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 07FDEA03158Structure · chafedRIGHT WING FIXED LEADING EDGE XOS 717 TO XOS 774 FOUND CHAFED 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 StructureSDR 07FDEA03157Longeron · crackedHFEC INSPECTION CARRIED OUT FOUND 01 EACH LOWER FASTENER HOLE ON THE LONGERON WITH CRACK INDICATION LOCATED NEAR THE RIGHT NOSE LANDING GEAR TRUNNION FITTING, APPROX TOTAL LENGTH OF 3/8 INCH LENGTH. 09-12-07 LONGERON LOCATED NEAR THE RIGHT HAND NOSE LANDINAug 27, 2007 · N585FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 07FDEA03156Longeron · crackedHFEC INSPECTION CARRIED OUT FOUND 01 EACH LOWER FASTENER HOLE ON THE LONGERON WITH CRACK INDICATION LOCATED NEAR THE LEFT NOSE LANDING GEAR TRUNNION FITTING, APPROX TOTAL LENGTH OF 1/2 INCH LENGTH. 09-12-07 COMPLIED WITH FEDEX E.A. 1-5310-115173, REPAIAug 27, 2007 · N585FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 07FDEA03155Spar Cap · corrodedLEFT WING, TRAILING EDGE REAR SPAR UPPER CAP AT STATION XORS 1042 FOUND CORRODED. COMPLIED WITH FEDEX E.A. 1-5710-115175, CLASSIFIED AS A MINOR REPAIR AS PER FEDEX GMM 6-2-100.Aug 27, 2007 · N585FE · Doug MD11F · Wing SparSDR 07FDEA03154Skin · dentedLEFT WING, NR 5 SLAT LEADING EDGE AREA FOUND WITH DENT. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG. 5 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Aug 27, 2007 · N585FE · Doug MD11F · Leading Edge DevicesSDR 07FDEA03135Fitting · crackedLEFT WING, OUTBOARD FLAP LEADING EDGE STOP BOLT FITTING FOUND CRACKED. 09-12-07 REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II. REPAIR CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.Aug 27, 2007 · N585FE · Doug MD11F · Leading Edge DevicesSDR 07FDEA03134Doubler · crackedCENTER LANDING GEAR STATION 1341.0 RIGHT DOUBLER FOUND CRACKED. 09-12-07 REMOVED AND REPLACED AS PER SRM 51-33-01 VOL.II. REPAIR CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.Aug 26, 2007 · N585FE · Doug MD11F · Fuselage Main, Plate/SkinSDR 07FDEA03133Doubler · crackedCENTER LANDING GEAR STATION 1341.0 LEFT DOUBLER FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Aug 26, 2007 · N585FE · Doug MD11F · Fuselage Main, Plate/SkinSDR 07FDEA03130Slat Track · crackedLEFT WING, FIXED LEADING EDGE NR 10 SLAT TRACK CUTOUT INBOARD CORNER FOUND CRACKED. 09-11-07 REPAIR CARRIED OUT AT LEFT HAND WING : FIXED LEADING EDGE NR 10 SLAT TRACK CUTOUT INBOARD CORNER AREA AS PER SRM 57-10-00 FIG. 21 VOL I. CLASSIFIED AS MAJOR REPAug 25, 2007 · N585FE · Doug MD11F · Leading Edge DevicesSDR 07FDEA03129Stringer · crackedLEFT WING LEADING EDGE CAVITY AREA STRINGER AT STATION XOS 790 FOUND CRACKED. 09-11-07 COMPLIED WITH FEDEX EA. 1-5710-115148, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.Aug 25, 2007 · N585FE · Doug MD11F · Wing, Longeron/StringerSDR 07FDEA03128Trunnion · crackedNOSE LANDING GEAR RIGHT TRUNNION FITTING SUSPECT CRACKED. 09-11-07 NOSE LANDING GEAR RIGHT HAND TRUNNION FITTING REPAIR CARRIED OUT AS PER SRM 53- 40-00 FIG. 23 VOL I. REPETITIVE INSPECTION REQUIRED FOR CRACK GROWTH AT NOT TO EXCEED 1500 LANDING INTERVAAug 25, 2007 · N585FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR 07FDEA03127Trunnion · crackedNOSE LANDING GEAR LEFT TRUNNION FITTING FOUND CRACKED. 09-11-07 NOSE LANDING GEAR LEFT HAND TRUNNION FITTING REPAIR CARRIED OUT AS PER SRM 53-40- 00 FIG. 23 VOL I. REPETITIVE INSPECTION REQUIRED FOR CRACK GROWTH AT NOT TO EXCEED 1500 LANDING INTERVALS. REAug 25, 2007 · N585FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR 07FDEA03126Stringer · crackedRIGHT WING LEADING EDGE CAVITY STRINGER AT XOS 789 FOUND CRACKED. COMPLIED WITH FEDEX E.A. 1-5710-115149, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.Aug 25, 2007 · N585FE · Doug MD11F · Wing, Longeron/StringerSDR 07FDEA03125Stringer · crackedRIGHT WING LEADING EDGE CAVITY STRINGER AT XOS 667 FOUND CRACKED. COMPLIED WITH FEDEX E.A. 1-5710-115147, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.Aug 25, 2007 · N585FE · Doug MD11F · Wing, Longeron/StringerSDR 07FDEA00578Element · failedAPU FIRE ALARM AND LIGHT CAME ON WITH APU FIRE LEVEL 3 ALERT AT 12000 FEET DESCENT ONTO FINAL APPROACH PULLED APU FIRE HANDLE AND DISCHARGED FIRE BOTTLE LIGHT WENT OUT AFTER 30 SECONDS BLEED AIR NR 2 AND NR 2 PACK AUTO SHUT DOWN. APU COMPARTMENT INSPECTION REFeb 25, 2007 · N585FE · Doug MD11 · Smoke DetectionSDR 06FDEA03441Wire · burnedLEVEL-1 ALERT TANK 2L AFT PUMP LOW. TANK 2L LT AFT CB POPPED. REPLACED NR 2 L PUMP IAW MM 28-22-01-4 NO HELP. REMOVED ELC TERMINAL FROM R2-56 2X AND CB STAYED IN. REINSTALLED ORIGINAL NR 2 L PUMP IAW MM 28-22-01-4. FOUND ELECTRICAL WIRES BURNED UNDER Sep 26, 2006 · N585FE · Doug MD11 · Fuselage Main, Bulkhead Fuselage wiringSDR 06FDEA1316Cadc · malfunctionedLOSS OF CADC 1 AFTER V1. RAN CLIST AND RETURN TO WSSS. REMOVED AND REPLACED NR 1 CADC AS PER MM 34-16-01-4, PERFORMED CADC NR 1 OPS TEST & CAT III RTS AS PER MM 34-16-01-5. PITOT STATIC TEST AS PER MM 34-11-00-2 CHK SATIS. A/C OK FOR SERVICE. PREMATURE RApr 5, 2006 · N585FE · Doug MD11 · Air Data ComputerSDR 06FDEA1263Trunnion · corrodedCENTER LANDING GEAR LEFT AFT MOUNTING HOLE FOUND WITH CORROSION AFTER LANDING GEAR REMOVAL. COMPLIED WITH FEDEX EA 1-5340-94620, FUSELAGE ATTACH FITTINGS CTR. LANDING GEAR TRUNNION SUPPORT FITTING CORROSION REWORK. REPAIR CLASSIFIED AS MAJOR REPAIR AS PER Mar 29, 2006 · N585FE · Doug MD11 · Fuselage, Landing Gear Attach FittingsSDR 06FDEA1262Trunnion · corrodedFOUND CENTER LANDING GEAR LEFT AFT MOUNTING HOLE FOUND WITH CORROSION AFTER LANDING GEAR REMOVAL. COMPLIED WITH FEDEX EA 1-5340-94620, FUSELAGE - ATTACH FITTINGS CTR. LANDING GEAR TRUNNION SUPPORT FITTING CORROSION REWORK. REPAIR CLASSIFIED AS MAJOR REPAIRMar 29, 2006 · N585FE · Doug MD11 · Fuselage, Landing Gear Attach FittingsSDR 06FDEA1218Trunnion · corrodedCENTER LANDING GEAR LEFT MOUNTING AREA LOWER SURFACE FOUND WITH SURFACE CORROSION AFTER LANDING GEAR REMOVAL. COMPLIED WITH FEDEX EA 1-5340-94620 FUSELAGE ATTACH FITTINGS CTR. LANDING GEAR TRUNNION SUPPORT FITTING CORROSION REWORK. REPAIR CLASSIFIED AS MAJMar 24, 2006 · N585FE · Doug MD11 · Fuselage, Landing Gear Attach FittingsSDR 06FDEA1150Roller · gougedLEFT HAND WING, INBOARD FLAP AFT UPPER ROLLER FITTING FOUND WITH GOUGED MARK AFTER REMOVAL FOR ROLLER REPLACEMENT. GOUGED MARK ON LEFT HAND WING, INBOARD FLAP AFT UPPER ROLLER FITTING REMOVED AND NEW SHOULDER BUSHING FABRICATED AND INSTALLED PER FEDEX EA 1- Mar 19, 2006 · N585FE · Doug MD11 · Trailing Edge FlapsSDR 06FDEA1151Skin · damagedLEFT HAND HORIZONTAL STABILIZER, CENTER PLANK UPPER SKIN AT STA XE=51.000 STRINGER 6, FOUND HOLE ELONGATED. COMPLIED WITH STEP 47 OF FEDEX EA 1-5510-94597.Mar 19, 2006 · N585FE · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR 06FDEA1113Seat Track · crackedFORWARD CARGO COMPARTMENT CEILING PANEL AREA, MAIN DECK SEAT TRACK AT STA 695.0, X= 27 SUSPECTED CRACKED. MAIN DECK SEAT TRACK AT STA 665.00 AND STA 745.00, X= 27 REPAIRED AS PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Mar 15, 2006 · N585FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA1008Skin · dentedLEFT INBOARD TRAILING EDGE FLAP LOWER SURFACE FOUND WITH DENTS AT OUTBOARD MID AREA. REPAIRED AS PER SRM 57-10-00 VOLUME I, FIGURE 2. CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100.Mar 12, 2006 · N585FE · Doug MD11 · Trailing Edge FlapsSDR 06FDEA0987Skin · crackedRIGHT HAND WING NR 3 SLAT TELESCOPIC ANTI-ICE LEADING EDGE SPRING CUTOUT AREA UPPER CORNER CRACKED. CURRENT SRM REPAIR IS ONLY APPLICABLE FOR LOWER SURFACE AREA OF THE WING FIXED LEADING EDGE CUTOUT AREAS. COMPLIED WITH FEDEX EA 1-5740-94606.Mar 8, 2006 · N585FE · Doug MD11 · Wing, Plate/SkinSDR 06FDEA0958Rib · crackedWITH REFERENCE TO FEDEX EA 1-5510-94597, LEFT HAND HORIZONTAL STABILIZER FORWARD UPPER RIB CAP AT STA XE = 51.00 FOUND CRACKED. COMPLIED WITH FEDEX EA 1-5510-94611.Mar 6, 2006 · N585FE · Doug MD11 · Horizontal Stabilizer StructureSDR 06FDEA0935Hinge Bracket · corrodedINSTRUCTED TO REMOVE AND REPLACE INBOARD TRAILING EDGE FLAP OUTBOARD HINGE BRACKET WITH P/N: ARC2512-501 BUT ITEM CAME WITH P/N: ARC2512-1. REVISION B REVISES FEDEX EA 1-5750-79754A P2 BY DELETING REMOVAL AND REPLACEMENT REQUIREMENT, SCHEDULING PART II AND PAMar 5, 2006 · N585FE · Doug MD11 · Trailing Edge FlapsSDR 06FDEA0874Skin · crackedLEFT HAND WING, NR 3 SLAT TELESCOPIC ANTI-ICE LEADING EDGE SPRING DOOR CUTOUT AREA UPPER CORNER CRACKED. COMPLIED WITH FEDEX EA 1-5740-94607. REPAIR CLASSIFIED AS MINOR PER FEDEX GMM 6-2-100.Feb 28, 2006 · N585FE · Doug MD11 · Leading Edge DevicesSDR 06FDEA0807Fitting · crackedEMPENNAGE, FORWARD UPPER DOG HOUSE ENTRANCE, CUT OUT EDGE FOUND CRACKED CORRECTIVE ACTION: SNRM NO.: N00958 - EMPENNAGE, FORWARD UPPER DOG HOUSE ENTRANCE, CUT OUT EDGE CRACKED AREA REPAIRED AS PER SRM 53-00-01 VOLUME I, FIGURE 5. REPAIR CLASSIFIED AS Feb 22, 2006 · N585FE · Doug MD11 · Empennage Flight Control Surfaces, Attach FittingsSDR 06FDEA0802Hinge Fitting · crackedRT WING, OB FLAP IB HINGE FITTING AT MOST OB LOWER BOLT HOLE FOUND WITH CRACK INDICATION. REPLACED AS PER AMM 27-50-30-4. OTBD FLAP ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-00-5 FOUND SATISFACTORY.Feb 21, 2006 · N585FE · Doug MD11 · Trailing Edge FlapsSDR 06FDEA0801Door · crackedRT WING, NR 3 SLAT TELESCOPIC ANTI-ICE LEADING EDGE SPRING DOOR CUTOUT AREA UPPER CORNER WITH APPROXIMATELY ONE (1) INCH CRACKED. COMPLIED WITH FEDEX EA 1-5740-94606.Feb 21, 2006 · N585FE · Doug MD11 · Leading Edge DevicesSDR 06FDEA0774Hinge · crackedLEFT HAND WING, OUTBOARD FLAP INBOARD HINGE AT MOST OUTBOARD LOWER BOLT HOLE FOUND WITH CRACK INDICATION. COMPLIED WITH FEDEX EA 1-5750-94604.Feb 20, 2006 · N585FE · Doug MD11 · Trailing Edge FlapsSDR 06FDEA0773Seat Track · crackedFORWARD CARGO COMPARTMENT CEILING AREA, MAIN DECK SEAT TRACK STA 635, X = 8, FOUND CRACKED. REPAIRED AS PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Feb 20, 2006 · N585FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA0772Seat Track · crackedFORWARD CARGO COMPARTMENT CEILING AREA, MAIN DECK SEAT TRACK STA 635, X = -8 FOUND CRACKED. REPAIRED AS PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Feb 20, 2006 · N585FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA0771Seat Track · crackedFORWARD CARGO COMPARTMENT CEILING AREA, MAIN DECK SEAT TRACK STA 635, X = 27 FOUND CRACKED. REPAIRED AS PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Feb 20, 2006 · N585FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA0708Bracket · crackedLEFT HAND WING, LEADING EDGE RIB BRACKET LOWER AREA, STA XORS 538, OUTBOARD SIDE OF REFUEL ACCESS 519CB CUTOUT AREA FOUND CRACKED ARB1187-15. REMOVED AND REPLACED AS PER SRM 51-31- 01 VOLUME II. NEW FORMER FABRICATED AS PER DWG ARB2917. REPAIR CLASSIFIEDFeb 17, 2006 · N585FE · Doug MD11 · Wing Miscellaneous StructureSDR 06FDEA0705Skin · unknownLEFT HAND HORIZONTAL STABILIZER, BARREL NUT AFT SKIN PLANK REPLACEMENT - TO COMPLY WITH FEDEX EA 1-5510-94597, SR11550010-77 STRINGER PANEL ASSY. COMPLIED WITH FEDEX EA 1-5510-94597.Feb 16, 2006 · N585FE · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR 06FDEA0704Skin · unknownRIGHT HAND HORIZONTAL STABILIZER, BARREL NUT AFT SKIN PLANK REPLACEMENT - TO COMPLY WITH FEDEX EA 1-5510-94598 SR11550010-78 STRINGER PANEL ASSY. COMPLIED WITH FEDEX EA 1-5510-94598.Feb 16, 2006 · N585FE · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR 06FDEA0670Stringer · crackedLEFT WING TANK, APPROXIMATELY 2.5 INCHES LONG CRACK FOUND ON OUTBOARD END OF STRINGER 43 DURING HFEC INSPECTION. REPAIRED AS PER SRM 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 06FDEA0669Stringer · crackedFOUND LEFT WING TANK, APPROXIMATELY ONE (1) INCH LONG CRACK FOUND ON OUTBOARD END OF STRINGER 16 DURING HFEC INSPECTION. REPAIRED AS PER SRM 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 06FDEA0668Stringer · crackedLEFT WING TANK, APPROXIMATELY 10.5 INCHES LONG CRACK FOUND ON OUTBOARD END OF STRINGER 12 DURING HFEC INSPECTION. REPAIRED AS PER SRM 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 06FDEA0667Stringer · crackedRIGHT WING TANK, APPROXIMATELY ONE (1) INCH LONG CRACK FOUND ON OUTBOARD END OF STRINGER 44 DURING HFEC INSPECTION. REPAIRED AS PER SRM 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 06FDEA0666Stringer · crackedRIGHT WING TANK, APPROXIMATELY ONE (1) INCH LONG CRACK FOUND ON OUTBOARD END OF STRINGER 43 DURING HFEC INSPECTION. REPAIRED AS PER SRM 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 06FDEA0665Stringer · crackedRIGHT WING TANK, APPROXIMATELY ONE (1) INCH LONG CRACK FOUND ON OUTBOARD END OF STRINGER 42 DURING HFEC INSPECTION. REPAIRED AS PER SRM 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 06FDEA0664Stringer · crackedRIGHT WING TANK, APPROXIMATELY TEN (10) INCHES LONG CRACK FOUND ON OUTBOARD END OF STRINGER 12 DURING HFEC INSPECTION. REPAIRED AS PER SRM 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 06FDEA0663Stringer · crackedRIGHT WING TANK, APPROXIMATELY NINE (9) INCHES LONG CRACK FOUND ON OUTBOARD END OF STRINGER 13 DURING HFEC INSPECTION. REPAIRED AS PER SRM 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 06FDEA0662Seat Track · crackedFOUND UPPER CARGO COMPARTMENT, SEAT TRACK AT STA 775, X = 47 CRACKED. REPAIR CARRIED OUT BETWEEN STA 725 TO STA 755, X = 47 AS PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Feb 13, 2006 · N585FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA0661Stringer · crackedRIGHT WING TANK, APPROXIMATELY TEN (10) INCHES LONG CRACK FOUND ON OUTBOARD END OF STRINGER 10 DURING HFEC INSPECTION. REPAIRED AS PER SRM 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 06FDEA0660Stringer · crackedLT WING TANK, APPROXIMATELY 10.5 INCHES LONG CRACK FOUND ON OUTBOARD END OF STRINGER 9 DURING HFEC INSPECTION. REPAIRED AS PER SRM 57-20-00 VOLUME I, FIGURE 20. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Feb 13, 2006 · N585FE · Doug MD11F · Wing, Longeron/StringerSDR 06FDEA0659Stringer · crackedLEFT WING TANK, APPROXIMATELY NINE (9) INCH LONG CRACK FOUND ON OUTBOARD END OF STRINGER 11 DURING HFEC INSPECTION. REPAIRED AS PER SRM 57-20-00 VOLUME I, FIGURE 1A. CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100.Feb 13, 2006 · N585FE · Doug MD11F · Wing, Longeron/Stringer
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