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.

SDR FDEA201001220227Valve · failedON CLIMB OUT RECEIVED LVL 2 ALERT TRIM AIR OFF TEMP REACHED 225 F. COCKPIT TEMP 99 F COULD NOT CONTROL TEMP IN AUTO WITH QRH OR MANUAL. TEMP LOWERED TO 190F AND REMAINED THERE UNTIL DECENT. FOUND FD TRIM AIR VALVE STUCK OPEN. PN 398398-3 CURRENTLY NIS ANJan 22, 2010 · N585FE · Doug MD11F · Cabin Temperature Control SystemSDR FDEA201001210205Dimmer · failed500 HRS INTO FLT AT CRUISE FL 360. CREW HEARD AN ARCING SOUND BY THE RT OBSERVERS POSITION, LIGHT SMOKE AND AN ACRID SMELL WERE ALSO NOTED. THE OVER-HEAD SWITCH PANEL LTG (C-30) CIRCUIT BREAKER POPPED AND SMOKE AND FUMES DISAPATED. OVERHEAD PANEL LIGHTS WERE Jan 21, 2010 · N585FE · Doug MD11F · Flight Compartment LightingSDR FDEA201001010002Wire Harness · shortedHAD A TANK 2L AFT PUMP LO ALERT, LEVEL 1 AFTER TAKE OFF FOR ENTIRE FLIGHT. CIRCUIT BREAKER WAS POPPED. FOLLOWED QRH AND KEPT CB OUT. WIRES RUNNING UNDER FLOOR PANELS SHOW SHORT. DISCOVERED DAMAGED AND MELTED WIRE HARNESS UNDER FLOOR PANEL 272CF. ROUTED NEJan 1, 2010 · N585FE · Doug MD11F · Fuel System WiringSDR FDEA200902200600Skin · misrepairedRIGHT WING NR 4 SLAT INNER SURFACE FOUND 03 EACH EXISTING REPAIRED PATCH AT APPROXIMATELY XORS 538. RIGHT WING NR 4 SLAT INNER SURFACE 03 EACH EXISTING DOUBLERS EVALUATED AND FOUND NOT IN ACCORDANCE WITH SRM REPAIR. EXISTING DOUBLERS 03 EACH REMOVED AND REFeb 20, 2009 · N585FE · Doug MD11F · Leading Edge DevicesSDR FDEA200902200599Skin · misrepairedFUSELAGE SKIN EXTERNAL FOUND WITH EXISTING DOUBLER REPAIRS AT STA 1801 LONGERON 37 RIGHT. FUSELAGE SKIN REPAIR AT STA 1801 LONGERON 37 RIGHT EVALUATED AND FOUND NOT IN ACCORDANCE WITH SRM 53-20-00 FIGURE 2 VOLUME I. EXISTING DOUBLER REPAIR AT FUSELAGE SKINFeb 20, 2009 · N585FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA200902200598Skin · misrepairedFUSELAGE SKIN EXTERNAL FOUND WITH EXISTING DOUBLER REPAIRS AT STA 1896 LONGERON 42 LT. REPAIR DOUBLER EVALUATED AND FOUND NOT IAW SRM 53-20-00 VOLUME I. EXISTING REPAIR DOUBLERS REMOVED AND NEW REPAIR CARRIED OUT AS PER SRM 53-20-00 FIGURE 2, VOLUME IEO NRFeb 20, 2009 · N585FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA200902190596Panel · corrodedLEFT STA 1229, XCW = 8 TO 20 CENTER WING UPPER PANEL FOUND CORROSION. REPAIRED AS PER EA NR 1-5710-127459, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Feb 19, 2009 · N585FE · Doug MD11F · Wing, Center BoxSDR FDEA200902190595Skin · corrodedRIGHT STA 1229, XCW = -8 CENTER WING UPPER PANEL FOUND CORROSION. REPAIRED AS PER EA NR 1-5710-127459, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Feb 19, 2009 · N585FE · Doug MD11F · Wing, Center BoxSDR FDEA200902190594Skin · corrodedRIGHT STA 1229, XCW = -46 TO -48 CENTER WING UPPER PANEL FOUND CORROSION. REPAIRED AS PER EA. NR 1-5710-127459, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Feb 19, 2009 · N585FE · Doug MD11F · Wing, Center BoxSDR FDEA200902190576Skin · corrodedMAIN DECK CARGO COMPARTMENT, CENTER WING UPPER SKIN PANEL STA 1229, X = - 50 TO X = - 80 FOUND WITH CORROSION AROUND FASTENER HEAD. REPAIRED AS PER E.A. NO. 1-5710-127459, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Feb 19, 2009 · N585FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200902190575Skin · corrodedMAIN DECK CARGO COMPARTMENT, CENTER WING UPPER SKIN PANEL STA 1229 X = -80 TO X = -100 FOUND WITH CORROSION AROUND FASTENER HEAD. REPAIRED AS PER EA NR 1-5710-127459, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Feb 19, 2009 · N585FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200902170571Skin · cracked17 FASTENER HOLES FOUND CRACK INDICATION DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT RIGHT WING LOWER SKIN ACCESS DOOR CUT- OUT BETWEEN XORS 690 AND XORS 700. COMPLIED WITH EA 1-5710-127455, CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-100.Feb 17, 2009 · N585FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200902170570Skin · cracked09 FASTENER HOLES FOUND CRACK INDICATION DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUT- OUT BETWEEN XORS 690 TO XORS 700. REAMED AND REPAIR CARRIED OUT AS PER EA 1-5710-127454, REPAIR CLASSIFIED AS MINOR AFeb 17, 2009 · N585FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200902160552Spar Cap · corrodedRIGHT WING UPPER SURFACE TRAILING EDGE REAR SPAR AREA APPROXIMATELY XORS 981 FOUND CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND OUT OF LIMIT AS PER SRM 57-10-00 FIGURE 17 VOLUME I. REPAIR CARRIED OUT ON REWORK AREA AS PER EA 1-5710-12Feb 16, 2009 · N585FE · Doug MD11F · Wing SparSDR FDEA200902160551Spar Cap · corrodedRIGHT WING UPPER SURFACE REAR SPAR CAP AT APPROXIMATELY XORS 1042 FOUND CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND OUT OF LIMIT AS PER SRM 57-10-00 FIGURE 17 VOLUME I. REPAIR CARRIED OUT ON REWORK AREA AS PER EA NR 1-5710-128576. Feb 16, 2009 · N585FE · Doug MD11F · Wing SparSDR FDEA200902160550Hinge Bracket · corrodedLEFT OUTBOARD FLAP INBOARD HINGE (WING MOUNTED) SIDE LINK ATTACHMENT LOWER SPOT FACE FOUND CORROSION. REWORKED AS PER SOPM 20-11-02. FOUND WITHIN LIMIT AS PER DRAWING NR ARC0502 AND CMM 57-44-08 FIGURE 604 REWORK LIMITS MINIMUM THICKNESS. REPAIR CLASSIFIEDFeb 16, 2009 · N585FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200902160549Hinge Bracket · corrodedRIGHT OUTBOARD FLAP INBOARD HINGE (WING MOUNTED) SIDE LINK ATTACHMENT SPOT FACE FOUND CORROSION. REWORKED AS PER SOPM 20-11-02. FOUND WITHIN LIMIT AS PER DRAWING ARC0502 AND CMM 57-44-08 FIGURE 604 REWORK LIMIT. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Feb 16, 2009 · N585FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200902160548Longeron Splice · crackedMAIN DECK CARGO COMPARTMENT, FUSELAGE LEFT LONGERON SPLICE AT STA 1651 LONGERON 13 FOUND CRACKED APPROXIMATELY 3 INCHES. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. NEW LONGERON SPLICE FABRICATED AS PER DRAWING AFA7181. REPAIR CLASSIFIED AS MAJOR ASFeb 16, 2009 · N585FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA200902160547Frame · dentedMAIN DECK CARGO COMPARTMENT, FUSELAGE RIGHT MAIN FRAME STA 1741 LONGERON 12 FOUND WITH DENT. REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPETITIVE INSPECTION TO BE CARRIED OUT AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM Feb 16, 2009 · N585FE · Doug MD11F · Fuselage Main, FrameSDR FDEA200902160546Frame · dentedMAIN DECK CARGO COMPARTMENT, FUSELAGE RIGHT MAIN FRAME STA 1681 LONGERON 12 FOUND WITH DENT. REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPETITIVE INSPECTION TO BE CARRIED OUT AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM Feb 16, 2009 · N585FE · Doug MD11F · Fuselage Main, FrameSDR FDEA200902160545Support Fitting · crackedCRACK INDICATION FOUND ON FIRST AND SECOND LAYER WEB FROM TOP DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON 0.520 INCH HOLE AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLE NR D. REPAIRED AS PER EA 1-5310-127450, REPAIR CLASSIFIED AS MAFeb 16, 2009 · N585FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200902160544Support Fitting · crackedCRACK INDICATION FOUND ON SECOND LAYER WEB FROM TOP DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON 0.520 INCH HOLE AT MAIN CARGO DOOR LOWER JAMB NR 6 SUPPORT FITTING AT HOLE NR D.Feb 16, 2009 · N585FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200902160543Support Fitting · crackedCRACK INDICATION FOUND ON SECOND LAYER WEB FROM TOP DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON 0.520 INCH HOLE AT MAIN CARGO DOOR LOWER JAMB NR 1 SUPPORT FITTING AT HOLE NR A. REPAIRED AS PER EA 1-5310-127450, REPAIR CLASSIFIED AS MAJOR AS PEFeb 16, 2009 · N585FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200902160542Skin · corrodedRIGHT HORIZONTAL STABILIZER BODY FAIRING ENCLOSED AREA AT STA 2164 FOUND WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II. REPAIR CARRIED OUT AS PER SRM 53-20-00 VOLUME I FIGURE 13. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Feb 16, 2009 · N585FE · Doug MD11F · Horizontal Stabilizer StructureSDR FDEA200902160541Hinge Bracket · corrodedRIGHT OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED) ACTUATOR ATTACHMENT LUG INBOARD BORE FOUND CORROSION. REWORKED AS PER EA 1-5750-127448, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Feb 16, 2009 · N585FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200902160540Hinge Bracket · corrodedLEFT OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED) SIDE LINK ATTACHMENT LOWER SPOT FACE FOUND CORROSION. REWORKED AS PER SOPM 20-11-02. FOUND WITHIN LIMIT AS PER DRAWING NR ARC0503 AND CMM 57-44-09 FIGURE 601 REWORK LIMITS. REPAIR CLASSIFIED AS MINOR AS PER GFeb 16, 2009 · N585FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200902160539Hinge Bracket · corrodedLEFT OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED) ACTUATOR ATTACHMENT INBOARD LUG BORE FOUND CORROSION. REWORKED AS PER EA 1-5750-127449, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Feb 16, 2009 · N585FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200902160538Hinge Bracket · corrodedLEFT OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED) ACTUATOR ATTACHMENT OUTBOARD LUG BORE FOUND CORROSION. REWORKED AS PER EA 1-5750-127449, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Feb 16, 2009 · N585FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200902150537Hinge Bracket · corrodedLEFT OUTBOARD FLAP INBOARD HINGE (WING MOUNTED) ACTUATOR ATTACHMENT LUG INBOARD, BORE FOUND CORROSION. REWORKED AS PER EA 1-5750-127447, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Feb 15, 2009 · N585FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200902150536Hinge Bracket · corrodedRIGHT OUTBOARD FLAP INBOARD HINGE (WING MOUNTED) ACTUATOR ATTACHMENT LUG OUTBOARD, BORE FOUND CORROSION. REWORKED AS PER EA 1-5750-127446, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Feb 15, 2009 · N585FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200902150535Hinge Bracket · corrodedRIGHT OUTBOARD FLAP INBOARD HINGE (WING MOUNTED) ACTUATOR ATTACHMENT LUG INBOARD, BORE FOUND CORROSION. REWORKED AS PER EA 1-5750-127446, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Feb 15, 2009 · N585FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200902150534Support Fitting · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON EXISTING 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLES NR B, NR C AND NR D. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFFeb 15, 2009 · N585FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200902150533Support Fitting · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON EXISTING 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 6 SUPPORT FITTING AT HOLES NR A, NR B, NR C AND NR D. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CFeb 15, 2009 · N585FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200902150532Support Fitting · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON EXISTING 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 5 SUPPORT FITTING AT HOLES NR B AND NR C. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIFeb 15, 2009 · N585FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200902150531Support Fitting · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON EXISTING 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 4 SUPPORT FITTING AT HOLES NR B AND NR C. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED ASFeb 15, 2009 · N585FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200902150530Door Frame · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON EXISTING 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 3 SUPPORT FITTING AT HOLES NR A, NR C AND NR D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I.Feb 15, 2009 · N585FE · Doug MD11F · Fuselage Main, StructureSDR FDEA200902150529Fitting · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON EXISTING 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 2 SUPPORT FITTING AT HOLES NR A, NR C AND NR D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I.Feb 15, 2009 · N585FE · Doug MD11F · Cargo/Baggage DoorsSDR FDEA200902150528Support Fitting · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON EXISTING 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 1 SUPPORT FITTING AT HOLES NR A, NR B, NR C AND NR D. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CFeb 15, 2009 · N585FE · Doug MD11F · Fuselage Main, StructureSDR FDEA200902150527Seat Track · corrodedMAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA 1341, X = 8.5 FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1, VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Feb 15, 2009 · N585FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200902150526Seat Track · corrodedMAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA 1079, X = -8.5 FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1, VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Feb 15, 2009 · N585FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200902150525Seat Track · corrodedMAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA 5-65, X = -27.5 FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Feb 15, 2009 · N585FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200902150524Seat Track · corrodedMAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA 5-65, X = 27.5 FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1, VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Feb 15, 2009 · N585FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200902150523Seat Track · crackedMAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA 1661, X = -47.5 FOUND CRACKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1, VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Feb 15, 2009 · N585FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200902150522Vane · delaminatedRIGHT WING INBOARD FLAP, FLAP VANE LOWER SURFACE FOUND DELAMINATED FROM CENTER TO OUTBOARD VANE TRACK. REMOVED AND REPLACED AS PER AMM 27-50-22-4. RT WING INBOARD FLAP VANE ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-5 FOUND STISFACTORY.Feb 15, 2009 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 08FDEA04230Retainer · crackedLEFT FWD EMERGENCY EXIT HATCH, SEAL RETAINERS, TWO RETAINERS CRACKED REPLACED LOWER AFT AND LOWER FWD SEAL RETAINERS ON LT FWD EMERGENCY EXIT HATCH REF DWG 50-7978 AND SRM 51-30-2 THIS IS CLASSIFIED AS A MINOR REPAIR.Oct 6, 2008 · N585FE · Doug MD11F · Emergency ExitsSDR 07FDEA03239Longeron · corrodedRIGHT WING TO FUSELAGE BODY FAIRING LONGERON 27, STA 1305 FOUND WITH CORROSION. 09-11-07 RIGHT HAND WING TO FUSELAGE BODY FAIRING LONGERON REMOVED & REPLACED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Aug 30, 2007 · N585FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 07FDEA03237Skin · damagedAFTER LEFT WING UPPER FUELTANK PANEL NR 531AT CUTOUT RUBSTRIP REMOVED. FOUND SKIN CUTOUT WITH 02 EACH DOUBLE HOLES. 09-11-07 COMPLIED WITH FEDEX E.A. 1-5710-115177, CLASSIFIED AS A MINOR REPAIR AS PER FEDEX GMM 6-2-100.Aug 30, 2007 · N585FE · Doug MD11F · Wing, Plate/SkinSDR 07FDEA03167Vane · corrodedLEFT WING, OUTBOARD FLAP VANE INSIDE OF LEADING EDGE ACCESS HOLE FOUND CORRODED. 09-11-07 REMOVED AND REPLACED AS PER AMM 27-50-32-4. ADJUSTMENT CARRIED OUT AS PER AMM 27-50-32-5 FOUND SATISFACTORY. LH WING OUTBOARD FLAP OPERATION CHECK CARRIED OUT AAug 28, 2007 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 07FDEA03160Strap · crackedLEFT WING, OUTBOARD FLAP INBOARD HINGE TENSION STRAP FOUND CRACKED. 09-12-07 REMOVED AND REPLACED AS PER FEDEX E.O. 1-5750-7-5004 PT1, REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Aug 27, 2007 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 07FDEA03159Structure · chafedRT WING FIXED LEADING EDGE BETWEEN XOS 680 TO XOS 717 FOUND CHAFING MARK. 09-11-07 REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG.15 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Aug 27, 2007 · N585FE · Doug MD11F · Wing Main, Frame Structure
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