Mcdonnell Douglas MD-11

Service difficulty reports · 7,956

Newest first. General aviation reporting is voluntary.

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 aircraft_model_key = 'MD11'
  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 07FDEA00723Stringer · crackedLT WING TANK - APPROX NINE (9) INCHES LENGTH CRACK FOUND AT STRINGER END 11L (XORS 704) DURING HFEC INSPECTION STRINGER END 11L (XORS 704)AT LT WING TANK REPAIR CARRIED OUT AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2Mar 8, 2007 · N597FE · Doug MD11 · Wing, Longeron/StringerSDR 07FDEA00722Stringer · crackedLEFT WING TANK, APPROX 1/2 INCH LENGTH CRACK FOUND AT STRINGER END 40L (XORS 747), DURING HFEC INSPECTION. (SUPPLEMENTAL 28 MARCH 07) STRINGER END 40L (XORS 747) ON LHW TANK REPAIR CARRIED OUT AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR Mar 8, 2007 · N597FE · Doug MD11 · Wing, Longeron/StringerSDR 07FDEA00696Seat Track · corrodedCABIN STA 1521 TO STA 5-93, X = -8.5 SEAT TRACK FOUND CORRODED. CORRODED SEAT TRACK AT STA 1521 TO STA 5-93, X = -8.5 REPAIRED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Mar 8, 2007 · N609FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA00695Seat Track · corrodedCABIN STA 1481 TO STA 5-33, X = -47.5 SEAT TRACK FOUND CORRODED. (SUPPLEMENTAL 23 MARCH 07) CORRODED SEAT TRACK AT STA 1481 TO STA 5-33, X = -47.5 REPAIRED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Mar 8, 2007 · N609FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA00639Stringer · crackedCRACK FOUND AT STRINGER END 9R (XORS 819), APPROX 13" LENGTH ON RIGHT WING TANK DURING HFEC INSPECTION. (SUPPLEMENTAL 23 MARCH 07) CRACK AT STRINGER END 9R (XORS 819) ON RIGHT HAND WING TANK TRIMMED OUT AND REPAIRED WITH SPLICES AS PER SRM 57-20-00 FIGURMar 4, 2007 · N609FE · Doug MD11 · Wing, Longeron/StringerSDR 07FDEA00638Stringer · crackedCRACK FOUND AT STRINGER END 10R (XORS 760), APPROX. 13" LENGTH ON RIGHT WING TANK, DURING HFEC INSPECTION. (SUPPLEMENTAL 23 MARCH 07) CRACK AT STRINGER END 10R (XORS 760) ON RIGHT HAND WING TANK SLOTTED OUT AND ANGLE REPAIR CARRIED OUT AS PER SRM 57-20-00 FMar 4, 2007 · N609FE · Doug MD11 · Wing, Longeron/StringerSDR 07FDEA00637Stringer · crackedCRACK FOUND AT STRINGER END 11R (XORS 704), APPROX 12.5" LENGTH ON RIGHT WING TANK, DURING HFEC INSPECTION. CRACK AT STRINGER END 11R (XORS 704) ON RIGHT HAND WING TANK TRIMMED OUT AND REPAIRED WITH SPLICES AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASMar 3, 2007 · N609FE · Doug MD11 · Wing, Longeron/StringerSDR 07FDEA00636Stringer · crackedCRACK FOUND AT STRINGER END 44L (XORS 523), APPROX 1" LENGTH ON LEFT WING TANK DURING HFEC INSPECTION. (SUPPLEMENTAL 23 MARCH 07) CRACK AT STRINGER END 44L (XORS 523) ON LEFT HAND WING TANK SLOTTED OUT AND REPAIRED WITH NEW REPAIR SPLICE AS PER SRM 57-Mar 3, 2007 · N609FE · Doug MD11 · Wing, Longeron/StringerSDR 07FDEA00635Stringer · crackedCRACK FOUND AT STRINGER END 14L (XORS 521), APPROX 13" LENGTH ON LEFT WING TANK DURING HFEC INSPECTION. CRACK AT STRINGER END 14L (XORS 521) ON LEFT HAND WING TANK TRIMMED OUT AND REPAIRED WITH SPLICE REPAIR AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASMar 3, 2007 · N609FE · Doug MD11 · Wing, Longeron/StringerSDR 07FDEA00634Stringer · crackedCRACK FOUND AT STRINGER END 42L (XORS 629), APPROX 1" LENGTH ON LEFT WING TANK DURING HFEC INSPECTION. (SUPPLEMENTAL 23 MARCH 07) CRACK AT STRINGER END 42L (XORS 629) ON LEFT HAND WING TANK SLOTTED OUT AND REPAIRED WITH NEW REPAIR SPLICE AS PER SRM 57-20Mar 3, 2007 · N609FE · Doug MD11 · Wing, Longeron/StringerSDR 07FDEA00633Stringer · crackedCRACK FOUND AT STRINGER END 9L (XORS 819), APPROX 10" LENGTH ON LEFT WING TANK DURING HFEC INSPECTION. SUPPLEMENTAL 21 MARCH 07, CRACK ON STRINGER END 9L (XORS 819) SLOTTED OUT AND REPAIRED WITH ANGLES AS PER SRM 57-20 -00 FIGURE 10 VOLUME I. REPAIR CLASSMar 3, 2007 · N609FE · Doug MD11 · Wing, Longeron/StringerSDR 07FDEA00632Duct · crackedRIGHT WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT FOUND CRACKED. (SUPPLEMENTAL 23 MARCH 07) CRACK AT RIGHT HAND WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT REPAIRED AS PER SRM 57 -10-00 FIGURE 42 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Mar 3, 2007 · N609FE · Doug MD11 · Leading Edge DevicesSDR 07FDEA00623Cap · corrodedLT WING, REAR SPAR UPPER CHORD AT STA 1035-1043 FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5710-105616, CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.Mar 1, 2007 · N586FE · Doug MD11 · Wing Main, Frame StructureSDR 07FDEA00622Spar Cap · corrodedFOUND LT WING, REAR SPAR LOWER CHORD AT STA 1063 - 1075 CORROSION. LT WING, REAR SPAR LOWER CHORD AT STA 1063 - 1075 REPAIRED AS PER FEDEX EA NR 1- 5710- 105615, WINGS, LEFT WING LOWER SPAR CAP AFT FLANGE CORROSION BETWEEN XORS=1063 AND XORS=1075 - REPAIR. Mar 1, 2007 · N586FE · Doug MD11 · Wing SparSDR 07FDEA00618Skin · corrodedMAIN DECK CARGO CENTER FUEL TANK UPPER SURFACE FOUND CORROSION AT STA 1218, X=75.25. COMPLIED WITH FEDEX EA 1-5710-105629. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Mar 1, 2007 · N601FE · Doug MD11 · Fuel StorageSDR 07FDEA00617Structure · chafedLT WING I/B FLAP L/E AT O/B HINGE AREA FOUND CHAFED. REPAIR CARRIED OUT AS PER SRM 57-00-01 FIG. 7 VOL.I. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.Mar 1, 2007 · N601FE · Doug MD11 · Trailing Edge FlapsSDR 07FDEA00616Door Frame · corrodedMAIN DECK CARGO DOOR JAMB UNDER CENTERING GUIDE AREA FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5310-106596. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Mar 1, 2007 · N601FE · Doug MD11 · Fuselage Main, StructureSDR 07FDEA00611Relay · burnedELECTRICAL ARCING AT NR 1 EPC BAY LT TOP SIDE RELAY R2-53, R2-57, R2-102 AND R2-252 AFFECTED. REMOVED AND REPLACED 4 RELAYS R2-53, R2-57, R2-102 AND R2-252 AS PER STANDARD WIRING PRACTICES MANUAL. WIRINGS SPLICE REPAIRED AS PER STANDARD WIRING PRACTICES MANFeb 27, 2007 · N586FE · Doug MD11 · Aircraft Fuel Filter/StrainerSDR 07FDEA00610Brake · separatedDURING TIRE CHANGE, FOUND THAT NR 1 BRAKE COMING APART REMOVED AND REPLACE NR 1 BRAKE PER AMM 32-43-01-4. OPS AND LEAK CHECK GOOD.Feb 27, 2007 · N617FE · Doug MD11 · BrakeSDR 07FDEA00555Frame · dentedMAIN DECK CARGO FRAME FOUND DENT AT STA 1641. REPAIR CARRIED OUT AS PER SRM 53-30-00 FIG. 1 VOL.I. REPETITIVE INSPECTION REQUIRED, INITIAL INSPECTION AT 14,500 CYCLES TO BE CARRIED OUT AND THEREAFTER 9500 CYCLES AS PER SRM 53-30-00 FIG.1. VOL.I. REPAIR Feb 26, 2007 · N601FE · Doug MD11 · Fuselage Main, FrameSDR 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 07FDEA00550Seat Track · corrodedMAIN DECK CARGO, FLOOR SEAT TRACK FOUND CORROSION AT STA 1508, X=-8.5. SEAT TRACK REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 1 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Feb 25, 2007 · N601FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA00549Spar Cap · corrodedLT WING REAR SPAR TOP CAP TAPER FILLER AT XORS=480 FOUND UPPER SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5720-106599. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.Feb 25, 2007 · N601FE · Doug MD11 · Wing SparSDR 07FDEA00548Spar Cap · corrodedLT WING REAR SPAR LWR CAP XORS=1050 FOUND UPPER SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5720-106594. CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.Feb 25, 2007 · N601FE · Doug MD11 · Wing SparSDR 07FDEA00547Seat Track · corrodedMAIN DECK CARGO, FLOOR SEAT TRACK FOUND CORROSION AT STA 5-0 TO 5-53, X=-75.25. SEAT TRACK REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 1 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Feb 24, 2007 · N601FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA00546Seat Track · corrodedMAIN DECK CARGO, FLOOR SEAT TRACK FOUND CORROSION AT STA 1521-1528, X=8.5. SEAT TRACK REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 1 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Feb 24, 2007 · N601FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA00544Rib · misalignedDURING REPLACEMENT OF RIB (P/N ARC4125-502) AT RIGHT HAND WING OUTBOARD FLAP FOUND FASTENER HOLE ON NEW FITTING FLANGE RADIUS UNABLE TO INSTALL FASTENER. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II ANDFEDEX E.A. 1-5750-88919 PT4, REPAIR CLASSIFIED AS Feb 22, 2007 · N624FE · Doug MD11 · Wing Main, Frame StructureSDR 07FDEA00543Bracket · corrodedRIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. REPAIRED AS PER FEDEX E.A. 1-5750-107782, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Feb 22, 2007 · N624FE · Doug MD11 · Wing Main, Frame StructureSDR 07FDEA00542Bracket · corrodedRIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK ATTACHMENT BARREL NUT BORE FOUND CORRODED. REPAIRED AS PER FEDEX E.A. 1-5750-107782, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Feb 22, 2007 · N624FE · Doug MD11 · Wing Main, Frame StructureSDR 07FDEA00539Skin · crackedDURING HFEC OPEN, HOLE INSPECTION, QTY: 03 FASTENER HOLES REVEALED CRACK INDICATION FACING FORWARD OF RIGHT WING LOWER SKIN AT ACCESS DOOR AREA (APPROX XORS 696). CARRIED OUT REPAIR AS PER FEDEX E.A. 1-5710-107789, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-10Feb 22, 2007 · N624FE · Doug MD11 · Wing, Plate/SkinSDR 07FDEA00538Unknown · corrodedCENTER CARGO BETWEEN STA 1561 TO STA 1581 STR 48R FOUND CORRODED. REPAIR CARRIED OUT AS PER SRM 53-10- 00 FIG. 2 VOL.I. CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.Feb 22, 2007 · N601FE · Doug MD11 · Fuselage Main, StructureSDR 07FDEA00536Seat Track · corrodedMAIN DECK CARGO, FLOOR SEAT TRACK FOUND CORROSION AT STA 1328, X=75.25. SEAT TRACK REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 1 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Feb 21, 2007 · N601FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA00535Seat Track · corrodedMAIN DECK CARGO, FLOOR SEAT TRACK FOUND CORROSION AT STA 1505, X= 75.25. SEAT TRACK REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 1 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Feb 21, 2007 · N601FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA00534Seat Track · corrodedMAIN DECK CARGO, FLOOR SEAT TRACK FOUND CORROSION AT STA 1521, X=8.5. SEAT TRACK REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 1 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Feb 21, 2007 · N601FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA00533Seat Track · corrodedMAIN DECK CARGO, FLOOR SEAT TRACK FOUND CORROSION AT STA 1495 - 1510, X=-75.25. SEAT TRACK REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 1 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Feb 21, 2007 · N601FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA00532Spar Cap · corrodedRT WING, REAR SPAR CAP FOUND TOP SURFACE AT XORS=1048 CORRODED. COMPLIED WITH FEDEX EA 1-5720-106595. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Feb 21, 2007 · N601FE · Doug MD11 · Wing SparSDR 07FDEA00528Buss · malfunctionedWHILE EXPERIENCING DU4,5 &6 INTERMITTENT BLANKING RECIEVED 'BUS R EMER AC OFF' LVL 1 ALERT,THEN 'IRU 2 ON BAT' LVL 1,FINALLY 'IRU2 FAIL' LVL 2 ALERT.LATER RECEIVED 'SELECT FADEC ALTN' LVL 2 ALERT ON ALL ENGINES,'ATC XPNR 1 & 2 'FAIL ALERTS,ETC. DIVERTED Feb 20, 2007 · N593FE · Doug MD11 · AC InverterSDR 07FDEA00531Structure · crackedRIGHT WING L/E TELESCOPING DUCT PASSAGE CUTOUT FOUND TOP I/B CORNER EDGE CRACKED. REPAIRED AS PER SRM 57-10-00 FIG. 42 VOL.I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Feb 20, 2007 · N601FE · Doug MD11 · Wing Main, Frame StructureSDR 07FDEA00529Angle · crackedFOUND CENTER UNDERWING TANK LT SIDE APPROX STA 1305 TO 1321 SUSPECT CRACK ON CORNER ANGLE SPLICE. COMPLIED WITH FEDEX EA 1-5310-106592. CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.Feb 20, 2007 · N601FE · Doug MD11 · Wing Main, Frame StructureSDR 07FDEA00507Stringer · crackedDURING HFEC INSPECTION, CRACK FOUND AT STRINGER 10 (XORS 760) IN LEFT TANK. REPAIR CARRIED OUT AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Feb 16, 2007 · N601FE · Doug MD11 · Wing, Longeron/StringerSDR 07FDEA00506Stringer · crackedDURING HFEC INSPECTION, CRACK FOUND AT STRINGER 09 (XORS 819) IN LEFT TANK. REPAIR CARRIED OUT PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Feb 16, 2007 · N601FE · Doug MD11 · Wing, Longeron/StringerSDR 07FDEA00505Stringer · crackedDURING HFEC INSPECTION, CRACK FOUND AT STRINGER 40 (XORS 747) IN LEFT TANK. REPAIR CARRIED OUT AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Feb 16, 2007 · N601FE · Doug MD11 · Wing, Longeron/StringerSDR 07FDEA00504Stringer · crackedDURING HFEC INSPECTION, CRACK FOUND AT STRINGER 44 (XORS 523) IN LEFT TANK. COMPLIED WITH FEDEX EA 1-5720-106593. REPAIR CLASSIFIED AS MINOR ALTERATION AS PER FEDEX GMM 6-2-100.Feb 16, 2007 · N601FE · Doug MD11 · Wing, Longeron/StringerSDR 07FDEA00503Stringer · crackedDURING HFEC INSPECTION, CRACK FOUND AT STRINGER 12 (XORS 642) IN LEFT TANK. REPAIR CARRIED OUT AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIED AS MAJOR AS PER FEDEX GMM 6-2-100.Feb 16, 2007 · N601FE · Doug MD11 · Wing, Longeron/StringerSDR 07FDEA00502Stringer · crackedDURING HFEC INSPECTION, CRACK FOUND AT STRINGER 13 (XORS 577) IN LEFT TANK. CARRIED OUT REPAIR AT LT WING STRINGER 13 AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Feb 16, 2007 · N601FE · Doug MD11 · Wing, Longeron/StringerSDR WRLA2007037Stiffener · crackedDURING 3C + 12A CHECK, EGAT MECHANIC FOUND RIGHT WHEEL WELL DOOR OUTBOARD JAMB ASSY STIFFENER CRACK L =.06" AT STA Y = 1474. REF DRAWING ANS7203. REMOVED THE CRACKED STIFFENER AND INSTALLED NEW PARTS PER MD-11 SRM 51-35-01 VOL II REV 38. CONDITION CHECK NORFeb 15, 2007 · N380WA · Doug MD11 · Fuselage Miscellaneous StructureSDR 07FDEA00501Stringer · crackedDURING HFEC INSPECTION, CRACK FOUND AT STRINGER 09 (XORS 819) IN RIGHT TANK. REPAIR CARRIED OUT PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Feb 15, 2007 · N601FE · Doug MD11 · Wing, Longeron/StringerSDR 07FDEA00500Stringer · crackedDURING HFEC INSPECTION, CRACK FOUND AT STRINGER 14 (XORS 521) IN RIGHT TANK. CARRIED OUT REPAIR AT RT WING STRINGER 14R (XORS 521) AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Feb 15, 2007 · N601FE · Doug MD11 · Wing, Longeron/StringerSDR 07FDEA00499Stringer · crackedDURING HFEC INSPECTION, CRACK FOUND AT STRINGER 13 (XORS 577) IN RIGHT TANK. CARRIED OUT REPAIR AT RT WING STRINGER NR 13 (XORS 577) AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Feb 15, 2007 · N601FE · Doug MD11 · Wing, Longeron/StringerSDR 07FDEA00498Stringer · crackedDURING HFEC INSPECTION, CRACK FOUND AT STRINGER 12 (XORS 642) IN RIGHT TANK. CARRIED OUT REPAIR AT RT WING STRINGER NR 12 (XORS 642) AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Feb 15, 2007 · N601FE · Doug MD11 · Wing, Longeron/Stringer
Back to Mcdonnell Douglas MD-11