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 06FDEA0658Stringer · crackedLT WING TANK, APPROXIMATELY TEN (10) INCHES LONG CRACK FOUND ON OUTBOARD END OF STRINGER 10 DURING HFEC INSPECTION. REPAIRED AS PER 57-20-00 VOLUME I, FIGURE 10. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Feb 13, 2006 · N585FE · Doug MD11F · Wing, Longeron/StringerSDR 04FDEA02891Bracket · misalignedMAIN DECK, NEW ANGLE BRACKET P/N ADA3548-1 FOR INTERCOSTAL ADA8392-1 INSTALLATION AT STA Y= 775 TO STA Y= 791.75 LONGERON 7L FOUND MISALIGNED WITH FUSELAGE TRANSVERSE FRAME EXISTING HOLE. NEW ANGLE BRACKET FABRICATED PER DAC DWG ADA3852 AND PART MARKED P/N FXOct 7, 2004 · N585FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 04FDEA02869Relay · defectiveCABIN EMERGENCY LIGHTING NOT ILLUMINATED WHEN SWITCHED (ON). CABIN EMERGENCY LIGHTING TROUBLESHOOTING CARRIED OUT IAW FIM 33-51-00. FOUND RELAY R2-5700 AT FAULT. REMOVED AND REPLACED RELAY R2-5700 IAW STANDARD WIRING PRACTICES. OPERATIONAL CHECK CARRIEDOct 5, 2004 · N585FE · Doug MD11F · Emergency LightingSDR 04FDEA02867Segment · corrodedENGINE NR 2 INLET BELLMOUTH TRANSITION RING LOWER SURFACE FOUND WITH CORROSION. ENGINE NR 2 INLET BELLMOUTH TRANSITION RING LOWER SURFACE CORROSION REPAIR CARRIED OUT.Oct 4, 2004 · N585FE · Doug MD11 · Engine Air Intake SystemSDR 04FDEA02863Structure · crackedLEFT WING, OUTBOARD FLAP, INBOARD AFT HINGE LOCATION MID ATTACHMENT FITTING SUSPECTED CRACKED. LEFT WING, OUTBOARD FLAP ASSEMBLY P/N NRC6753-503. REMOVED AND REPLACED PER AMM 27-50-30.Oct 1, 2004 · N585FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02846Line · crackedCENTER CARGO COMPARTMENT, LEFT SIDEWALL AREA AT APPROXIMATELY AT STA Y= 1801, A CRACKED OF 1 1/4 INCH FOUND AT THE FUEL SHROUD LINE. CENTER CARGO COMPARTMENT, LEFT SIDEWALL AREA AT APPROXIMATELY AT STA Y= 1801, 1 1/4 INCH CRACKED AT THE FUEL SHROUD LINE REPAISep 29, 2004 · N585FE · Doug MD11F · Aircraft Fuel Distribution SystemSDR 04FDEA02845Line · crackedCENTER CARGO COMPARTMENT, LT SIDEWALL AREA AT APPROXIMATELY AT STA Y= 1781, A CRACKED OF 1.1/8 INCH FOUND AT THE FUEL SHROUD LINE. CENTER CARGO COMPARTMENT, LEFT SIDEWALL AREA AT APPROXIMATELY AT STA Y= 1781, 1 1/8 INCH CRACKED AT THE FUEL SHROUD LINE. REPAISep 29, 2004 · N585FE · Doug MD11F · Aircraft Fuel Distribution SystemSDR 04FDEA02841Longeron · crackedCENTER CARGO, LONGERON 39R LOCATED BETWEEN STA Y= 1887 TO Y= 1902 FOUND WITH CORROSION CRACK. CENTER CARGO, LONGERON 39R LOCATED BETWEEN STA Y= 1887 TO Y= 1902. REMOVED PER SRM 53-10-00 VOLUME I. NEW LONGERON FABRICATED PER DRAWING NR: AFA7093. REPAIR SPLSep 29, 2004 · N585FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 04FDEA02812Frame · dentedTRANSVERSE FRAME AT LT STA Y= 1701 BETWEEN LONGERON 12L AND 13L DENTED BY CARGO IMPINGEMENT. REPAIRED PER SRM 53-30-00 VOLUME I FIGURE 1. INITIAL INSPECTION TO BE CARRIED OUT AT 22, 951 CYCLES AND REPETITIVE INSPECTION THEREAFTER EVERY 9, 500 FLIGHT CYCLES Sep 23, 2004 · N585FE · Doug MD11F · Fuselage Main, FrameSDR 04FDEA02811Frame · dentedTRANSVERSE FRAME AT LT STA Y= 1721 BETWEEN LONGERON 12L AND 13L DENTED BY CARGO IMPINGEMENT. INITIAL INSPECTION TO BE CARRIED OUT AT 22, 951 FLIGHT CYCLES AND REPETITIVE INSPECTION THEREAFTER EVERY 9, 500 FLIGHT CYCLES PER THE GUIDELINES OF MD-11 SRM 53-Sep 23, 2004 · N585FE · Doug MD11F · Fuselage Main, FrameSDR 04FDEA02809Hinge · corrodedLT WING, IB FLAP, OB AFT HINGE PIVOT HOLE IB SPOTFACE CORRODED. CORROSION REMOVED AND FOUND WITHIN LIMITS PER CMM 57-52-03.Sep 23, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02808Hinge · corrodedLT WING, IB FLAP, OB AFT HINGE IB PIVOT HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMTS PER CMM 57-52-03, PAGES 442 TO 443. ORIGINAL DIAMETER= 1.289, FINAL DIAMETER= 1.291. COMPLIED WITH FEDEX EA 1-5750-79749Sep 23, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02807Hinge · corrodedRT WING, IB FLAP, OB AFT HINGE PIVOT HOLE OB SPOTFACE CORRODED. CORROSION REMOVED AND FOUND WITHIN LIMITS PER CMM 57-52-03.Sep 23, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02806Hinge · corrodedRT WING, IB FLAP, OB AFT HINGE OB PIVOT HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMTS PER CMM 57-52-03, PAGES 442 TO 443. ORIGINAL DIAMETER = 1.249, FINAL DIAMETER = 1.257. COMPLIED WITH FEDEX EA 1-5750-79749,Sep 23, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02805Hinge · corrodedRT WING, IB FLAP, OB AFT HINGE PIVOT HOLE IB SPOTFACE CORRODED. CORROSION REMOVED AND FOUND WITHIN LIMITS PER CMM 57-52-03 PAGES 442 TO 443.Sep 23, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02804Hinge · corrodedRT WING, IB FLAP, OB AFT HINGE IB PIVOT HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMTS PER CMM 57-52-03, PAGES 442 TO 443. ORIGINAL DIAMETER= 1.251, FINAL DIAMETER= 1.314. COMPLIED WITH FEDEX EA 1-5750-79749,Sep 23, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02792Stop Fitting · crackedLEFT WING, OUTBOARD FLAP ATTACHMENT STOP FITTING FOUND CRACKED. LEFT WING, OUTBOARD FLAP ASSEMBLY P/N NRC6753-503. REMOVED AND REPLACED PER AMM 27-50-30.Sep 21, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02791Hinge Bracket · corrodedRT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD SPOTFACE ATTACHMENT CORRODED. RT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD SPOTFACE ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINSep 21, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02790Hinge Bracket · corrodedRT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD ATTACHMENT CORRODED. RT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.187 Sep 21, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02785Hinge Bracket · corrodedRT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, INBOARD PIVOT HOLE SPOTFACE CORRODED. RT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, INBOARD PIVOT HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.504 INCH, REMAINING THICKNESep 21, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02789Hinge · corrodedRT WING, OB FLAP, OB AFT HINGE ACTUATOR ROD END HOLE, IB SPOTFACE ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 21, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02788Hinge · corrodedRT WING, OB FLAP, OB AFT HINGE ACTUATOR ROD END HOLE IB ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 21, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02787Hinge · corrodedRT WING, OB FLAP, OB AFT HINGE, OB PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 21, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02786Hinge · corrodedRT WING, OB FLAP, OB AFT HINGE, OB PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 21, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02759Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE INBOARD ATTACHMENT CORRODED. LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE INBOARD ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.18Sep 20, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02757Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE OUTBOARD ATTACHMENT CORRODED. LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE OUTBOARD ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.Sep 20, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02755Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, INBOARD PIVOT HOLE CORRODED. LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, INBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.093 INCH, FINAL DIAMETER=1.095 INCH AND REPASep 20, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02753Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT OUTBOARD HOLE CORRODED. LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT OUTBOARD HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.079 INCH, FINAL DIAMETER=1.081 INCH AND REPASep 20, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02751Splice · crackedCENTER ACCESSORY COMPARTMENT, LONGERON 38R END SPLICE AT BETWEEN STA Y= 6-100 TO STA Y= 1139 CRACKED. CRACKED AREA AT CENTER ACCESSORY COMPARTMENT, LONGERON 38R END SPLICE AT BETWEEN STA Y= 6-100 TO STA Y= 1139 TRIMMED OUT AS PER SRM 53-00-01 VOL I AND EA NSep 20, 2004 · N585FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 04FDEA02750Stringer · crackedAFT CARGO, WASTE TANK AT STA Y= 1988 STRINGER END NR 45L FROM BOTTOM SUSPECT CRACKED. AFT CARGO, WASTE TANK AT STA Y= 1988 STRINGER END NR 45L SPLICE FITTING. REMOVED AND REPLACED PER SRM 51-31-01 VOLUME II.Sep 20, 2004 · N585FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 04FDEA02768Hinge Bracket · corrodedRT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, INBOARD ATTACHMENT CORRODED. RT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, INBOARD ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.187 INCHSep 20, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02767Hinge Bracket · corrodedRT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, INBOARD SPOTFACE ATTACHMENT CORRODED. RT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, INBOARD SPOTFACE ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL TSep 20, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02766Hinge Bracket · corrodedRT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, OUTBOARD ATTACHMENT CORRODED. RT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, OUTBOARD ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.187 INSep 20, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02764Hinge Bracket · corrodedRT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, OUTBOARD SPOTFACE ATTACHMENT CORRODED. RT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, OUTBOARD SPOTFACE ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINSep 20, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02763Hinge Bracket · corrodedRT WING, OUTBOARD FLAP, INBOARD HINGE INBOARD PIVOT HOLE CORRODED. RT WING, OUTBOARD FLAP, INBOARD HINGE INBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.093 INCH, FINAL DIAMETER=1.096 INCH AND REPAIRED AS PER EA NSep 20, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02762Hinge Bracket · corrodedRT WING, OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORRODED. RT WING, OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.503 INCH, REMAINING THICKNESS=0Sep 20, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02761Hinge Bracket · corrodedRT WING, OUTBOARD FLAP, INBOARD AFT HINGE OUTBOARD PIVOT HOLE CORRODED. RT WING, OUTBOARD FLAP, INBOARD AFT HINGE OUTBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.089 INCH, FINAL DIAMETER=1.091 INCH AND REPAIRED ASep 20, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02760Hinge Bracket · corrodedRT WING, OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORRODED. RT WING, OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.505 INCH, REMAINING THICKNESSSep 20, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02758Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE INBOARD SPOTFACE ATTACHMENT CORRODED. LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE INBOARD SPOTFACE ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGSep 20, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02756Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE OUTBOARD SPOTFACE ATTACHMENT CORRODED. LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE OUTBOARD SPOTFACE ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. Sep 20, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02754Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORRODED. LT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.501 INCH, REMAINING THICKNESep 20, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02752Hinge Bracket · corrodedLT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORRODED. LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.509 INCH, REMAINING THICKNSep 20, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02784Hinge · corrodedRT WING, OB FLAP, OB AFT HINGE, IB PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 20, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02782Hinge · corrodedSNRM NR N0486- LT WING, OB FLAP, IB AFT HINGE ACTUATOR ROD END HOLE, IB ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.189 AND REPAIRED AS PER EA#1-5750-79749.Sep 20, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02781Hinge · corrodedLT WING, OB FLAP, IB AFT HINGE ACTUATOR ROD END HOLE, IB SPOTFACE ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 20, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02780Hinge · corrodedSNRM NR N0488- LT WING, OB FLAP, IB AFT HINGE ACTUATOR ROD END HOLE, OB ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.189 AND REPAIRED AS PER EA1-5750-79749.Sep 20, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02779Hinge · corrodedLT WING, OB FLAP, IB AFT HINGE ACTUATOR ROD END HOLE, OB SPOTFACE ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 20, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02778Hinge · corrodedLT WING, OB FLAP, IB AFT HINGE IB PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 20, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02777Hinge · corrodedLT WING, OB FLAP, IB AFT HINGE PIVOT HOLE, IB SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 20, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02776Hinge · corrodedSNRM NR N0483 LT WING, OB FLAP, IB AFT HINGE OB PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 20, 2004 · N585FE · Doug MD11F · Trailing Edge Flaps
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