR FDEA202203210613Skin · damagedAGING AIRCRAFT - EXISTING REPAIR DOUBLER FOUND AT RIGHT HAND WING INBOARD FLAP LOWER SEGMENT UPPER SKIN XIFH 288.14 EXISTING REPAIR DOUBLER AT RIGHT HAND WING INBOARD FLAP LOWER SEGMENT UPPER SKIN XIFH 288.14 EVALUATED AND FOUND REPAIR DOUBLER DAMAGED ANDSDR FDEA202203210612Skin · damagedAGING AIRCRAFT - EXISTING REPAIR DOUBLER FOUND AT RIGHT HAND WING INBOARD FLAP LOWER SEGMENT UPPER SKIN XIFH 261.69. EXISTING REPAIR DOUBLER AT RIGHT HAND WING INBOARD FLAP LOWER SEGMENT UPPER SKIN XIFH 261.69 EVALUATED AND FOUND EXISTING REPAIR DOUBLER DASDR FDEA202203200605Stiffener · crackedLEFT HAND WING LOWER STIFFENER AT APPROXIMATELY XOS 542 FOUND CRACK. LEFT HAND WING LOWER AT APPROXIMATELY XOS 542 CRACKED STIFFENER REMOVED AND REPLACED AS PER SRM 51-31-01-OG. STIFFENER FABRICATED AS PER DOUGLAS DRAWING ARB 2918 REVISION G. REPAIR CLASSSDR FDEA202203200604Former · crackedLEFT HAND WING UPPER FORMER AT APPROXIMATELY XOS 912 FOUND CRACKED. LEFT HAND WING UPPER COMPARTMENT FIXED LEADING EDGE APPROXIMATELY XOS 912 CRACKED FORMER REMOVED AND REPLACED AS PER SRM 51-31-01-OG. FORMER FABRICATED AS PER DOUGLAS DRAWING ARB 2921 REVSDR FDEA202203200603Stiffener · crackedRIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT AT APPROXIMATELY XOS 542 STIFFENER FOUND CRACKED. RIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT AT APPROXIMATELY XOS 542 CRACKED STIFFENER REMOVED AND REPLACED AS PER SRM 51-31-01-OG. STIFFENER FABRISDR FDEA202203200602Doubler · crackedRIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT AT APPROXIMATELY XOS 789 RIB DOUBLER FOUND CRACKED. RIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT AT APPROXIMATELY XOS 789 RIB DOUBLER REMOVED AND REPLACED AS PER SRM 51-31-0-OG. RIB DOUBLER FABRICATEDSDR FDEA202203200601Former · crackedLEFT HAND WING FIXED LEADING EDGE AT APPROXIMATELY XOS = 789 FORMER FOUND CRACKED. LEFT HAND WING FIXED LEADING EDGE AT APPROXIMATELY XOS = 789 CRACKED FORMER REMOVED AND REPLACED AS PER SRM 51-31-01-OG. FORMER FABRICATED AS PER DOUGLAS DRAWING ARB 2930
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