Boeing MD-11F

Service difficulty reports · 31,317

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 = 'MD11F'
  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 FDEA2020082751890Support · corrodedRT WING, OUTBOARD FLAP VANE NR 1 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT RT WING, OUTBOARD FLAP VANE NR 1 SUPPORT FITTING. ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND EXCEEDS LIMIT AS PER MD-11 SRM 57-50-02-2R FIGURE 201 REPAug 15, 2020 · N625FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2020082751889Support · corrodedRT WING, OUTBOARD FLAP VANE NR 2 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT RT WING, OUTBOARD FLAP VANE NR 2 SUPPORT FITTING. ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND EXCEEDS LIMIT AS PER MD-11 SRM 57-50-02-2R FIGURE 201 REPAug 15, 2020 · N625FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2020082651891Support Fitting · corrodedRIGHT HAND WING - OUTBOARD FLAP VANE NUMBER 3 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION CORROSION AT RIGHT HAND WING - OUTBOARD FLAP VANE NUMBER 3 SUPPORT FITTING ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND WITHIN LIMIT AS PER MD-11 SRMAug 15, 2020 · N625FE · Doug MD11F · Trailing Edge FlapsSDR IPXA2020082659520Rib · corrodedINSPECTION TYPE:2CRT O/B ELEVATOR L/E RIB AT STA. XE=215.120 HAS CORROSION.REMOVED AND REPLACED CORRODED RT O/B ELEVATOR L/E RIB AT STA. XE=215.120 IAW MD-11 SRM 51-33-01. (MINOR)Aug 15, 2020 · N285UP · Doug MD11F · Elevator, Spar/RibSDR FDEA2020081851893Vane · corrodedLEFT HAND WING - OUTBOARD FLAP VANE NUMBER 4 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSIONAug 15, 2020 · N625FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2020081851892Vane · corrodedLEFT HAND WING - OUTBOARD FLAP VANE NUMBER 2 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSIONAug 15, 2020 · N625FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2020081851891Vane · corrodedRIGHT HAND WING - OUTBOARD FLAP VANE NUMBER 3 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSIONAug 15, 2020 · N625FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2020081851890Vane · corrodedRIGHT HAND WING - OUTBOARD FLAP VANE NUMBER 1 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSIONAug 15, 2020 · N625FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2020081851889Vane · corrodedRIGHT HAND WING - OUTBOARD FLAP VANE NUMBER 2 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSIONAug 15, 2020 · N625FE · Doug MD11F · Trailing Edge FlapsSDR FDEA202008141886Hinge Fitting · corrodedRIGHT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE HOLE BORE FOUND CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52-03 AND E.A. Aug 14, 2020 · N625FE · Doug MD11F · Trailing Edge FlapsSDR FDEA202008141885Hinge Fitting · corrodedLEFT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSION. REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-52-03. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52-03 AND E.A. # 1-5750Aug 14, 2020 · N625FE · Doug MD11F · Trailing Edge FlapsSDR FDEA202008141884Hinge Fitting · corrodedLEFT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION. REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-52-03. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52-03 AND E.A. # 1-5750-Aug 14, 2020 · N625FE · Doug MD11F · Trailing Edge FlapsSDR FDEA202008141883Hinge Fitting · corrodedRIGHT HAND WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT HAND WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHAug 14, 2020 · N625FE · Doug MD11F · Trailing Edge FlapsSDR FDEA202008141882Hinge Fitting · corrodedLEFT HAND WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT HAND WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHINAug 14, 2020 · N625FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2020082631873Floor Panel · delaminatedMAIN DECK CARGO COMPARTMENT , CENTER FLOOR PANEL #283BF FOUND DELAMINATED AT ZONE 280 STATION 1561 - 1641 . DELAMINATED MAIN DECK CARGO COMPARTMENT CENTER FLOOR PANEL #283BF AT ZONE 280 STATION 1561 TO STATION 1641 REMOVED AS PER AMM 53-21-01-4 . FLOOR PANEAug 13, 2020 · N625FE · Doug MD11F · Fuselage Floor PanelSDR IPXA2020082429358Fitting · wornINSPECTION TYPE:2C, RIGHT OTBD ELEVATOR CAM FITTING IS WORN AT THE #6 RIB. REPAIRED CAM FITTING IAW EA 011-5520-01-A8472 REV. I/R, AND EO MD11-5520-77483-A. (MINOR)Aug 13, 2020 · N285UP · Doug MD11F · Elevator StructureSDR FDEA2020081431873Floor Panel · damagedMAIN DECK CARGO COMPARTMENT CENTER FLOOR PANEL 283BF FOUND DAMAGED AT ZONE 280 STA 1561-STA 1641.Aug 13, 2020 · N625FE · Doug MD11F · Fuselage Floor PanelSDR FDEA202008121866Longeron Splice · corrodedFORWARD CARGO - BILGE AREA STATION 6-0 LONGERON SPLICE FOUND CORROSION . CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 205 ALLOWABLE DAMAGE . CORRODED LONGERON SPLICE AT STATION 6-0 LONGERON 51 RIGHT REMOVED AND REPLACED AS PER Aug 12, 2020 · N625FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2020082859569Intercostal · crackedINSPECTION TYPE:2C LOWER VERTICAL STABILIZER REAR CENTER SPAR TO REAR SPAR INTERCOSTAL RT SIDE IS CRACKED. REPAIRED CRACKED LOWER VERTICAL STABILIZER REAR CENTER SPAR TO REAR SPAR INTERCOSTAL RT SIDE IAW EA 011-5530-01-A8485 REV. I/R AND EO MD11-5530-77665-AAug 11, 2020 · N285UP · Doug MD11F · Vertical StabilizerSDR FDEA202008111861Bracket · corrodedRIGHT HAND WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT HAND WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MDAug 11, 2020 · N625FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2020082611860Bracket · corrodedRIGHT HAND WING - WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT HAND WING - WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-1Aug 11, 2020 · N625FE · Doug MD11F · Wing, Control SurfacesSDR FDEA2020082611859Bracket · corrodedRIGHT HAND WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION CORROSION AT RIGHT HAND WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD- Aug 11, 2020 · N625FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2020081211861Structure · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSIONAug 11, 2020 · N625FE · Doug MD11F · Wing Main, Frame StructureSDR FDEA2020081211860Structure · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORRODED.Aug 11, 2020 · N625FE · Doug MD11F · Wing Main, Frame StructureSDR FDEA2020081211859Structure · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORRODED.Aug 11, 2020 · N625FE · Doug MD11F · Wing Main, Frame StructureSDR IPXA2020081158916Seat Track · crackedSEAT TRACK CRACKED AT BS 1046, LBL 8.5. REPAIRED IAW EO MD11-5310-77459-A.Aug 11, 2020 · N254UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202008101854Bracket · corrodedLEFTT HAND WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE CORROSION. CORROSION AT LEFTT HAND WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD- 1Aug 10, 2020 · N625FE · Doug MD11F · Wing Main, Frame StructureSDR FDEA202008101853Bracket · corrodedRIGHT HAND WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE CORROSION CORROSION AT RIGHT HAND WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD- 11Aug 10, 2020 · N625FE · Doug MD11F · Wing Main, Frame StructureSDR FDEA202008101852Bracket · corrodedRIGHT HAND WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE BORE FOUND CORROSION. CORROSION AT RIGHT HAND WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MDAug 10, 2020 · N625FE · Doug MD11F · Wing Main, Frame StructureSDR FDEA202008101851Bracket · corrodedRIGHT HAND WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT HAND WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSIZEAug 10, 2020 · N625FE · Doug MD11F · Wing Main, Frame StructureSDR FDEA202008101850Bracket · corrodedLEFT HAND WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT HAND WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE(#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MDAug 10, 2020 · N625FE · Doug MD11F · Wing Main, Frame StructureSDR FDEA202008101849Bracket · corrodedLEFT HAND WING - WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT HAND WING - WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE(#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-1Aug 10, 2020 · N625FE · Doug MD11F · Wing Main, Frame StructureSDR FDEA202008101848Bracket · corrodedLEFT HAND WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION. CORROSION AT LEFT HAND WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE(#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD- 1Aug 10, 2020 · N625FE · Doug MD11F · Leading Edge DevicesSDR FDEA202008101847Bracket · corrodedLEFT HAND WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE FOUND CORROSION. CORROSION AT LEFT HAND WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE(#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 Aug 10, 2020 · N625FE · Doug MD11F · Leading Edge DevicesSDR FDEA202008101846Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE CORRODED. CORROSION AT LEFT HAND WING - WING SIDE OUTBOARD FLAP INBOARD HINGEPIVOT HOLE BORE(#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED BUSHING FABRICATEAug 10, 2020 · N625FE · Doug MD11F · Leading Edge DevicesSDR FDEA202008101845Seat Track · damagedMAIN DECK CARGO, SEAT TRACK CROWN AREA DAMAGED AT STATION 5-10 , X = - 47.5. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 10, 2020 · N625FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2020082879553Aileron · damagedINSPECTION TYPE:2C RT WING I/B AILERON ACTUATOR MOUNT FITTING O/B BUSHING IS MIGRATED. REPAIRED RT WING I/B AILERON ACTUATOR MOUNT FITTING O/B MIGRATED BUSHING IAW VT-SAA EA 011-5750-01-A8493 REV. IR AND UPS EO MD11-5750-77629-A(MINOR).Aug 9, 2020 · N285UP · Doug MD11F · AileronsSDR IPXA2020082879552Bushing · migratedINSPECTION TYPE:2C RT WING I/B AILERON ACTUATOR MOUNT FITTING I/B BUSHING IS MIGRATED.REPAIRED RT WING I/B AILERON ACTUATOR MOUNT FITTING I/B MIGRATED BUSHING IAW VT-SAA EA 011-5750-01-A8493 REV. IR AND UPS EO MD11-5750-77629-A (MINOR).Aug 9, 2020 · N285UP · Doug MD11F · Wing, Control SurfacesSDR FDEA2020082091843Seat Track · damagedMAIN DECK CARGO, FOUND THE SEAT TRACK AT BS 1521 , RBL 75.25 HAD CROWN DAMAGE. THE SEAT TRACK CROWN WAS EVALUATED AND FOUND TO EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT FROM BSAug 9, 2020 · N625FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2020082091842Seat Track · damagedMAIN DECK CARGO, FOUND THE SEAT TRACK AT BS 5-10 , LBL 47.5 WITH CROWN DAMAGE. THE SEAT TRACK CROWN WAS EVALUATED AND FOUND TO EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT BS 5-43 TAug 9, 2020 · N625FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2020082091841Seat Track · damagedMAIN DECK CARGO COMPARTMENT , FOUND THE SEAT TRACK AT BS 1541 , RBL 47.5 HAD CROWN DAMAGE. THE SEAT TRCK CROWN WAS EVALUATED AND FOUND TO EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEAug 9, 2020 · N625FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2020082091840Seat Track · damagedMAIN DECK CARGO, FOUND THE SEAT TRACK AT BS 1700 , LBL 47.5 HAD CROWN DAMAGED . CROWN EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPLACEED FROM BS 1711 TO 1651 IAW SRM 53-00-52-2R, FIGURE 20Aug 9, 2020 · N625FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2020082691839Seat Track · wornCABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK CROWN WORN AT STATION 585 , X = - 8.5 . CABIN - MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 585 , X = - 8.5 , WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE Aug 9, 2020 · N625FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2020082691838Seat Track · wornCABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK CROWN WORN AT STATION 535 , X = - 8.5 . CABIN - MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 535, X = - 8.5 , WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAug 9, 2020 · N625FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2020082691837Skin · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT INSPECTION AT LEFT HAND WING FIXED LEADING EDGE CORNER 11 OF FUEL ACCESS DOOR , FORWARD INBOARD CORNER APPROXIMATELY 1/4 INCHES LENGTH AT XOS 610 . AT LEFT HAND WING FIXED LEADING EDGE CORNER 11 OFAug 9, 2020 · N625FE · Doug MD11F · Wing, Plate/SkinSDR IPXA2020082429350Fitting · wornINSPECTION TYPE:2C, LEFT OTBD ELEVATOR CAM FITTING IS WORN JUST O/B OF THE #7 BEARING.REPAIRED CAM FITTING IAW EA 011-5520-01-A8472 REV. I/R, AND EO MD11-5520-77483-A. (MINOR)Aug 9, 2020 · N285UP · Doug MD11F · Elevator StructureSDR IPXA2020082429349Fitting · wornINSPECTION TYPE:2C, LEFT OTBD ELEVATOR CAM FITTING IS WORN JUST I/B OF THE #9 BEARING.REPAIRED CAM FITTING IAW EA 011-5520-01-A8472 REV. I/R AND EO MD11-5520-77483-A. (MINOR)Aug 9, 2020 · N285UP · Doug MD11F · Elevator StructureSDR IPXA2020082429348Fitting · wornINSPECTION TYPE:2C, LEFT INBD ELEVATOR O/B CAM FITTING IS WORN.REPAIRED CAM FITTING IAW EA 011-5520-01-A8472 REV. I/R AND EO MD11-5520-77483-A. (MINOR)Aug 9, 2020 · N285UP · Doug MD11F · Elevator StructureSDR FDEA2020081891839Seat Track · damagedCABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK CROWN AREA DAMAGED AT STATION 585 , X = - 8.5 . CABIN - MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 585 , X = - 8.5 , DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 Aug 9, 2020 · N625FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2020081891838Seat Track · damagedCABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK CROWN AREA DAMAGED AT STATION 535 , X = - 8.5 . CABIN - MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 535, X = - 8.5 , DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 Aug 9, 2020 · N625FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
Back to Boeing MD-11F