N605FE

Service difficulty reports · 508

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 = 'N605FE' 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.

SDR 03FDEA01166Hinge · looseLT WING O/B FLAP (FLAP SIDE) O/B HINGE I/B AND O/B PIVOT HOLES BUSHING FOUND LOOSE. LEFT O/B FLAP (FLAP SIDE) O/B HINGE I/B AND O/B PIVOT HOLES REPAIRED AS PER FEDEX EA 1-5750-69278 - WINGS TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP/INBOARD SUPPORT BRACKET COJul 25, 2003 · N605FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA01164Hinge · corrodedRIGHT O/B FLAP (FLAP SIDE) I/B HINGE I/B AND O/B ACTUATOR HOLES CORRODED. RIGHT WING O/B FLAP (FLAP SIDE) I/B HINGE I/B AND O/B ACTUATOR HOLES REPAIRED AS PER FEDEX EA 1-5750-69277, TITLE: WINGS- TRAILING EDGE AND TRAILING EDGE DEVICES - RIGHT OUTBOARD FLAPJul 23, 2003 · N605FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA01163Hinge · corrodedRIGHT O/B FLAP (FLAP SIDE) I/B HINGE I/B PIVOT HOLE AND I/B PIVOT LUG INNER AND OUTER SURFACES FOUND CORRODED. RIGHT WING O/B FLAP (FLAP SIDE) I/B HINGE I/B PIVOT HOLE AND I/B LUG INNER AND OUTER SURFACES REPAIRED AS PER FEDEX EA 1-5750-69277, TITLE: WINGS - Jul 23, 2003 · N605FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA01135Hinge · corrodedLEFT O/B FLAP (FLAP SIDE) - I/B HINGE BRACKET I/B ACTUATOR ATTACHMENT HOLE FOUND CORRODED. LEFT WING O/B FLAP (FLAP SIDE) - I/B HINGE BRACKET I/B ACTUATOR ATTACHMENT HOLE REPAIRED AS PER FEDEX EA 1-5750-69278, TITLE: WINGS TRAILING EDGE DEVICES - LT OUTBOARD Jul 23, 2003 · N605FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA01137Hinge · corrodedLT O/B FLAP (FLAP SIDE) - I/B HINGE I/B PIVOT HOLE AND I/B LUG INNER AND OUTER SURFACE CORRODED. LEFT WING O/B FLAP (FLAP SIDE) - I/B HINGE- I/B PIVOT HOLE AND I/B LUG INNER AND OUTER SURFACE REPAIRED AS PER FEDEX EA 1-5750-69278, TITLE: WINGS - TRAILING EDGEJul 23, 2003 · N605FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA01136Hinge · corrodedLEFT O/B FLAP (FLAP SIDE) - I/B HINGE O/B ACTUATOR ATTACHMENT HOLE CORRODED. LEFT WING O/B FLAP (FLAP SIDE) - I/B HINGE O/B ACTUATOR ATTACHMENT HOLE REPAIRED AS PER FEDEX EA 1-5750-69278, TITLE: WINGS - TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP/INBOARD SUPJul 23, 2003 · N605FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA01138Hinge · corrodedLEFT O/B FLAP (FLAP SIDE) - I/B HINGE O/B PIVOT HOLE CORRODED. SNRM N0463 - LEFT WING O/B FLAP (FLAP SIDE) - I/B HINGE O/B PIVOT HOLE REPAIRED AS PER FEDEX EA 1-5750-69278, LEFT OUTBOARD FLAP/INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.Jul 23, 2003 · N605FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA01165Hinge · corrodedRIGHT WING- O/B FLAP (FLAP SIDE) I/B HINGE O/B PIVOT HOLE CORRODED. RIGHT WING- O/B FLAP (FLAP SIDE) I/B HINGE O/B PIVOT HOLE REPAIRED AS PER FEDEX EA 1-5750-69277, TITLE: WINGS- TRAILING EDGE AND TRAILING EDGE DEVICES- RIGHT OUTBOARD FLAP / INBOARD SUPPORT BJul 23, 2003 · N605FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA01162Hinge · corrodedRIGHT WING - O/B FLAP (FLAP SIDE) O/B HINGE I/B PIVOT HOLE AND I/B PIVOT LUG INNER AND OUTER LUG SURFACES FOUND CORRODED.Jul 23, 2003 · N605FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA01134Hinge · corrodedLT I/B FLAP (FLAP SIDE) - O/B HINGE O/B PIVOT HOLE AND O/B PIVOT LUG INNER AND OUTER SURFACES CORRODED. LT I/B FLAP (FLAP SIDE)- O/B HINGE O/B PIVOT HOLE AND O/B PIVOT LUG INNER AND OUTER SURFACES REPAIRED AS PER FEDEX EA 1-5750-69256 - WINGS - TRAILING EDGJul 23, 2003 · N605FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA01139Hinge · corrodedRIGHT I/B FLAP (FLAP SIDE) - O/B HINGE O/B PIVOT HOLE AND LUG INNER AND OUTER SURFACE CORRODED. RT I/B FLAP (FLAP SIDE)- O/B HINGE, O/B PIVOT HOLE AND LUG INNER AND OUTER SURFACE REPAIRED AS PER FEDEX EA 1-5750-69257 - WINGS - TRAILING EDGE & TRAILING EDGE Jul 23, 2003 · N605FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA01140Hinge · corrodedRIGHT I/B FLAP (FLAP SIDE) - O/B HINGE I/B PIVOT HOLE AND LUG INNER SURFACE CORRODED. RT I/B FLAP (FLAP SIDE)- O/B HINGE I/B PIVOT HOLE AND LUG INNER SURFACE REPAIRED AS PER FEDEX EA 1-5750-69257 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RT INBD FLJul 23, 2003 · N605FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA01161Skin · bulgedRT WING PANEL AT STA XORS 1042 REAR SPAR SKIN BULGE. RT WING PANEL AT STA XORS 1042 REAR SPAR SKIN BULGE REPAIRED AS PER FEDEX EA 1-5720-69399 - WINGS - OUTER WING - RH REAR SPAR/TRAILING EDGE CORROSION REWORK.Jul 22, 2003 · N605FE · Doug MD11 · Wing, Plate/SkinSDR 03FDEA01128Hinge Fitting · crackedLEFT WING OUTBOARD FLAP INBOARD HINGE FITTING OUTBOARD SIDE LINK FOUND CRACKED. CRACKED O/B SIDE LINK FITTING OF LEFT WING O/B FLAP I/B HINGE FITTING REMOVED AND REPLACED WITH NEW FITTING AS PER SRM 51-33-01 VOL II.Jul 21, 2003 · N605FE · Doug MD11 · Trailing Edge FlapsSDR 02FDEA00419Fastener · brokenDURING B-CHECK FOUND 1 TAPER LOCK FASTENER BROKEN ON REAR SPAR LOWER CAP OF CENTER WING REF EA 1-5314-64689. R/R FASTENER PER E.A.Jun 18, 2002 · N605FE · Doug MD11 · FastenersSDR 02FDEA00200Aileron · illuminated02-67 AILERON DEFLECT DISAGREE ALERT CAME ON IN FLT. DIVERT TO RCTP DUE TO INCREASE FUEL BURN. ** S/D ** COMINGMar 13, 2002 · N605FE · Doug MD11F · Aileron Control SystemSDR 02FDEA00141Wire Harness · brokenNR 1 ENG GENERATOR FEEDER CABLE N012-2-00B (AL) BROKEN NEAR LT WING ROOT FEED THROUGH. REMOVED AND REPLACED NR 1 ENG GEN FEEDER LINE CABLE AND CLAMPS PER MM 24-22-03-5.Feb 24, 2002 · N605FE · Doug MD11F · Electrical Power System WiringSDR 02FDEA00138Wire Harness · brokenNR 3 ENG GENERATOR FEEDER CABLE N117-1-00A (AL) NEAR TERMINAL STRIP S3-385R BROKEN. REMOVED AND REPLACED NR 3 ENG GEN FEEDER LINE CABLE AND CLAMPS PER MM 24-22-03-5.Feb 20, 2002 · N605FE · Doug MD11F · Electrical Power System WiringSDR 02FDEA00129Rib · crackedRIGHT WING L/E COMPT RIB FOUND CRACKED AT STA XORS 694 APPROX 3 INCHES. REMOVED AND REPLACED RIB PER DWG ARB 2922.Feb 17, 2002 · N605FE · Doug MD11F · Wing, Rib/BulkheadSDR 02FDEA00133Spar · bulgedLT WING UPPER FIXED T/E PANEL BULGED AT BS XOR 674 (CTR OF NR 4 SPOILER). REMOVED AND REPLACED OUTER WING REAR SPAR/TRAILING EDGE PER EA 1-5720-60680.Feb 16, 2002 · N605FE · Doug MD11F · Wing SparSDR 02FDEA00132Spar · corrodedLT WING UPPER FIXED T/E PANEL BULGE AT BS XOR 772.5 (O/B OF NR 5 SPOILER). REMOVED AND REPLACED OUTER WING REAR SPAR/TRAILING EDGE PER EA 1-5720-60680.Feb 16, 2002 · N605FE · Doug MD11F · Wing SparSDR 02FDEA00134Bearing · out of positionRT WING O/B SLAT DRIVE MECHANISM FWD BEARING MIGRATED. REMOVED AND REPLACED WING OUTBOARD SLAT DRIVE MECH PER EA 1-2780-60721.Feb 16, 2002 · N605FE · Doug MD11F · Leading Edge Slat ActuatorSDR 02FDEA00169Bearing · out of positionRT WING O/B SLAT DRIVE MECHANISM FWD BEARING MIGRATED.Feb 16, 2002 · N605FE · Doug MD11F · Leading Edge Slat ActuatorSDR 01FDEA00940Actuator · failed01-356 ON T/O UPON FLAP RETRACTION RECEIVED LEVEL 2 DEFLECTED AILERON DISAGREE ALERT. ** S/D ** COMINGOct 31, 2001 · N605FE · Doug MD11F · Aileron Control SystemSDR 01FDEA00816Flap · vibrationVIBRATION ON SELECTING FLAPS TO 50 DEG. NO PROBLEMS FOUND ON FLT CONTROL INSP. AC OK FOR SERVICE.Sep 8, 2001 · N605FE · Doug MD11F · Trailing Edge Flap Control SystemSDR 01FDEA00519O-Ring · brokenIN CR HYD 1 OFF ILLUM. REMOVED AND REPLACED BROKEN O-RING PER SMP. LEAK CK OK.Jul 6, 2001 · N605FE · Doug MD11F · Hydraulic System, MainSDR 01FDEA00435O-Ring · leakingHYD SYS NR 1 FAIL 1 HR INTO FLT FOUND LEAKS FROM HOL STAB CONTROL VALVE NR 2 SYS NR 1 PRESS LINE ON VALVE FITTING. REMOVED AND REPLACED DELAMINATED O-RING OF FITTING.Jun 12, 2001 · N605FE · Doug MD11F · Hydraulic System, MainSDR 01FDEA00019Filter · malfunctionedRECEIVED TANK 2 FWD PMP LO ALERT. ACCOMPLISH CKLIST. NR 2 ENG FLAMED OUT AFTERWARDS. FOR PRECAUTION REMOVED AND REPLACED NR 2 ENG FUEL FILTER AND NO LEAK PER 73-11-04-6. FUEL SHROUD DRAIN FOUND NO LEAK PER MM 28-25-00-6.Jan 12, 2001 · N605FE · Doug MD11F · Aircraft Fuel Filter/StrainerSDR 00FDEA00865Epcu · faulty00-347 ON DEPART HAD MOMENTARY TOTAL ELECTRICAL PWR FAILURE. R&R EPCU PER MM 24-08-01-4, 24-20-17.Dec 6, 2000 · N605FE · Doug MD11F · AC Generation SystemSDR 00FDEA00044Window · cracked00-25 - FO SLIDING WINDOW OUTER PANE OBSERVED CRACKING IN OUTER PANE, CRACK PROGRESSING APPROX 1 PER 5 MIN AT FL 330. CONTACTED ANC MAINT AND ADVISED TO RETURN TO PANC. REMOVED AND REPLACED RT CLEAR VIEW WINDOW PER MM 56-12-01-4. WINDOW OPS CK GOOD. REMOVEJan 31, 2000 · N605FE · Doug MD11F · Flight Compartment WindowsSDR 00FDEA00023Seat Track · crackedSNRM 263, 264, 265, 266, 268 UPPER CARGO COMPT 263-LT BS 635, LBL 28. 264- LT BS 635, LBS 48. 265- LT BS 755, LBL 28. 266- LT BS 755, LBL 48. 268- RT BS 637, RBL 48, SEAT TRACKS CRACKED. SEAT TRACKS REPAIRED AS PER SRM 53-70-00.Jan 12, 2000 · N605FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 00FDEA00027Seat Track · crackedSNRM 159 - MAIN DECK - SEAT TRACK FOUND CRACKED AT BS 970.5 X = 47.5 RT CRACK LENGTH APPROX 2 INCHES. REPAIRED SEAT TRACK PER SRM 53-70-00 VOL 1.Jan 11, 2000 · N605FE · Doug MD11F · Fuselage Main, Floor BeamSDR 99FDEA00394Fire Wire · failedSHUTDOWN NR 2 ENG IN FLT DUE TO FIRE WARN IND, DISCHARGED FIRE-X BOTTLE. REMOVED AND REPLACED HARNESSES 420804-0000, 420896-0000, & 224W9727-517. ALSO, REPLACED FIRE-X BOTTLE (P/N 895564-10. RAN ENG, CHECK GOOD.Sep 17, 1999 · N605FE · Doug MD11F · Fire DetectionSDR 99FDEA00317Fire Loop · failed99-196- WHILE CLIMB, ENG NR 2 FIRE ALERT WARNING ACTIVATED. ENG SHUTDOWN IAW FLT MANUAL. NR 2 FIRE AGENT DISCHARGED. REMOVED AND REPLACED UP RT FIRE DET ASSY A, HARNESS OF DH4 TO DH23, DH22 TO DH7, AND DH7 TO DH8 FOR MAINT PREVENTION PER MD-11. RUN ENG WITHAug 6, 1999 · N605FE · Doug MD11F · Fire DetectionSDR 99FDEA00080Keel Beam · damagedUNDERWING KEEL STRUCTURE WAS DAMAGED IN LAND INCIDENT AND HAS BEEN OPER UNDER REPETITIVE INSP PER EA 1-5330-33495 AND 1-5330-39772 BS 1401 TO 1451 Z-60 TO Z-110. *S/D* COMPLIED WITH EA 1-5310-40320 FUSELAGE - UNDERWING KEEL STRUCTURE REPAIR.Feb 7, 1999 · N605FE · Doug MD11F · Fuselage Main, KeelSDR 99FDEA00082Skin · damagedA/C SUSTAINED DAMAGE TO FUSELAGE SKIN DURING LANDING INCIDENT BS 623 FROM L36 TO L48 LT. *S/D* COMPLIED WITH EA 1-5330-40318 FUSELAGE, SKINS-SPLICE REPAIR OF SKIN AT BS 623, L36-L48, LT AND RT.Jan 22, 1999 · N605FE · Doug MD11F · Fuselage Main, Plate/SkinSDR 99FDEA00081Bulkhead · damagedFWD FUSELAGE WAS DAMAGED IN LAND INCIDENT AND HAS BEEN OPER UNDER REPETITIVE INSP PER EA 1-5330-39764. BULKHEAD AT BS 595 WAS STRESSED. *S/D* COMPLIED WITH EA 1-5310-40319- FUSELAGE, MAIN FRAME - REPAIR OF BS 595 PRESSURE BULKHEAD.Jan 19, 1999 · N605FE · Doug MD11F · Fuselage Main, BulkheadSDR 98FDEA00086Wire · failedAFTER TAKEOFF AND GEAR RETRACTION HAD 4 RED GEAR UNSAFE LIGHTS. FOLLOWED EMERGENCY PROCEDURES THAT HAD US CYCLE GEAR SEVERAL TIMES WITH NO SUCCESS. GEAR EXTENDS NORMALLY. VERIFIED PROBLEM WAS WITH INDICATION. WHILE ON GROUND INDICATION DID NOT SHIFT FROM GFeb 5, 1998 · N605FE · Doug MD11F · Landing Gear System WiringSDR 97FDEA00769Control Module · malfunctionedGOT A SLATS DISAGREE WHEN SLAT HANDLE WAS IN THE RETRACT POSITION. RETURNED FLAP HANDLE TO THE 0 DEGREES/EXTEND POSITION AND SLATS INDICATED EXTENDED. FOUND SLAT CONTROL POWER A C1 RESET C/B AND ATTEMPTED TO RETRACT SLATS. GOT THE SAME SLATS DISAGREE ALERT Oct 17, 1997 · N605FE · Doug MD11F · Leading Edge Slat Position Indicating SystemSDR 97FDEA00431Splice · crackedCENTER W/W RT AND LT TRUNNION SUPPORT BOOT STRAP SPLICES CRACKED 5 EA. 1 EA. SPLICE CRACKED 10 INCHES STA 1465, REF SNRM NR N00646. 1 EA BOOT STRAP SPLICE CRACKED 6 INCH AT Y-STA 1489, REF SNRM NR N00648. 1 EA BOOT STRAP SPLICE CRACKED 1 INCH AT Y-STA 1465, Jul 15, 1997 · N605FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 97FDEA00394Spacer · gougedSNRM N00514 REF: TO EO 1-3210-7-3303B-P2. THE RT MAIN GEAR FWD TRUNNION IN COMPLIANCE WITH EO DISCOVERED THAT THE INNER SPACER ASSEMBLY WAS DAMAGED BEYOND LIMITS. DEEP GOUGES AND PITS IN INNER BUSHINGS. CLOSED OFF LUBE PASSAGE. REMOVED AND REPLACED SPACJul 7, 1997 · N605FE · Doug MD11F · Main Landing Gear Attach SectionSDR 97FDEA00393Spacer · gougedSNRM N00517 REF: TO EO 1-3210-7-3303B-P1. LT MAIN GEAR FWD TRUNNION, IN COMPLIANCE WITH EO DISCOVERED THE INNER SPACER ASSEMBLY WAS DAMAGED BEYOND LIMITS. DEEP GOUGES AND PITS, RESTRICTED LUBE PASSAGE. INSTALLED NEW SLEEVE ASSEMBLY PER M/M 32-11-01-04. CJul 7, 1997 · N605FE · Doug MD11F · Main Landing Gear Attach SectionSDR 97FDEA00386Bushings · galledTHE RT MAIN GEAR FORWARD TRUNNION SUPPORT FITTING, BOTH FWD AND AFT BUSHINGS HAVE MINOR GALLING AND SCORING FROM REMOVAL OF PIVOT PIN AT BOTTOM I/B AREA OF BUSHINGS. TRUNNION BUSHINGS MEASURED WITH IN WEAR LIMITS 3.754 PER CMM 32-10-02.Jul 5, 1997 · N605FE · Doug MD11F · Main Landing Gear Attach SectionSDR 97FDEA00384Bushing · galledLT MLG FWD TRUNNION BUSHINGS DON'T HAVE ENOUGH CLEARANCE BETWEEN THEM TO PROVIDE PROPER GREASE CHANNEL PASSAGE. INSTALLED NEW BUSHINGS PER CMM 20-20-07 AND CMM 32-10-02.Jul 5, 1997 · N605FE · Doug MD11F · Main Landing Gear Attach SectionSDR 97FDEA00383Bushings · galledSNRM N00505 REF: TO EO 1-3210-7-3303B-P1, THE LT MAIN GEAR FWD TRUNNION SUPPORT FITTING BOTH FWD AND AFT BUSHINGS HAVE SEVERE GALLING 7 SCORING DURING REMOVAL OF PIVOT PIN, INNER BORE. *S/D* INSTALLED NEW BUSHING IN FWD TRUNNION PER CMM 20-20-07 AND SEALEJul 5, 1997 · N605FE · Doug MD11F · Main Landing Gear Attach SectionSDR 97FDEA00385Bushing · galledRT MLG FWD TRUNNION BUSHINGS DON'T HAVE ENOUGH CLEARANCE BETWEEN THEM TO PROVIDE PROPER GREASE CHANNEL PASSAGE. INSTALLED NEW BUSHINGS PER CMM 20-20-07 AND CMM 32-10-02.Jul 4, 1997 · N605FE · Doug MD11F · Main Landing Gear Attach SectionSDR 97FDEA00372Skin · wrinkledFUSELAGE SKIN WRINKLED AT STA 595 TO 615 LONG 27 TO 47 LEFT SIDE AND AT STA 595 TO 615 LONG 27 TO 47 RIGHT SIDE. ALSO, AT STA 475 LONG 27 RIGHT SIDE AFT OF R1 DOOR. *S/D* MEASURED DEPRESSED AREA OF SKIN DIM IS 6 X 11.080 DENT IS WITHIN LIMITS PER SRM 53-20Jun 27, 1997 · N605FE · Doug MD11F · Fuselage Main, Plate/SkinSDR 97FDEA00198Trim Motor · crackedHYD SYS 3 FAIL ALERT DISPLAYED ON CLIMBOUT, TOTAL LOSS OF HYD QTY, SYSTEM AUTO SHUTDOWN. FOUND HORIZONTAL STAB TRIM MOTOR CRACKED VERTICALLY. REMOVED AND REPLACED HORIZONTAL STAB TRIM MOTOR M1-16. REMOVED AND REPLACED BOTH PUMPS AND FILTERS PER M/M.Mar 20, 1997 · N605FE · Doug MD11F · Stabilizer Control SystemSDR 97FDEA00140Engine · failedDURING FLIGHT THE NUMBER 2 ENGINE HAD AN OIL OVER TEMP AND OIL LOST PROBLEM. THE FLIGHT CREW FOLLOWED THE FLIGHT MANUAL AND SHUT DOWN THE ENGINE IN FLIGHT. REMOVED AND REPLACED THE NUMBER 2 ENGINE.Mar 5, 1997 · N605FE · Doug MD11F · Engine (Turbine/Turboprop)SDR 97FDEA00116Seal · leakingNUMBER 2 ENGINE OIL QUANTITY WENT TO 5 QUARTS APPROXIMATELY 15 MINUTES AFTER TAKEOFF AND CONTINUED TO DROP. ENGINE WAS SHUT DOWN AND A/C RETURNED. FOUND OIL LEAKING FROM GENERATOR STATOR CANNON PLUG. REMOVED AND REPLACED GENERATOR STATOR ASSEMBLY AND PACKINFeb 21, 1997 · N605FE · Doug MD11F · Turbine Engine Oil System
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