N585FE
Service difficulty reports · 491
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 = 'N585FE' 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 = 'N585FE' 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 FDEA202401250117Seat Track · damagedMAIN DECK ,LOCK STA. 759 RBL 8" HAS A DAMAGED SEAT TRACK UNDER IT. REPLACED SEAT TRACKSDR FDEA202212162927Control Panel · shortedDESCENDING THROUGH 15,000 FEET ON ARRIVAL INTO MEMPHIS LEVEL THREE APU FIRE MESSAGE. FOLLOWED QRH, PULLED APU AGENT DISCHARGE HANDLE, DISPENSING BOTH FIRE BOTTLES IN ACCORDANCE WITH CHECKLIST. APU FIRE MESSAGE STAYED ON. DECLARED AN EMERGENCY WITH ATC ANDSDR FDEA202210072509Wire · brokenEMERGENCY EXIT SIGN ABOVE R1 DOOR INOP. RELAMPED-NO HELP. REMOVED AND REPLACED POWER SUPPLY, NO FIX. IAW AMM 33-51-01-4 REMAINS ON MEL. REPAIRED A BROKEN WIRE B370-17-20 IAW SWPM 20-10-03. EMERGENCY LIGHTS OP TEST GOOD.SDR FDEA202210072508Wire · brokenEMERGENCY EXIT SIGN ABOVE R1 DOOR INOP. RELAMPED-NO HELP. REMOVED AND REPLACED POWER SUPPLY NO JOY. IN REF. TO AMM 33-51-01-4 REMAINS ON MEL FACT 07OCT22 08:47 ANC U REPAIRED BROKEN WIRE B370-17-20 IN REF TO SWPM 20-10-03. EMERGENCY LIGHTS OP TESDR FDEA202208272081Warning Message · false activationPDIS 585 32-41 1079 27AUG22 ANC OPEN U TIRE PRESSURE LO IN CRUISE. CONTINUAL DECREASE IN PRESSURE LEFT NOSE TIRE. LOW OF 83 PSI AT LANDING. TIRE PRESS DIFF ALERT ON ROLLOUT. INSPECTION OF TIRE INDICATED NORMAL. ***EMERGENCY DECLARED*** FACSDR FDEA202208272082Tire · leakingPDIS 585 32-41 1079 27AUG22 ANC FACT U TIRE PRESSURE LO IN CRUISE. CONTINUAL DECREASE IN PRESSURE LEFT NOSE TIRE. LOW OF 83 PSI AT LANDING. TIRE PRESS DIFF ALERT ON ROLLOUT. INSPECTION OF TIRE INDICATED NORMAL. ***EMERGENCY DECLARED*** R/I SDR FDEA202208171987Floorbeam · crackedDURING HIGH FREQUENCY EDDY CURRENT ON LEFT HAND OVERWING FLOOR BEAM AND THE UPPER AND LOWER FLANGES AT X = 90 TO X = 116 STATION Y = 1305, FOUND 02 EACH CRACK AT UPPER FLANGE 2ND FASTENER FROM INBOARD NEAR X = 116 AFT SIDE APPROXIMATELY CRACK 1.3Ï¿½ AND SDR FDEA202208091932Floorbeam · corrodedLOWER AFT CARGO COMPARTMENT STATION 1841, X 32 TO X-30 FLOOR SUPPORT FOUND WITH CORROSION. CORROSION AT LOWER AFT CARGO COMPARTMENT STATION 1841, X 32 TO X-30 FLOOR SUPPORT REMOVED AS PER SRM 51-21-01-OG AND FOUND EXCEED LIMIT AS PER SRM 53-00-00- 2R RESDR FDEA202208091934Rib · crackedRIGHT WING Ï¿½ NUMBER 6 SLAT INNER RIB AT STATION XOS 868.476 FOUND CRACK AFTER SKIN REMOVAL. RIGHT WING NUMBER 6 SLAT INNER RIB AT STATION XOS 868.476 REMOVED AND REPLACED AS PER SRM 51-31-01-OG. RIB FABRICATED AS PER DOUGLAS DRAWING ARB 1828 REVISION B. SDR FDEA202208091933Rib · crackedRIGHT WING Ï¿½ NUMBER 6 SLAT INNER RIB AT STATION XOS 863.325 FOUND CRACK AFTER SKIN REMOVAL. RIGHT WING NUMBER 6 SLAT INNER RIB AT STATION XOS 863.325 REMOVED AND REPLACED AS PER SRM 51-31-01-OG. RIB FABRICATED AS PER DOUGLAS DRAWING ARB 1828 REVISION B. SDR FDEA202208061903Skin · damagedLEFT HAND WING INBOARD FLAP OUTBOARD TRAILING EDGE BETWEEN XIFH 247.32 AND XIFH 251.32 EXISITING REPAIR DOUBLER UNABLE TO COMPLY WITH E.A. # : 1-5750-T0357767 B P2 WORK STEP 1. LEFT HAND WING INBOARD FLAP OUTBOARD TRAILING EDGE BETWEEN XIFH 247.32 AND XIFHSDR FDEA202208031844Seat Track · wornCABIN - STATION 508, X = 27.5 SEAT TRACK CROWN FOUND DAMAGED. CABIN - AT SEAT TRACK STATION 508 , X = 27.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONALSDR FDEA202208031843Seat Track · damagedCABIN - STATION 508, X = 8.5 SEAT TRACK CROWN FOUND DAMAGE. CABIN - AT SEAT TRACK STATION 508 X = 8.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEATSDR FDEA202208021833Longeron · corrodedLOWER FORWARD CARGO COMPARTMENT BILGE UNDER FLOOR STATION 6-55, LONGERON 48 RIGHT HAND FOUND WITH CORROSION. CORROSION AT LOWER FORWARD CARGO COMPARTMENT BILGE UNDER FLOOR STATION 6-55, LONGERON 48 RIGHT HAND REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00SDR FDEA202208011832Rib · crackedRIGHT WING - NUMBER 6 SLAT INNER RIB AT STATION XOS 858.175 FOUND CRACK. RIGHT WING NUMBER 6 SLAT AT STATION XOS 858.175 CRACKED INNER RIB REMOVED AND REPLACED AS PER SRM 51-31-01-OG. RIB FABRICATED AS PER DOUGLAS DRAWING ARB1827 REVISION C. REPAIR CLASSIFSDR FDEA202207311829Cargo Track · corrodedLOWER AFT CARGO COMPARTMENT STATION 1923 X 29.31 SEAT TRACK FOUND WITH SURFACE CORROSION. CORROSION AT LOWER AFT CARGO COMPARTMENT STATION 1923 X 30 SEAT TRACK REMOVED AS PER SRM 51-21-01-OG AND FOUND EXCEED LIMIT AS PER ALLOWABLE DAMAGE 1 FIGURE 101SDR FDEA202207311828Doubler · chafedRIGHT WING Ï¿½ FIXED LEADING EDGE FORWARD SURFACE REPAIR DOUBLER AT STATION XOS 767 FOUND CHAFFED. RIGHT WING FIXED LEADING EDGE FORWARD SURFACE AT STATION XOS 767 CHAFFED REPAIR DOUBLER REMOVED AS PER SRM 51-31-01-OG AND CARRIED OUT REPAIR AS PER SRM 57-SDR FDEA202207311827Doubler · crackedRIGHT WING Ï¿½ FIXED LEADING EDGE RIB DOUBLER AT STATION XOS 789 FOUND CRACK. RIGHT WING FIXED LEADING EDGE CRACKED RIB DOUBLER AT STATION XOS 789 REMOVED AND REPLACED AS PER SRM 51-31-01-OG. RIB DOUBLER FABRICATED AS PER DOUGLAS DRAWING ARB3954 REVISION SDR FDEA202207311826Doubler · crackedLEFT WING Ï¿½ FIXED LEADING EDGE RIB DOUBLER AT STATION XOS 789 FOUND CRACK. LEFT WING FIXED LEADING EDGE CRACKED RIB DOUBLER AT STATION XOS 789 REMOVED AND REPLACED AS PER SRM 51-31-01-OG. RIB DOUBLER FABRICATED AS PER DOUGLAS DRAWING ARB3954 REVISION K.SDR FDEA202207311825Doubler · crackedRIGHT WING Ï¿½ FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 711 FOUND CRACK. RIGHT WING FIXED LEADING EDGE AT STATION XOS 711 CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2SDR FDEA202207311824Doubler · crackedLEFT WING Ï¿½ FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 545 FOUND CRACK. LEFT WING FIXED LEADING EDGE AT STATION XOS 545 CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-1SDR FDEA202207311823Doubler · crackedLEFT WING Ï¿½ FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 655 FOUND CRACK. LEFT WING FIXED LEADING EDGE AT STATION XOS 655 CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-1SDR FDEA202207291815Seat Track · wornCABIN Ï¿½ STATION 1249, X = - 27.5 SEAT TRACK CROWN FOUND DAMAGED. CABIN - AT SEAT TRACK STATION 1249 , X = - 27.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SSDR FDEA202207291814Trunnion · crackedDURING HIGH FRIQUENCY EDDY CURRENT SURFACE INSPECTION ON THE RIGHT HAND NOSE LANDING GEAR TRUNION FITTING AFT OF NOSE LANDING GEAR DOOR AFT HINGE FITTING SLOT OUT AREA FOUND 01 EACH CRACKS WITH LENGTH APPROXIMATELY 0.2Ï¿½. RIGHT HAND NOSE LANDING GEAR TRUSDR FDEA202207291813Trunnion · crackedDURING HIGH FRIQUENCY EDDY CURRENT SURFACE INSPECTION ON THE LEFT HAND NOSE LANDING GEAR TRUNION FITTING AFT OF NOSE LANDING GEAR DOOR AFT HINGE FITTING SLOT OUT AREA FOUND 01 EACH CRACKS WITH LENGTH APPROXIMATELY 0.4Ï¿½.SDR FDEA202207291812Doubler · crackedLEFT WING Ï¿½ FIXED LEADING EDGE RIB DOUBLER FOUND CRACK AT STATION XOS 667. LEFT WING FIXED LEADING EDGE CRACKED RIB DOUBLER AT STATION XOS 667 REMOVED AND REPLACED AS PER SRM 51-31-01-OG. RIB DOUBLER FABRICATED AS PER DOUGLAS DRAWING ARB3954 REVISION KSDR FDEA202207291811Stiffener · crackedRIGHT WING Ï¿½ FIXED LEADING EDGE LOWER STIFFENER FOUND CRACK AT STATION XOS 542. RIGHT WING FIXED LEADING EDGE LOWER CRACKED STIFFENER AT STATION XOS 542 REMOVED AND REPLACED AS PER SRM 51-31-01-OG. STIFFENER FABRICATED AS PER DOUGLAS DRAWING ARB2918 REVSDR FDEA202207291810Former · crackedRIGHT WING Ï¿½ FIXED LEADING EDGE UPPER FORMER FOUND CRACK AT STATION XOS 584. RIGHT WING FIXED LEADING EDGE AT STATION XOS 584 CRACKED UPPER FORMER REMOVED AND REPLACED AS PER SRM 51-31-01-OG. FORMER FABRICATED AS PER DOUGLAS DRAWING ARB 2931 REVISION HSDR FDEA202207291809Former · crackedLEFT WING Ï¿½ FIXED LEADING EDGE UPPER FORMER FOUND CRACK AT STATION XOS 584. LEFT WING FIXED LEADING EDGE AT STATION XOS 584 CRACKED UPPER FORMER REMOVED AND REPLACED AS PER SRM 51-31-01-OG. FORMER FABRICATED AS PER DOUGLAS DRAWING ARB 2931 REVISION H. RSDR FDEA202202020177Switch · failedPDIS 585 52-30 0345 02FEB22 IUD OPEN U AIR TURN BACK AFTER TAKEOFF FROM OTBH. MAIN CARGO VENT DOOR OPEN, NO ALERTS. DUMPED APPROXIMATELY 58K BEFORE LANDING. INSPECT VENT DOOR. PART 02FEB22 04:51 MC1 U IDENTIFIED PARTS SWITCH 27/32/52 MPN:SDR FDEA202109062234Light · no testEMERGENCY LIGHT TEST FAIL DURING PREFLIGHT WITH EMER LT BATT 1 LO (LEVEL 1 ALERT). PERFORMED OPERATIONAL TEST OF THE EMERGENCY LIGHTING SYSTEM REF AMM 33-50-00-5. NO FURTHER FAULTS FOUND.OPS CHECK GOOD AT THIS TIME.SDR FDEA202008272042Hinge Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSIONS. CORROSIONS AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CSDR FDEA202008272041Hinge Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSIONS. CORROSIONS AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMMSDR FDEA202008272040Hinge Fitting · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSIONS. CORROSIONS AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRSDR FDEA202008272039Lug · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSIONS. CORROSIONS AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMSDR FDEA202008272038Lug · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSIONS. CORROSIONS AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM SDR FDEA202008252013Beam · crackedCABIN, MAIN DECK CARGO COMPARTMENT LEFT 3 DOOR NUMBER 1 (UPPER) BEAM AFT DOOR STOP NUMBER 1 FOUND CRACKED AT STATION 838.330, Z=51.367. CABIN, MAIN DECK CARGO COMPARTMENT LEFT 3 DOOR NUMBER 1 (UPPER) BEAM AFT DOOR STOP NUMBER 1 STATION 838.330, Z=51.367. REMSDR FDEA2020082652012Beam · crackedCABIN, MAIN DECK CARGO COMPARTMENT RIGHT 3 DOOR NR 1 (UPPER) BEAM AFT DOOR STOP NR1 FOUND CRACKED AT STATION 838.330 , Z= - 51.367. CABIN, MAIN DECK CARGO COMPARTMENT RIGHT 3 DOOR NR 1 (UPPER) BEAM AFT DOOR STOP NR 1 STATION 838.330, Z= -51.367. REMOVED AND SDR FDEA202008211966Hinge · out of limitsMAIN DECK - UPPER CARGO DOOR SIDE FORWARD HINGES ( PART NUMBER ACA 7332-1) FOUND 8 LOBES OUT OF LIMITS. MAIN DECK, UPPER CARGO DOOR SIDE FORWARD HINGES (P/N ACA 7332-1) 9 LOBES, REWORKED AS PER MD-11 SRM 51-21-01-0G. REPAIR BUSHINGS (09EA) FABRICATED BY MASDR FDEA2020081091836Seat Track · damagedMAIN DECK CARGO COMPARTMENT SEAT TRACK CROWN DAMAGED AT BS 755 , LBL 27.5. DAMAGE REMOVED AND FOUND WITHIN LIMITS IAW SRM 53-00-52-1A. FIGURE 101. ALLOWABLE DAMAGE 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR FDEA202009081828Support · corrodedRT WING, OUTBOARD FLAP VANE NR 4 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT RT WING, OUTBOARD FLAP VANE NR 4 SUPPORT FITTING ECCENTRIC HOLE BORE. REWORKED BY MACHINING AND FOUND EXCEEDS LIMIT, AS PER MD-11 SRM 57-50-02-2R FIGURE 201 SDR FDEA2020090881827Support · corrodedRT WING, OUTBOARD FLAP VANE NR 3 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT RT WING, OUTBOARD FLAP VANE NR 3 SUPPORT FITTING ECCENTRIC HOLE BORE. REWORKED BY MACHINING AND FOUND EXCEEDS LIMIT, AS PER MD-11 SRM 57-50-02-2R FIGURE 201 SDR FDEA2020090481824Support Fitting · corrodedLT WING, OUTBOARD FLAP VANE NR 5 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT LT WING, OUTBOARD FLAP VANE NR 5 SUPPORT FITTING ECCENTRIC HOLE BORE. REWORKED BY MACHINING AND FOUND EXCEEDS LIMIT AS PER MD-11 SRM 57-50-02-2R FIGURE 201 RSDR FDEA2020090481822Support · corrodedLT WING, OUTBOARD FLAP VANE NR 3 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT LT WING, OUTBOARD FLAP VANE NR 3 SUPPORT FITTING ECCENTRIC HOLE BORE. REWORKED BY MACHINING AND FOUND EXCEEDS LIMIT AS PER MD-11 SRM 57-50-02-2R FIGURE 201 RSDR FDEA2020081081828Support Fitting · corrodedRIGHT WING OUTBOARD FLAP VANE NR 4 SUPPORT FITTING ECCENTRIC HOLE BORE WAS FOUND CORRODED.SDR FDEA2020081081827Support Fitting · corrodedRIGHT WING OUTBOARD FLAP VANE NR 3 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORRODED.SDR FDEA2020081081824Support Fitting · corrodedLEFT WING OUTBOARD FLAP VANE NR 5 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORRODED.SDR FDEA2020081081822Vane · corrodedLEFT WING, OUTBOARD FLAP VANE NR 3 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORRODED.SDR FDEA202008071796Floorbeam · corrodedUPON REMOVAL OF LAVATORY MODULE IN THE CABIN, RIGHT. BS 420, X -20 - X -27, THE FLOORBEAM STRUCTURE WAS FOUND CORRODED. FLOOR SUPPORT REMOVE AND REPLACED BY FABRICATION PER DOUGLAS DRAWING # WSP0668 REVISION 'B' AND INSTALLED PER MD - 11 AMM 20-50-02 . REPSDR FDEA202008071795Floor Panel · corrodedFORWARD MAIN DECK CARGO COMPARTMENT FLOOR PANEL EDGE FOUND WITH CORROSION AT LEFT BS 475 - 503 , X 19.5 TO X 26.5. REMOVE AND REPLACED AS PER SRM 51-31-01-OG . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
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