Boeing MD-11F

Service difficulty reports · 31,320

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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 FDEA201708172249Former · crackedRT WING LEADING EDGE CAVITY AT STA XOS 584 FORMER FOUND CRACKED. CRACKED FORMER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED NEW FORMER AS PER DRAWING ARB 2931 REVISION H. INSTALLED NEW FORMER AT RT WING LEADING EDGE AT STA XOS 584 AS PER SRM 51-33-01-0G. RAug 17, 2017 · N584FE · Doug MD11F · Wing Main, Frame StructureSDR FDEA201708172248Former · crackedRT WING LEADING EDGE CAVITY UPPER FORMER AT STA XOS 584 FOUND CRACKED. CRACKED FORMER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED NEW FORMER AS PER DRAWING ARB 2931 REVISION H. INSTALLED NEW FORMER AT RT WING LEADING EDGE CAVITY UPPER AT STA XOS 584 AS PER Aug 17, 2017 · N584FE · Doug MD11F · Wing Main, Frame StructureSDR IPXA2017081820660Solenoid · inoperativeL1 DOOR INOPERATIVE PRIOR TO DEPARTURE. REMOVED AND REPLACED L1 DOOR LOCK RELEASE SOLENOID IAW AMM 52-10-06.Aug 17, 2017 · N282UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2017081720606Bar · out of positionTHRUST BAR ON PORT CREW ENTRY DOOR AJAR. REINSTALLED THRUST BAR.Aug 16, 2017 · N257UP · Doug MD11F · Passenger/Crew DoorsSDR FDEA201708162235Hinge · corrodedLEFT WING, INBD FLAP, OTBD FWD HINGE (WING SIDE) PIVOT LUG SPOTFACE FOUND CORRODED. THE CORROSION WAS REWORKED AND FOUND WITHIN LIMITS IAW CMM 57-44-07. REPAIRED IAW EA 1-5750-T0331118, B, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 16, 2017 · N590FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201708162233Hinge · corrodedLEFT WING, INBD FLAP OTBD FWD HINGE (WING SIDE) PIVOT BORE FOUND CORROSION. CORROSION REWORKED AND FOUND WITHIN LIMIT IAW CMM 57-44-07. REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0331118 B, PART 1, STEPS F 1 AND F 3. THE REPAIR WAS CLASSIFIEDAug 16, 2017 · N590FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201708152217Frame · crackedMAIN DECK CARGO BAY R3 DOOR FWD LOWER FUSELAGE FRAME WEB FOUND CRACKED AT RT BS 1255, BETWEEN LONGERONS AND 27R. REPAIRED IAW EA 1-5310-T0335060, P1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 15, 2017 · N584FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201708152219Door Frame · crackedMAIN DECK CARGO BAY L3 DOOR AFT LOWER FRAME WEB CRACKED AT BS 1310, BETWEEN LONGERONS 26L AND 27L. REPAIRED IAW SRM 53-40-15-2R, FIGURE 201, REPAIR 3. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 15, 2017 · N584FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201708152218Door Frame · crackedMAIN DECK CARGO BAY L3 DOOR FWD LOWER FRAME WEB CRACKED AT BS 1255, BETWEEN LONGERONS 26L AND 27L. REPAIRED IAW SRM 53-40-15-2R, FIGURE 201, REPAIR 3. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 15, 2017 · N584FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201708152213Doubler · crackedRIGHT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 709 - 714 CRACKED. THE DOUBLER WAS REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 15, 2017 · N584FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201708152211Doubler · crackedRIGHT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 692 - 698 CRACKED. THE DOUBLER WAS REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 15, 2017 · N584FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201708152209Support · crackedLEFT WING LEADING EDGE LOWER ACCESS PANEL SUPPORT FOUND CRACK AT XOS 543. ACCESS PANEL REMOVED IAW SRM 51-31-01-0G. FABRICATED A NEW SUPPORT IAW DRAWING ARB 2933, REVISION AJ. INSTALLED A NEW SUPPORT IAW SRM 51-33-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR Aug 15, 2017 · N584FE · Doug MD11F · Wing Miscellaneous StructureSDR FDEA201708152208Former · crackedLEFT WING LEADING EDGE SKIN INTERNAL FRAME SUPPORT BRACKET FOUND CRACK AT XOS 584. FORMER REMOVED IAW SRM 51-31-01-0G. FABRICATED A NEW FORMER IAW DRAWING ARB 2931, REVISION H, AND INSTALLED THE FORMER IAW SRM 51-33- 01-0G. THE REPAIR WAS CLASSIFIED AS MAAug 15, 2017 · N584FE · Doug MD11F · Wing Main, Frame StructureSDR FDEA201708152207Doubler · crackedLEFT WING LEADING EDGE SKIN INTERNAL SUPPORT BEADED DOUBLER FOUND CRACK AT XOS 613. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 15, 2017 · N584FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201708152206Doubler · crackedLEFT WING LEADING EDGE SKIN INTERNAL SUPPORT BEADED DOUBLER FOUND CRACKED AT XOS 640. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 15, 2017 · N584FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201708152205Doubler · crackedLEFT WING LEADING EDGE SKIN INTERNAL SUPPORT DOUBLER FOUND CRACKED AT XOS 627 . REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 15, 2017 · N584FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201708152204Stiffener · crackedLEFT WING LEADING EDGE LOWER SKIN SUPPORT STIFFENER FOUND CRACK AT XOS 547. THE STIFFENER WAS REMOVED AND REPLACED IAW SRM 51-31-01-0G AND DRAWING ARB 2918, REVISION G, AND SRM 51-35-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 15, 2017 · N584FE · Doug MD11F · Wing, Plate/SkinSDR IPXA2017081820658Sign · damagedL1 DOOR EMERGENCY EXIT SIGN FELL OFF AND IS DAMAGED. R & R THE EXIT SIGN IAW MM 33-27-05-000-805. OPS CHECKED NORMAL.Aug 15, 2017 · N273UP · Doug MD11F · Emergency LightingSDR FDEA201708152215Doubler · crackedRT WING LEADING EDGE CAVITY BEADED DOUBLER AT STA XOS 542 - XOS 546 FOUND CRACKED. REPAIR CARRIED OUT AT RT WING LEADING EDGE CAVITY BEADED DOUBLER AT STA XOS 542 - XOS 546 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-10Aug 15, 2017 · N584FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201708152214Doubler · crackedRT WING LEADING EDGE CAVITY BEADED DOUBLER AT STA XOS 536- XOS 541 FOUND CRACKED. REPAIR CARRIED OUT AT RT WING LEADING EDGE CAVITY BEADED DOUBLER AT STA XOS 536- XOS 541 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 15, 2017 · N584FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201708152212Doubler · crackedRT WING LEADING EDGE CAVITY BEADED DOUBLER AT STA XOS 579 - XOS 584 FOUND CRACKED. REPAIR CARRIED OUT AT RT WING LEADING EDGE CAVITY BEADED DOUBLER AT STA XOS 579 - XOS 584 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-10Aug 15, 2017 · N584FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201708152210Splice · corrodedCENTER LANDING GEAR, RT FWD UPPER BRACE ATTACH FITTING SPLICE FOUND CORRODED BS 1461. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-00-2R, FIGURE 202. REMOVED IAW SRM 51-33-01-0G, FABRICATED A NEW SPLICE IAW DRAWING AEA 7130, REVISION C, AND INSTAAug 15, 2017 · N584FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR IPXA2017082320881Channel · crackedINSPECTION TYPE: 3C, WIRE HARNESS SUPPORT CHANNEL CRACKED. REMOVED, FABRICATED, AND INSTALLED THE CHANNEL IAW DWG ARL0502, SRM 51-35-01, AND SRM 51-33-01.Aug 15, 2017 · N254UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2017082420910Floor Panel · delaminatedINSPECTION TYPE: 3C, COURIER AREA FLOOR PANEL DELAMINATED NEAR BS 459. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT FLOOR PANEL IAW DWG WSP0825 AND AMM 53-21-04.Aug 14, 2017 · N254UP · Doug MD11F · Fuselage Floor PanelSDR FDEA201708142199Frame · damagedAGING A/C-EXISTING REPAIR ON FRAME AT MAIN CARGO COMPARTMENT STA 1721, L11L. EXISTING REPAIR ON FRAME AT MAIN CARGO COMPARTMENT STA 1721 L11L EVALUATED AND FOUND EXISTING FRAME REPAIR DAMAGED. DAMAGED EXISTING REPAIR ON FRAME AT MAIN CARGO COMPARTMENT STA 1721Aug 14, 2017 · N598FE · Doug MD11F · Fuselage Main, FrameSDR IPXA2017081820654Web · crackedINSPECTION TYPE: SV, RT WW OVERWING UPPER FUEL TANK AFT WEB IS CRACKED AT BS 1372 AND RBL 80. REPAIRED THE WEB IAW EA 011-5710-01-A6940, REV I/R, AND EO MD11-5710-65307-A. MAJORAug 14, 2017 · N286UP · Doug MD11F · Fuel StorageSDR IPXA2017081820653Web · crackedINSPECTION TYPE: SV, LT WW OVERWING UPPER FUEL TANK AFT WEB IS CRACKED AT BS 1372 AND LBL 80. REPAIRED THE WEB IAW EA 011-5710-01-A6940, REV I/R, AND EO MD11-5710-65307-A. (MAJOR)Aug 14, 2017 · N286UP · Doug MD11F · Fuel StorageSDR FDEA201708142200Longeron · corrodedFOUND LONGERON 52L CORRODED AT LOWER BEACON MOUNT PLATE BS 1671. REPAIRED THE LONGERON IAW SRM 53-00-05-2RAug 14, 2017 · N589FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201708132195Frame · damagedAGING A/C-EXISTING REPAIR ON FRAME LOWER YOKE AREA AT MAIN CARGO COMPARTMENT STA 535 L24L. EXISTING REPAIR ON FRAME LOWER YOKE AT MAIN CARGO COMPARTMENT STA 535 L24L EVALUATED AND FOUND DAMAGED. DAMAGED EXISTING REPAIR ON FRAME LOWER YOKE AT MAIN CARGO COMPARTAug 13, 2017 · N598FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201708132194Frame · damagedAGING A/C-EXISTING REPAIR ON FRAME UPPER YOKE AREA AT MAIN CARGO COMPARTMENT STA 535 L19L. EXISTING REPAIR ON FRAME UPPER YOKE AREA AT MAIN CARGO COMPARTMENT STA 535 L19L EVALUATED AND FOUND DAMAGED. DAMAGED EXISTING REPAIR ON FRAME UPPER YOKE AREA AT MAIN CARAug 13, 2017 · N598FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201708132193Membrane · damagedAGING A/C-EXISTING REPAIR FOUND IN COCKPIT FLOOR AT RT OBSERVER SEAT BASE WEB PANEL STA 360, X=0. EXISTING REPAIR FOUND IN COCKPIT FLOOR AT RT OBSERVER SEAT BASE WEB PANEL EVALUATED AND FOUND DAMAGED. DAMAGED EXISTING REPAIR REMOVED AND REPLACED WITH NEW COCKPAug 13, 2017 · N598FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201708132192Seat Track · damagedAGING A/C-EXISTING REPAIR ON SEAT TRACK AT MAIN CARGO COMPARTMENT BETWEEN STA 745 TO STA 765, X=-8.5 EXISTING REPAIR ON SEAT TRACK AT MAIN CARGO COMPARTMENT BETWEEN STA 745 TO STA 785, X=-8.5 EVALUATED AND FOUND DAMAGED. DAMAGED SEAT TRACK AT MAIN CARGO COMPARAug 13, 2017 · N598FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201708122198Wire · damagedDURING A SERVICE CHECK, FOUND EMERGENCY EXIT SIGN LIGHT INOPERATIVE ABOVE L1 ENTRY DOOR MOUNTED ON SLIDING CEILING PANEL. PERFORMED VISUAL INSPECTION OF WIRE B319-15-20 AND B319-16-20 RUN BETWEEN SIGN LIGHT ASSY L2-721 AND TERMINAL BLOCK S3-728. SEVERALAug 12, 2017 · N621FE · Doug MD11F · Light System WiringSDR IPXA2017083021169Floor Panel · delaminatedINSPECTION TYPE: 3C, MAIN CABIN FLOOR PANEL 231GF DELAMINATED. REPAIRED THE FLOOR PANEL IAW EA 011-5310-01-A6955 REV. IR AND EO MD11-5310-65462-A, MAJOR.Aug 11, 2017 · N254UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2017083021168Floor Panel · delaminatedINSPECTION TYPE: 3C, MAIN CABIN FLOOR PANEL 231HF DELAMINATED. REPAIRED THE FLOOR PANEL IAW EA 011-5310-01-A6954, REV IR, AND EO MD11-5310-65459-A. MAJOR.Aug 11, 2017 · N254UP · Doug MD11F · Fuselage Floor PanelSDR FDEA201708112190Light · inoperativeR1 DOOR SLIDE PRESS TO TEST INDICATOR IS INOP. REMOVED AND REPLACED EMERGENCY SLIDE PRESS TO TEST LIGHT BULBS AS REQUIRED. OPS CHECKED NORMAL PER MM 25-61-04-5. OK FOR SERVICE.Aug 11, 2017 · N615FE · Doug MD11F · Emergency EquipmentSDR IPXA2017081420473Sign · detachedEXIT SIGN AT THE RT DOOR, FELL OFF DURING TAKE OFF. REPLACED THE SIGN ASSY IAW AMM 33-27-05. OPS TESTED GOOD.Aug 11, 2017 · N257UP · Doug MD11F · Emergency LightingSDR FDEA201708102172Doubler · crackedRIGHT WING FIXED LEADING EDGE DOUBLER AT XOS 667 FOUND CRACKED. A NEW DOUBLER WAS FABRICATED IAW DRAWING ARB3954, REVISION K. REMOVED AND REPLACED THE DOUBLER IAW SRM 51-31-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 10, 2017 · N598FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201708102171Hinge Bracket · corrodedRIGHT WING INBOARD FLAP OUTBOARD AFT HINGE BRACKET (FLAP SIDE) PIVOT OUTBOARD BORE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-132256 G, PART 5, STEPS 2 AND 3. THE REPAIR WASAug 10, 2017 · N590FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201708102167Hinge Fitting · corrodedLEFT WING INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT OUTBOARD BORE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-152244 H, PART 6, STEPS 2 AND 3. THE REPAIR CLASSIFIED AAug 10, 2017 · N590FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201708102166Hinge Fitting · corrodedLEFT WING INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBOARD BORE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-132244 H, PART 6, STEPS 2 AND 3. REPAIR CLASSIFIED AS Aug 10, 2017 · N590FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201708102169Hinge Bracket · corrodedRIGHT WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACH OUTBOARD BORE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-07. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331120 B, PART 1, STEPS F1 AND F 3. THEAug 10, 2017 · N590FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201708102168Hinge Bracket · corrodedRIGHT WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACH INBOARD BORE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-07. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331120 B, PART 1, STEP F 1 AND F 3, THEAug 10, 2017 · N590FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201708102175Cable · brokenRIGHT WING OUTBOARD NR 8 SLAT HAS A BROKEN DRIVE CABLE. REPLACED THE SLAT CABLES 84E & 84F IAW AMM 20-20-06-2. PERFORMED TENSION ADJUSTMENT OF THE DRIVE CABLE.Aug 10, 2017 · N574FE · Doug MD11F · Leading Edge Slat Control SystemSDR IPXA2017081120403Idg · inoperativeATB DUE TO LOSS OF FIRST OFFICERS INSTRUMENTS WITH LOSS OF AUTO THROTTLES AND AUTO PILOT HAS A NO CAMPARE ON AIRSPEED . FADER LEVEL 2 ALERT AIRSPEED UNRELIABLE LOST 1ST OFFICERS FMC OVERHEAD PANEL LIGHT AFTER REPLACEMENT OF R2-3 RELAY AND REPLACEMENT OF THEAug 10, 2017 · N284UP · Doug MD11F · AC Generator-AlternatorSDR FDEA201708092165Seat Track · gougedMAIN DECK SEAT TRACK AT STATION 5-6, RBL 47.5, FOUND THE CROWN DAMAGED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1. REPLACED THE SEAT TRACK IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-10Aug 9, 2017 · N598FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201708092164Doubler · crackedRIGHT WING FIXED LEADING EDGE RIB DOUBLER AT XOS 584 FOUND CRACKED. A NEW DOUBLER WAS FABRICATED IAW DRAWING ARB2931, REVISION J. REMOVED AND REPLACED THE DOUBLER IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 9, 2017 · N598FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201708092163Doubler · crackedRIGHT WING FIXED LEADING EDGE RIB DOUBLER AT XOS 789 FOUND CRACKED. A NEW DOUBLER WAS FABRICATED IAW DRAWING ARB3954, REVISION K. REMOVED AND REPLACED THE DOUBLER IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 9, 2017 · N598FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201708092162Doubler · crackedRIGHT WING FIXED LEADING EDGE RIB DOUBLER AT XOS 906 FOUND CRACKED. A NEW DOUBLER WAS FABRICATED IAW DRAWING ARB3954 REVISION K. REMOVED AND REPLACED THE DOUBLER IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 9, 2017 · N598FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201708092161Former · crackedRIGHT WING FIXED LEADING EDGE FORMER ASSY AT XOS 667 FOUND CRACKED. A NEW FORMER WAS FABRICATED IAW DRAWING ARB2924, REVISION B. REMOVED AND REPLACED THE FORMER IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 9, 2017 · N598FE · Doug MD11F · Wing Main, Frame Structure
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