Boeing MD-11F

Service difficulty reports · 31,317

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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"

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SDR IPXA2020070357257Angle · puncturedINSPECTION TYPE:3C EXTENDED TAILCONE HAS PUNCTURED THROUGH THE RT Z-FRAME. REPAIRED EXTENDED TAILCONE RT Z-FRAME IAW EA 011-5300-1-A8334 REV IR AND EO MD11-5350-77041-A. (MINOR)May 28, 2020 · N262UP · Doug MD11F · Aerodynamic FairingsSDR IPXA2020070157198Support · crackedINSPECTION TYPE:3C CENTER CARGO COMPARTMENT FLOORBEAM SUPPORT RIGHT SIDE AT STA 5-32 BL-16R CRACKED. REMOVED CRACKED FLOOR BEAM SUPPORT, FABRICATED AND INSTALLED IN CENTER CARGO RT SIDE AT STA 5-32 BL-16R IAW SRM 51-35-01.May 28, 2020 · N262UP · Doug MD11F · Fuselage Main, Floor BeamSDR FDEA2020052981070Seat Track · damagedCABIN - SEAT TRACK CROWN AREA DAMAGED AT STATION 5-83, X = 8.5. CABIN - AT SEAT TRACK STATION 5-83 X = 8.5, DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REMOVED AND REPLACED May 28, 2020 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2020052981069Seat Track · corrodedCABIN - SEAT TRACK TOP SURFACE CORROSION AT STATION 5-43, X = 8.5. CABIN - AT SEAT TRACK TOP SURFACE STATION 5-43 X = 8.5, CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REMOVED AND REPLACMay 28, 2020 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2020052981068Seat Track · corrodedMAIN DECK CARGO COMPARTMENT AT STATION 1096 X = 27.5 SEAT TRACK FLANGE FOUND CORROSION. MAIN DECK CARGO COMPARTMENT AT STATION 1096 X = 27.5 SEAT TRACK FLANGE, CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CMay 28, 2020 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2020052981067Seat Track · corrodedMAIN DECK CARGO COMPARTMENT AT STATION 1111 X = 8.5 SEAT TRACK FLANGE FOUND CORROSION. MAIN DECK CARGO COMPARTMENT STATION 1111 X = 8.5 AT SEAT TRACK FLANGE CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRMay 28, 2020 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2020052981072Seat Track · damagedCABIN SEAT TRACK CROWN AREA DAMAGED AT STATION 1289, X = 8.5. SEAT TRACK CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATIOMay 28, 2020 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2020052981071Seat Track · damagedCABIN - SEAT TRACK CROWN AREA DAMAGED AT STATION 5-05, X = -47.5. SEAT TRACK DAMAGE CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1, DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLMay 28, 2020 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2020052981075Floor Panel · delaminatedMAIN CABIN: FLOOR PANEL DELAMINATED AT LBL 90, STATION 779-839. FABRICATED NEW FLOOR PANEL IN MAIN CABIN AT LBL 90, STATION 779-839 IAW DRAWING SRZ25-005.May 28, 2020 · N593FE · Doug MD11F · Fuselage Floor PanelSDR FDEA2020070671062Sensor · failedAPPROX 2:15 INTO FLIGHT AT FL 300, LVL1 BRAKE DIFF TEMP ALERT NR 1 SHOWED 200, NR2 SHOWED 190, ALL OTHER SHOWED ABOUT 65. THEN NR 2 CONTINUE TO CLIMB, REMAINING APPROX 212. AS THE TEMP WAS CLIMBING WE DECLARED EMERG AND DIVERTED TO PVG. NO PROBLEM ON LANDINGMay 27, 2020 · N610FE · Doug MD11F · Landing Gear Brake SystemSDR IPXA2020070357256Longeron Splice · crackedINSPECTION TYPE:3C CENTER CARGO COMP LONGERON 33R SPLICE CRACKED INSIDE CHANNEL AT STA 5-123. REMOVED CRACKED SPLICE, FABRICATED AND INSTALLED IN CENTER CARGO LONGERON 33R AT STA 5-123 IAW SRM 51-33-01. (MINOR)May 27, 2020 · N262UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2020070357255Longeron Splice · crackedINSPECTION TYPE:3C CENTER CARGO COMP LONGERON 28R SPLICE CRACKED INSIDE CHANNEL AT STA 5-123. REMOVED CRACKED SPLICE, FABRICATED AND INSTALLED IN CENTER CARGO ON LONGERON 28R AT STA 5-123 IAW SRM 51-33-01. (MINOR)May 27, 2020 · N262UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2020070257254Longeron Splice · crackedINSPECTION TYPE:3C CENTER CARGO COMP LONGERON 41L SPLICE CRACKED INSIDE CHANNEL AT STA 5-123. REMOVED CRACKED SPLICE, FABRICATED AND INSTALLED IN CENTER CARGO ON LONGERON 41L AT STA 5-123 IAW SRM 51-33-01. (MINOR)May 27, 2020 · N262UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2020070257252Longeron Splice · crackedINSPECTION TYPE:3C CENTER CARGO COMP LONGERON 40R SPLICE CRACKED AT CHANNEL STA 5-123. REMOVED CRACKED SPLICE, FABRICATED AND INSTALLED IN CENTER CARGO LONGERON 40R AT STA 5-123 IAW DRAWING N5A6774. (MINOR)May 27, 2020 · N262UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2020070357251Longeron Splice · crackedINSPECTION TYPE:3C CENTER CARGO COMP LONGERON 43L SPLICE CRACKED INSIDE CHANNEL AT STA 5-123. REMOVED CRACKED SPLICE, FABRICATED AND INSTALLED IN CENTER CARGO LONGERON 43L AT STA 5-123 IAW SRM 51-33-01. (MINOR)May 27, 2020 · N262UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2020070157200Support Strut · brokenINSPECTION TYPE:3C CENTER CARGO COMPARTMENT FLOORBEAM TO FRAME SUPPORT STRUT BROKEN IN HALF AT STA 5-32 LBL-17. REMOVED BROKEN FRAME SUPPORT STRUT, FABRICATED AND INSTALLED IN CENTER CARGO AT STA 5-32 LBL-17 IAW SRM 51-35-01. (MINOR)May 27, 2020 · N262UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2020063057199Floor Support · corrodedINSPECTION TYPE:3C MAIN CARGO FLOOR CENTER LINE AT STA 1381 FLOOR SUPPORT HAS CORROSION. REMOVED CORRODED FLOOR SUPPORT, FABRICATED AND INSTALLED IN MAIN CARGO AT STA 1381 X=0 IAW SRM 51-35-01.May 27, 2020 · N262UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2020062957115Longeron Splice · crackedINSPECTION TYPE:3C, CENTER CARGO COMPARTMENT LONGERON 35R SLPICE CRACKED INSIDE RADUIS AT STA 5-123.REMOVED CRACKED LONGERON SPLICE, FABRICATED AND INSTALLED IN CENTER CARGO AT LONGERON 35R STA 5-123 IAW SRM 51-33-01. (MINOR)May 27, 2020 · N262UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2020061256483Fitting · damagedINSPECTION TYPE:4C RT I/B ELEVATOR NR 2 MOUNT FITTING BOTH BUSHINGS ARE MIGRATED. REPAIRED RT I/B ELEVATOR NR 2 MOUNT FITTING I/B & O/B MIGRATED BUSHINGS IAW EA 011-5510-01-A8310 REV IR AND EO MD11-5520-76797-A. (MINOR)May 27, 2020 · N276UP · Doug MD11F · Elevator Miscellaneous StructureSDR IPXA2020061556482Bushing · migratedINSPECTION TYPE:4C LT O/B ELEVATOR NR 5 MOUNT FITTING I/B BUSHING IS MIGRATED. REPAIRED LT O/B ELEVATOR NR 5 MOUNT FITTING I/B MIGRATED BUSHING IAW EA 011-5510-01-A8311 REV IR AND EO MD11-5520-76758-A. (MINOR)May 27, 2020 · N276UP · Doug MD11F · Elevator Miscellaneous StructureSDR IPXA2020061556525Skin · corrodedINSPECTION TYPE:4C FUSELAGE SKIN IS BULGED JUST FWD OF STA 5-32 AT LONGERON 51L. REPAIRED FUSELAGE SKIN CORROSION BETWEEN STA 5-11 - 5-32 AT LONGERON 51L IAW EA 011-5340-01-A8308 REV IR AND EO MD11-5340-76855-A. (MAJOR)May 27, 2020 · N276UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2020061056367Fitting · wornINSPECTION TYPE:4C RT OB ELEVATOR OB OF NR 8 BEARING CAM FITTING WORN. REPAIRED RT OB ELEVATOR OB OF NR 8 BEARING CAM FITTING IAW EA 011-5520-01-A8302 REV IR AND EO MD11-5520-76695-A. (MINOR)May 27, 2020 · N276UP · Doug MD11F · Elevator Miscellaneous StructureSDR IPXA2020061056366Fitting · wornINSPECTION TYPE:4C RT DETACHABLE ELEVATOR OB CAM FITTING WORN. REPAIRED WORN RT DETACHABLE OB CAM FITTING IAW EA 011-5520-01-A8302 IR AND EO MD11-5520-76695-A. (MINOR)May 27, 2020 · N276UP · Doug MD11F · Elevator Miscellaneous StructureSDR IPXA2020061056365Fitting · wornINSPECTION TYPE:4C LT IB ELEVATOR OB CAM FITTING WORN. REPAIRED LT IB ELEVATOR OB CAM FITTING IAW EA 011-5520-01-A8302 REV IR AND EO MD11-5520-76695-A. (MINOR)May 27, 2020 · N276UP · Doug MD11F · Elevator Miscellaneous StructureSDR IPXA2020061056362Fitting · wornINSPECTION TYPE:4C LT IB ELEVATOR IB CAM FITTING WORN. REPAIRED WORN LT IB ELEVATOR IB CAM FITTING IAW EA 011-5520-01-A8302 REV IR AND EO MD11-5520-76695-A. (MINOR)May 27, 2020 · N276UP · Doug MD11F · Elevator Miscellaneous StructureSDR IPXA2020061056361Fitting · wornINSPECTION TYPE:4C LT OB ELEVATOR CAM FITTING O/B OF NR 8 BEARING IS WORN. REPAIRED WORN LT OB ELEVATOR CAM FITTING O/B OF NR 8 BEARING IAW EA 011-5520-01-A8302 REV IR AND EO MD11-5520-76695-A. (MINOR)May 27, 2020 · N276UP · Doug MD11F · Elevator Miscellaneous StructureSDR IPXA2020061056356Fitting · wornINSPECTION TYPE:4C LT O/B ELEVATOR CAM FITTING I/B OF NR 7 BEARING IS WORN. REPAIRED WORN LT O/B ELEVATOR CAM FITTING I/B OF NR 7 BEARING IAW EA 011-5520-01-A8302 REV IR AND EO MD11-5520-76695-A. (MINOR)May 27, 2020 · N257UP · Doug MD11F · Elevator Miscellaneous StructureSDR FDEA2020061071062Sensor · faultyAPPROX 2:15 INTO FLIGHT AT FL 300, LVL1 BRAKE DIFF TEMP ALERT NR 1 SHOWED 200 NR 2 SHOWED 190, ALL OTHER SHOWED ABOUT 65 THEN NR 2 CONTINUE TO CLIMB, REMAINING APPROX 212. AS THE TEMP WAS CLIMBING WE DECLARED EMERG AND DIVERTED TO PVG. NO PROBLEM ON LANDING. BMay 27, 2020 · N610FE · Doug MD11F · Landing Gear Brake SystemSDR FDEA2020052971061Unknown · malfunctionedON PREFLIGHT INSP CREW REPORTED EMERG LIGHT BATT LO ALERT. RESET POWER FOR EMER BATTERY PACK U1-1756, OPS TESTED EMER LIGHTS NORMAL AS MM 33-51-01-5 REQUIRES. A/C OK TO CONTINUE SERVICE.May 27, 2020 · N631FE · Doug MD11F · Emergency LightingSDR FDEA2020052971064Warning System · false activationDURING PREFLIGHT, CREW REPORTED WHEN TESTING EMERGENCY LIGHTS EIS MESSAGE SHOWED EMERGENCY LIGHTS BATTERY LOW. EMERGENCY LIGHTS OPERATIONS CHECK 'SATIS' IAW AMM 33-52-01-5, PLACARD REMOVED.May 27, 2020 · N595FE · Doug MD11F · Emergency LightingSDR FDEA2020052971062Warning System · activatedAPPROXIMATELY 2:15 INTO FLIGHT AT FL300, LVL1 BRAKE DIFF TEMP ALERT NR 1 SHOWED 200? NR 2 SHOWED 190?, ALL OTHER SHOWED ABOUT 65? THEN NR 2 CONTINUE TO CLIMB. REMAINING APPROX 212?. AS THE TEMP WAS CLIMBING WE DECLARED EMERGENCY AND DIVERTED TO PVG. NO PRMay 27, 2020 · N610FE · Doug MD11F · Landing Gear Brake SystemSDR IPXA2020052955919Actuator · faultyINSPECTION TYPE: N/A DIVERSION NR CPD NR 2 FAULT CFDS PROBABLY CAUSE CPC - 2 MOTOR / OFV. R & R NR 2 OUTFLOW VALVE ACT IAW AMM 21-31-20-000-801. OPS TEST OK 21-31-01-01-036.May 27, 2020 · N284UP · Doug MD11F · Pressure Regulator/Outflow ValveSDR IPXA2020072097943Seat Track · crackedINSPECTION TYPE:3C, MAIN CARGO TRACK CRACKED AT STA 839 X= -75.50. REPAIRED THE CRACKED CARGO TRACK IAW SRM 53-00-52, REPAIR 1, FIG 201, REV.66. MAJOR.May 26, 2020 · N262UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2020072097941Floor Support · crackedINSPECTION TYPE:3C, MAIN CARGO FLOOR SUPPORT AT BS 775 RBL-80 IS CRACKED. REMOVED CRACKED FLOOR SUPPORT, FABRICATED AND INSTALLED IN MAIN CARGO IAW DWG ACA3763.May 26, 2020 · N262UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2020061556599Spar Cap · corrodedINSPECTION TYPE:2C LT WING REAR SPAR UPPER CAP HAS CORROSION BETWEEN STA XORS= 784.5 & 826.5. REPAIRED CORRODED LT WING REAR UPPER CAP BETWEEN STA XORS= 784.5 & 826.5 IAW EA 011-5710-01-A8317 REV. I/R AND EO MD11-5710-76848-A. (MINOR)May 26, 2020 · N276UP · Doug MD11F · Wing SparSDR FDEA202005261044Trunnion · crackedNOSE LANDING GEAR LEFT HAND TRUNNION FITTING SUSPECTED CRACKED AT STATION Y = 595 CRACKED NOSE LANDING GEAR LEFT HAND TRUNNION FITTING AT STATION Y = 595 REPAIRED AS PER SRM 53-10-14-2R FIGURE 202 REPAIR 2. INITIAL INSPECTION TO BE CARRIED OUT AT 1500 FLIGHT CMay 26, 2020 · N620FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR IPXA2020072097946Tee Fitting · chafedINSPECTION TYPE:3C, RIGHT WING FIXED L/E LWR T CHORD AND UPPER ANGLE ARE CHAFED FROM THE TELESCOPIC DUCT PANEL ON I/B SIDE.REMOVED CHAFED T-CHORD, FABRICATED AND INSTALLED ON RH WING FIXED L/E XOS-464 IAW DWG ARB2926.May 25, 2020 · N262UP · Doug MD11F · Wing Main, Frame StructureSDR IPXA2020072097945Cap · chafedINSPECTION TYPE:3C, RT WING FIXED L/E LOWER T-CHORD AND UPPER ANGLE CHAFED FROM TELESCOPIC DUCT PANEL ON I/B SIDE.REMOVED CHAFED T-CAP, FABRICATED AND INSTALLED ON RH WING FIXED L/E XOS=464 IAW DWG 1284.May 25, 2020 · N262UP · Doug MD11F · Wing Main, Frame StructureSDR IPXA2020072097944Splice Angle · chafedINSPECTION TYPE:3C, RT WING FIXED L/E LWR T CHORD AND UPPER ANGLE CHAFED FROM THE TELESCOPIC DUCT PANEL ON I/B SIDE. REMOVED CHAFED SPLICE ANGLE, FABRICATED AND INSTALLED ON THE RT WING FIXED L/E XOS=464 IAW DWG 1284.May 25, 2020 · N262UP · Doug MD11F · Wing Main, Frame StructureSDR IPXA2020070757466Support Angle · crackedINSPECTION TYPE:3C, RH WING L/E PANEL SUPPORT ANGLE ATTACHED TO RIB AT XORS 995 IS CRACKED.REMOVED CRACKED ANGLE, FABRICATED AND INSTALLED ON RH WING L/E RIB AT STA XORS 995 IAW DWG ARB2920. (MINOR)May 25, 2020 · N262UP · Doug MD11F · Wing Miscellaneous StructureSDR IPXA2020062957118Rib · crackedINSPECTION TYPE:3CRH WING FIXED L/E RIB IS CRACKED ON T/E AT STA XORS 471.REMOVED CRACKED RIB, FABRICATED AND INSTALLED ON RH WING FIXED L/E AT STA XORS 471 IAW SRM 51-35-01. (MINOR)May 25, 2020 · N262UP · Doug MD11F · Wing, Rib/BulkheadSDR IPXA2020062256762Doubler · crackedINSPECTION TYPE:3C RT WING FIXED L/E BEADED DOUBLER IS CRACKED AT STA XOS 659. REPAIRED CRACKED RT WING FIXED L/E BEADED DOUBLER AT STA XOS 659 IAW SRM 57-40-02 REPAIR 15 FIG 205. (MAJOR)May 25, 2020 · N262UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2020061456571Support Angle · crackedINSPECTION TYPE:3C WTB SUPPORT ANGLE IS CRACKED AT THE TOP, IN THE RADUIS AT STA 1581 BETWEEN L30L AND L31L. FABRICATED AND REPLACED CRACKED ANGLE AT STA 1581 BETWEEN STA L30L AND L31L IAW SRM 51-33-01 AND SRM 51-35-01. (MINOR)May 25, 2020 · N262UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA202008058653Seat Track · corrodedINSPECTION TYPE:C3, MAIN CABIN FLOOR, BS 1130 TO 1530, X-107 SEAT TRACK HAD CORROSION IN SEVERAL AREAS. REMOVED AND REPLACED THE SEAT TRACK BETWEEN BS 1276 AND 1410 IAW SRM 53-00-52, REPAIR 1, FIG 201, AND ACA7414. MAJOR REPAIR.May 24, 2020 · N262UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2020062436898Web · crackedINSPECTION TYPE:3C, UPPER CARGO COMPARTMENT L-3 DOOR FWD JAMB TORQUE BOX WEB IS CRACKED BETWEEN STA 1250 - 1256REPAIRED CRACKED L3 DOOR FWD JAMB TORQUE BOX WEB BETWEEN STA 1250-1256 IAW SRM 53-40-15 REPAIR 3 FIG 201 REV 66. (MAJOR)May 24, 2020 · N262UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2020062256860Torque Box · crackedINSPECTION TYPE:3C UPPER CARGO COMPARTMENTL3 DOOR AFT JAMB TORQUE BOX HAS 2EA CRACKES AROUND WEB LIGHTNING HOLE. REPAIRED CRACKED L3 DOOR AFT JAMB TORQUE BOX WEB AROUND LIGHTNING HOLE BETWEEN STA 1305.25 AND 1315.42 IAW SRM 53-40-15 REPAIR 3 FIG 201 REV 66. (May 24, 2020 · N262UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2020061556621Beam · crackedINSPECTION TYPE:2C RT O/B FLAP I/B HINGE AFT BEAM IS CRACKED. REMOVED, FABRICATED AND REPLACED BEAM IAW DWG ARC 2419 AND SRM 51-31-01. (MINOR)May 24, 2020 · N276UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2020061556618Skin · delaminatedINSPECTION TYPE:2C RT O/B AILERON UPPER SURFACE I/B T/E IS DELAMINATED. REMOVED AND REPLACED RT O/B AILERON IAW EO MD11-2700-74700-C. (MINOR)May 24, 2020 · N276UP · Doug MD11F · AileronsSDR IPXA2020061556598Panel · corrodedINSPECTION TYPE:2C RT WING REAR SPAR SPOILER PANEL IS CORRODED BETWEEN STA XOFH= 453.931 TO XOSP= 498.20. REPAIRED CORRODED RT WING REAR SPAR SPOILER PANEL SILL BETWEEN STA XOFH= 453.931 TO XOSP= 498.20 IAW SRM 57-50-02 REPAIR 10 FIG 201. (MINOR)May 24, 2020 · N276UP · Doug MD11F · SpoilersSDR IPXA2020061556515Filler · corrodedINSPECTION TYPE:4C RT WING UPPER SURFACE FWD OF I/B AILERON HAS CORROSION. REPAIRED RT WING UPPER T/E SPACER FILLER CORROSION BETWEEN STA XORS 408 - XORS 420 IAW EA 011-5700-01-A8331 REV IR AND EO MD11-5710-76851-A. (MINOR)May 24, 2020 · N276UP · Doug MD11F · Wing, Plate/Skin
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