Boeing 747-44AF

Service difficulty reports · 1,135

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 = '74744AF'
  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 IPXA2026060288417Erosion Shield · damagedL/H WING L/E NO.1 V.C FLAP EXTERNAL INBD SIDE AND UPPER CORNER AREA. I.A.W. SRM 57-43-02-2R-5 REV. 106 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIR AS BELOW : REMOVE THE RAIN EROSION SHIELDS AND CLEAN. APPLY THE SEALANT TO REPAIR AREA CURED AT 70F FOR 48 HMay 28, 2026 · N577UP · Boeing 74744AF · Nacelle/Pylon, Main FrameSDR IPXA2026062168918Shear Tie · crackedCRACKED PERFORM EO-80332-JIC002 REQ 2 FOUND BS 1000 RT FRONT SPAR SHEAR TIE AT RBL 33.99 CRACK. IAW AMM 28-11-01-004-001, REV 116. REMOVED CENTER TANK ACCESS DOOR 132CZ. GVI AND CONDITION CHECKED NORMAL. REPAIR DAMAGE SHEAR TIE IAW EO-80332-JIC010, REV 3. CONMay 27, 2026 · N577UP · Boeing 74744AF · Fuselage Internal Mounting StructureSDR IPXA2026062158860Seat Track · corrodedFAULT - AFT CARGO COMPARTMENT SEAT TRACK CORROSION AT STA 1820 RBL 45. REMOVE DAMAGE SEAT TRACK I.A.W SRM 51-40-02-0G REV.106. INSTALLED FABRICATED PARTS I.A.W SRM 51-40-02-0G REV.106 AND BOEING DWG NO 65B06061 SH51 REV.- AND 65B06061 SH54 REV.-.May 26, 2026 · N577UP · Boeing 74744AF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026061858195Seal · brokenBROKEN SEAL , NR 1 ENG RT T/R FWD LWR CLOSURE DOOR LWR SEAL. REMOVED DAMAGE SEAL IAW SRM 51-40-02-0G, REV 106. INSTALLED NEW SEAL IAW SRM 51-40-02-0G, REV 106 AND IPC 78-32-22, REV 96.May 26, 2026 · N577UP · Boeing 74744AF · Engine Thrust ReverserSDR IPXA2026060858286Door · chafedCHAFING - SKIN, NO. 1 ENG R/H T/R BLOWOUT DOOR INNER L/E SKIN. IAW SRM 51-40-02-0G REV. 106 AND ST ENGINEERING IPC 78-32-22 REV. 96 INSTALLED NEW BLOWOUT DOOR.May 26, 2026 · N577UP · Boeing 74744AF · Engine Thrust ReverserSDR IPXA2026060258511Nose Cowl · dentedDENT - SKIN, NO. 1 ENG NOSE COWL INNER BARREL 11:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUTOUT ( DIA : 0.7", 22" FROM FWD EDGE AND AT 11 O'CLOCK ON THE INNER BARREL OF NR 1 ENF INLET COWL) FILL THE CUTOUT WITH ADHESIVE CURED AT 200°F FOR 1 HOUR IAMay 26, 2026 · N577UP · Boeing 74744AF · Nacelle/Pylon, Plate/SkinSDR IPXA2026052949093Flap · damagedFAULT-DAMAGE-MOLDING SEAL, L/H WING INBD L/E NO.13 KRUEGER FLAP INBD UPPER ATTACHED. I.A.W. SRM 57-43-02-2R-1 REV. 106 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIRMay 25, 2026 · N577UP · Boeing 74744AF · Leading Edge DevicesSDR IPXA2026052949133Flap · damagedFAULT-DAMAGE-MOLDING SEAL, L/H WING INBD L/E NO.11 KRUEGER FLAP INBD UPPER ATTACHED I.A.W. SRM 57-43-02-2R-1 REV. 106 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIRÂMay 25, 2026 · N577UP · Boeing 74744AF · Leading Edge DevicesSDR IPXA2026061809637Washer · missingMAJOR REPAIR, DUE TO PERFORM INSPECTION, NO WASHER INSTALLED UNDER FASTENERS HEAD ON DOUBLER, LH SIDE. ACCOMPLISH REPAIR IAW EO-97812 REQ1 REV.1 AND EO-96283-REQ2, REV 1.May 22, 2026 · N577UP · Boeing 74744AF · Fuselage Main, Plate/SkinSDR IPXA2026061809643Washer · missingDUE TO PERFORMED INSPECTION, NO WASHER INSTALLED UNDER FASTENERS HEAD ON DOUBLER, RH SIDE. ACCOMPLISH REPAIR IAW EO-97813 REQ1 REV.1 AND UPS EO-96283-REQ3 REV.1.May 22, 2026 · N577UP · Boeing 74744AF · Fuselage Main, Plate/SkinSDR IPXA2026060120516Fuel Sys · out of balanceAFTER LEVEL OFF ENG 3 FUEL INDICATED 2,000LBS LESS THAN ENG 2. WE BALANCED THE FUEL MANUALLY BUT HAD TO CONTINUE TO BALANCE THE FUEL THE ENTIRE FLIGHT. SUSPECT ENG 3 PUMPS ARE STRONGER THAN ENG2 PUMPS. REMOVED AND REPLACED MAIN 2 AFT BOOST PUMP REF AMM 28-22-May 11, 2026 · N572UP · Boeing 74744AF · Aircraft Fuel Distribution SystemSDR IPXA2026051220516Transfer Sys · malfunctionedAFTER LEVEL OFF ENG 3 FUEL INDICATED 2,000LBS LESS THAN ENG 2. WE BALANCED THE FUEL MANUALLY BUT HAD TO CONTINUE TO BALANCE THE FUEL THE ENTIRE FLIGHT. SUSPECT ENG 3 PUMPS ARE STRONGER THAN ENG 2 PUMPS DEFERRED IAW EO-97441.May 11, 2026 · N572UP · Boeing 74744AF · Aircraft Fuel Distribution SystemSDR IPXA2026042797242Adapter · corrodedADDITION SDR AND CPCP FOR SATELLITE COMMUNICATIONS (SATCOM) SYSTEM [T3F18E0082B65]. REVIEWED PER GMM-MTX 09.05.01.09.Apr 27, 2026 · N575UP · Boeing 74744AF · Fuselage Miscellaneous StructureSDR IPXA2026042329452Bolt · wornRIGHT WING OUTBOARD MID FLAP, T/E UPPER SKIN, BOLT WORN 1 EA. REMOVE THE WORN MATERIALS AND CLEAN. I.A.W DWG 65B08533, SHEET 3, ZONE C12, VIEW 2B6, REV.C. AND PSDL 65B08533 SHEET DL, REV.A. INSTALL THE RH WING OUTBD MID FLAP SUPPORT STRUT.Apr 16, 2026 · N575UP · Boeing 74744AF · Trailing Edge FlapsSDR IPXA2026042187945Fairing · damagedENLARGED HOLE NR 4 AFT FAIRING HOLE .IAW AMM 51-24-11-477-083 REV.116, REPAINT PEEL OFF AREA. CHECK NORMAL.Apr 14, 2026 · N575UP · Boeing 74744AF · Trailing Edge FlapsSDR IPXA2026042571341Angle · crackedFOUND MAIN DECK SIDE CARGO DOOR ANGLE ASSY DAMAGE. IAW SRM 51-40-02-0G REV.106. REMOVED DAMAGE ANGLE IAW SRM 51-40-02-0G REV.106, AND DWG 65B57353, SH 2, REV G, INSTALLED NEW CLIP.Apr 13, 2026 · N575UP · Boeing 74744AF · Cargo/Baggage DoorsSDR IPXA2026042162642Fitting · chafedFOUND L1 ENTRY DOOR CUTOUT AFT LOWER FITTING CHAFING. REQUEST PERFORM OK TO CLOSE CHECK FOR L1 DOOR AFT SIDE LOWER SIDEWALL PANEL.Apr 12, 2026 · N575UP · Boeing 74744AF · Fuselage Miscellaneous StructureSDR IPXA2026041750112Seal · brokenBROKEN SEAL, LT WING LANDING GEAR W/W CUTOUT FWD LWR SEAL. IAW SRM 51-40-02-0G, REV 106. REMOVED DAMAGE SEAL IAW SRM 51-40-02-0G REV. 106 AND DWG 65B10555, SH 3, REV G INSTALLED NEW SEAL.Apr 11, 2026 · N575UP · Boeing 74744AF · Fuselage Main, StructureSDR IPXA2026042047400Rub Strip · chafedCHAFED STRIP , NR 2 ENGINE LT CORE COWL INNER AFT UPPER AREA. IAW AMM 71-11-06-004-001-J00, REV 116. REMOVED THE CORE COWL. IAW SRM 51-40-02-0G, REV. 106, REMOVED DAMAGE STRIP IAW SRM 51-40-02-0G, REV 106, AND CMM IPL 71-13-23, REV 47. INSTALLED NEW STRIP IApr 11, 2026 · N575UP · Boeing 74744AF · Nacelle/Pylon, Main FrameSDR IPXA2026042547996Tube · wornWORN FLARED TUBE OF ENG-1 ADP. I.A.W.AMM 29-11-15-002-001 REV116 AND AMM29-11-15-402-009, REV 116. REPLACED THE SPEED CONTROL AIR PRESSURE LINEApr 11, 2026 · N575UP · Boeing 74744AF · Hydraulic System, MainSDR IPXA2026042447341Retainer · crackedCRACKED RETAINER, NR 2 ENG RT T/R TRANSLATING COWL UPPER TEE TRACK HINGE PIN CRACKED. IAW AMM 70-50-00-912-034, REV 116 REPLACED THE RETAINER.Apr 11, 2026 · N575UP · Boeing 74744AF · Engine Thrust ReverserSDR IPXA2026042046129Rub Strip · brokenNO. 2 ENG NOSE COWL AFT FLANGE WEAR STRIP , AT 6 O'CLOCK POSITION. I.A.W SRM 51-40-02-0G REV. 106 AND GOODRICH AEROSTRUCTURES CMM IPL 71-11-16 REV.54 INSTALLED NEW STRIP.Apr 11, 2026 · N575UP · Boeing 74744AF · Nacelle/Pylon, Main FrameSDR IPXA2026042147492Seal · frayedFRAYED SEAL, NR 1 PYLON OTBD AFT FAIRING DOOR LWR SEAL. IAW SRM 51-40-02-0G, REV 106, REMOVED DAMAGE SEAL. IAW GMM-MTX 9.08, REV 15, REQUIREMENT AND EGAT WORK SHEET 60275 AND DWG 323U2325, SH 11, REV A. DWG 323U2325-153, PL, REV A, AND ORIGINAL PART AS Apr 11, 2026 · N575UP · Boeing 74744AF · Nacelle/Pylon, Main FrameSDR IPXA2026042150427Angle · crackedCRACKED ANGLE, NR 4 ENG RT THRUST REVERSER DRIAN TUBE SUPPORT CLAMP. IAW SRM 51-40-02-0G, REV 106. REMOVED DAMAGE ANGLE. IAW SRM 51-40-02-0G, REV 106, & IPC 78-32-52, REV 96. INSTALLED NEW ANGLE.Apr 11, 2026 · N575UP · Boeing 74744AF · Engine Thrust ReverserSDR IPXA2026042047446Seal · brokenBROKEN SEAL, NR 4 PYLON LT AFT FAIRING DOOR LWR SEAL. IAW SRM 51-40-02-0G, REV 106 REMOVED DAMAGE SEAL. IAW GMM-MTX CH 9.08, REV 15 REQUIREMENT AND EGAT WORK SHEET 60267 AND DWG 323U2325, SH 11, REV A, DWG 323U2325-153, PL REV A, AND ORIGINAL PART AS A SAMApr 11, 2026 · N575UP · Boeing 74744AF · Nacelle/Pylon, Main FrameSDR IPXA2026041649774Scoop · damagedENLARGED HOLE, LT WING OUTBD LOWER FUEL VENT SCOOP PANEL FWD FASTENER HOLE. IAW DWG 112U0700, SHEET 01, REV D. REMOVED LT WING FUEL VENT SCOOP PANEL IAW DWG 112U0700, SHEET 01, REV. D. INSTALLED LT WING FUEL VENT SCOOP PANEL.Apr 11, 2026 · N575UP · Boeing 74744AF · Wing Main, Frame StructureSDR IPXA2026041547552Bracket · chafedCHAFED BRACKET, NR 1 ENG LT T/R LWR FWD CLOSURE DOOR T/E AREA. I.A.W SRM 51-40-02-0G REV. 106 REMOVED DAMAGE BRACKET. I.A.W SRM 51-40-02-0G REV. 106 AND ST ENGINEERING IPC 78-32-21 REV. 96 INSTALLED NEW BRACKET.Apr 11, 2026 · N575UP · Boeing 74744AF · Engine Thrust ReverserSDR IPXA2026041547525Bracket · chafedCHAFED BRACKET, NR 1 ENG RT THRUST REVERSER LWR FWD CLOSURE DOOR T/E AREA. I.A.W SRM 51-40-02-0G REV. 106 REMOVED DAMAGE BRACKET. I.A.W SRM 51-40-02-0G REV. 106 AND ST ENGINEERING IPC 78-32-22 REV. 96 INSTALLED NEW BRACKET.Apr 11, 2026 · N575UP · Boeing 74744AF · Engine Thrust ReverserSDR IPXA2026041547574Bracket · chafedCHAFED BRACKET, NR 2 ENG RT THRUST REVERSER FWD LWR CLOSURE DOOR T/E AREA. IAW SRM 51-40-02-0G, REV 106 REMOVED DAMAGE BRACKET. IAW SRM 51-40-02-0G, REV 106 & IPC 78-32-22 REV. 96 INSTALLED NEW BRACKET.Apr 11, 2026 · N575UP · Boeing 74744AF · Engine Thrust ReverserSDR IPXA2026042128355Seal · brokenBROKEN SEAL , NR 3 ENG, LT THRUST REVERSER AFT LWR AREA. IAW SRM 51-40-02-0G, REV 106, AND IPC 78-32-21 REV. 96, INSTALLED NEW SEAL.Apr 10, 2026 · N575UP · Boeing 74744AF · Engine Thrust ReverserSDR IPXA2026042028336Bracket · crackedCRACKED BRACKET, NR 3 ENG LT THRUST REVERSER HINGE PANEL SUPPORT BRACKET. IAW SRM 51-40-02-0G, REV 106. REMOVED DAMAGE BRACKET. IAW SRM 51-40-02-0G, REV 106, AND IPC 78-32-21, REV 96 INSTALLED NEW BRACKET.Apr 10, 2026 · N575UP · Boeing 74744AF · Engine Thrust ReverserSDR IPXA2026042711816Cover · crackedFAULT - R/H WING L/E VARIABLE CAMBER FLAP #17 INBD ROTARY ACTUATOR HAS CRACKED OTBD COVER. NO.5385. I.A.W AMM 27-81-07-004-001 REV 116 REMOVE NO.17 V.C FLAP INBD'S OUTBD ROTARY ACTUATOR. I.A.W AMM 27-81-07-404-008 REV.116 STEP 3.F.(2).(P) TO STEP 3.G.(2) ACCApr 9, 2026 · N575UP · Boeing 74744AF · Trailing Edge Flap ActuatorSDR IPXA2026042711853Cover · crackedFAULT - R/H WING L/E VARIABLE CAMBER FLAP #17 OTBD ROTARY ACTUATOR HAS CRACKED OTBD COVER. NO.5311. I.A.W AMM 27-81-07-004-001 REV 116 REMOVE NO.17 V.C FLAP ROTARY ACTUATOR. I.A.W AMM 27-81-07-404-008 REV.116 STEP 3.F.(2).(P) TO STEP 3.G.(2) ACCOMPLISHED THE IApr 9, 2026 · N575UP · Boeing 74744AF · Trailing Edge Flap ActuatorSDR IPXA2026042711764Cover · crackedLT WING L/E VARIABLE CAMBER FLAP NR 2 ROTARY ACTUATOR AT HAS CRACKED COVER. IAW AMM 27-81-07-004-001 REV 116 REMOVE NR 2 V.C FLAP ROTARY ACTUATOR. IAW AMM 27-81-07-404-008, REV.116, STEP 3.F.(2).(P) TO STEP 3.G.(2). ACCOMPLISHED THE INSTALLATION AND ADJUST Apr 9, 2026 · N575UP · Boeing 74744AF · Trailing Edge Flap ActuatorSDR IPXA2026042713748Cover · crackedRIGHT WING L/E VARIABLE CAMBER FLAP 24 ROTARY ACTUATOR AT HAS CRACKED COVER. IAW AMM 27-81-07-004-001, REV 116. REMOVE 24 V.C FLAP ROTARY ACTUATOR. IAW AMM 27-81-07-404-008, REV 116. STEP 3.F.(2).(P) TO STEP 3.G.(2). ACCOMPLISHED THE INSTALLATION AND AApr 9, 2026 · N575UP · Boeing 74744AF · Trailing Edge Flap ActuatorSDR IPXA2026042711916Cover · crackedLEFT WING LE VARIABLE CAMBER FLAP NR 5, ROTARY ACTUATOR AT HAS CRACKED COVER. 5386. IAW AMM 27-81-07-004-001, REV 116. REMOVED NR 5 VC FLAP ROTARY ACTUATOR. I.A.W AMM 27-81-07-404-008 REV.116 STEP 3.F.(2). P TO STEP 3.G. (2). ACCOMPLISHED THE INSTALLATION ANApr 9, 2026 · N575UP · Boeing 74744AF · Trailing Edge Flap ActuatorSDR IPXA2026042411547Cover · crackedCRACK- COVER, NO.4 ENG R/H T/R ACTUATOR ACCESS PNL 446B, 446C, 445C. I.A.W.AMM 78-31-10-004-001-J00 REV116 REMOVED THE PANEL 446B 446C 445C. I.A.W.AMM 78-31-10-404-008-J00 REV116 INSTALLED THE PANEL 446B 446C 445C WITH NEW.Apr 9, 2026 · N575UP · Boeing 74744AF · Engine Thrust ReverserSDR IPXA2026042411487Cover · crackedCRACK- COVER, NO.3 ENG R/H T/R ACTUATOR ACCESS PNL 436B, 436C. I.A.W.AMM 78-31-10-004-001-J00 REV116 REMOVED THE PANEL 436B 436C. I.A.W.AMM 78-31-10-404-008-J00 REV116 INSTALLED THE PANEL 436B 436C WITH NEW.Apr 9, 2026 · N575UP · Boeing 74744AF · Engine Thrust ReverserSDR IPXA2026042014756Rub Strip · chafedCHAFED RUB STRIP, NR 3 ENG RT CORE COWL AFT UPR RUB STRIP. I.A.W SRM 51-40-02-0G REV. 106 AND CMM IPL 71-13-24 REV.50 INSTALLED NEW STRIP.Apr 9, 2026 · N575UP · Boeing 74744AF · Nacelle/Pylon, Main FrameSDR IPXA2026042114858Seal · brokenBROKEN - SEAL, NR 4 ENG RT T/R CLOSURE DOOR FWD AREA. I.A.W SRM 51-40-02-0G REV. 106 REMOVED DAMAGE SEAL. I.A.W SRM 51-40-02-0G REV. 106 AND ST ENGINEERING IPC 78-32-22 REV. 96 INSTALLED NEW SEAL.Apr 9, 2026 · N575UP · Boeing 74744AF · Engine Thrust ReverserSDR IPXA2026042014715Rub Strip · chafedCHAFING AND MISSING - STRIP AND RIVET, NO.3 ENG L/H CORE COWL AFT UPR WEAR STRIP. IAW SRM 51-40-02-0G REV. 106 AND GOODRICH AEROSTRUCTURES CMM IPL 71-13-23 REV.47 INSTALLED NEW STRIP.Apr 9, 2026 · N575UP · Boeing 74744AF · Nacelle/Pylon, Main FrameSDR IPXA2026042315124Nose Cowl · dentedDENTED SKIN, NR 2 ENG NOSE COWL INNER BARREL NEAR 2:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.4", 5.5" FROM AFT EDGE, 59.5" FROM LWR EDGE, AT 2 O'CLOCK ON THE INNER BARREL OF NO.2 ENG INLET COWL ). FILL THE CUT OUT WITH ADHESIVE CUREDApr 9, 2026 · N575UP · Boeing 74744AF · Nacelle/Pylon, Main FrameSDR IPXA2026042214799Seal Depressor · crackedCRACKED DEPRESSURE SEAL, AFT CARGO DOOR CUTOUT AFT SIDE. I.A.W SRM 51-40-02-0G REV.106 REMOVE DAMAGE DRPRESSOR SEAL AND DEPRESSOR. I.A.W SRM 51-40-02-0G REV.106 AND BOEING DWG NO.65B01865 SH10 REV E AND BOEING DWG NO.65B06880 SH2 REV B INSTALL NEW DRPRESSOR Apr 9, 2026 · N575UP · Boeing 74744AF · Cargo/Baggage DoorsSDR IPXA2026041815210Fairing · dentedDENTED SKIN, LT WING T/E FLAP NR 4 AFT FAIRING EXTERNAL SURFACE LOWER SIDE ADJACENT AFT CONE. IAW SRM 57-53-70-2R-1 REFER TO SRM 51-70-17-0G-0 REV. 106 PERFORM REPAIR AS BELOW STEP: 1.1 REMOVE THE DAMAGE MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CApr 9, 2026 · N575UP · Boeing 74744AF · Trailing Edge FlapsSDR IPXA2026041811914Skin · crackedRIGHT WING INBOARD T/E UPPER FIXED PANEL SKIN CRACK, WBL 235.2. I.A.W. 747-400F SRM 57-51-01-2R-1 REFER TO SRM 51-70-07-0G-0 REV. 106 PERFORM REPAIR AS BELOW STEP: 1.1 REMOVE THE CRACK MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 26Apr 9, 2026 · N575UP · Boeing 74744AF · Wing, Plate/SkinSDR IPXA2026041322009Window · crackedAT FL 370 FWD WINDOW LEFT CRACKED. R & R L1 WINDOW IAW AMM 56-11-01/401. REPLACED WINDOW HEAT CONTROL UNIT IAW AMM 30-41-01/401. OPS CHKD WINDSHIED HEATER SYS AND WIPER IAW AMM 30-41-00/501 & 30-42-00/501, CHKD NORMAL, AIRCRAFT OK FOR SERVICE.Apr 9, 2026 · N572UP · Boeing 74744AF · Flight Compartment WindowsSDR IPXA2026041214960Floorboard · damagedMAJOR REPAIR. DAMAGED FLOORBOARD ON RT MAIN CARGO DECK BS 1220. REMOVE THE DAMAGED PANEL IN ACCORDANCE WITH AMM 53-21-02. INSTALL THE REPLACEMENT FLOOR PANEL PER AMM 53-21-02.Apr 9, 2026 · N575UP · Boeing 74744AF · Fuselage Floor PanelSDR IPXA2026041022009Window · crackedAT FL 370, FWD WINDOW LEFT CRACKEDApr 9, 2026 · N572UP · Boeing 74744AF · Flight Compartment WindowsSDR IPXA2026042573876Panel · brokenFWD CARGO COMPARTMENT CEILING PANEL ASSY ZIPPER BROKEN AT STA 840 - 860. .I.A.W AMM25-52-01-004-049 REV116 AND I.A.W AMM25-52-01-404-062 REV116 REPLACE PANEL ASSY WITH NEW PARTS.Apr 7, 2026 · N575UP · Boeing 74744AF · Cargo CompartmentsSDR IPXA2026042355538Support · wornFOUND LT WING OTBD FLAP NR 7 SUPPORT STRUT (OTBD TO INBD) UPPER AND LOWER PANEL WORN. I.A.W DWG 65B08533, SHEET 3, ZONE C12, VIEW 2B6, REV.C. REMOVED THE LH WING OUTBD FLAP NO.7 SUPPORT STRUT (OUTBD TO INBD). FAULT- FOUND LH WING OUTBD FLAP NO.7 SUPPORT STRUTApr 6, 2026 · N575UP · Boeing 74744AF · Wing Miscellaneous Structure
Back to Boeing 747-44AF