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 IPXA2024050972896Skin · dentedLEFT WING NR 2 SPOILER UPPER SURFACE FOUND DENT, 1.DIA:0.76", DEPTH:0.005", 29" FROM T/E, 16.5" FROM INBD EDGE, 2. DIA:0.66", DEPTH:0.007", 29.25" FROM T/E,18.5" FROM INBD (REPAIR) REPAIR I/A/W: B747-400F (REV. 100) SRM 51-70-10-2R-2 AND 51-70-10-2R-0 PER SRM May 2, 2024 · N575UP · Boeing 74744AF · SpoilersSDR IPXA2024051474370Skin · dentedRIGHT WING NO.10 SPOILER UPPER SURFACE FOUND DENT, DIA:0.8", DEPTH:0.006", 10.5", FROM T/E, 16.5" FROM INBD EDGE (REPAIR) REPAIR I/A/W: B747-400F (REV. 100) SRM 51-70-10-2R-2 AND 51-70-10-2R-0 PER SRM 57-20-01-2R-1 (DETAIL I). REPAIR CLASSIFICATION: MAJOR REPAMay 2, 2024 · N575UP · Boeing 74744AF · SpoilersSDR IPXA2024051272845Skin · dentedLEFT WING NR 3 SPOILER UPPER SURFACE FOUND DENT, 1. DIA:0.52", DEPTH:0.003", 36.5" FROM T/E, 19.5" FROM OUTBD EDGE. (REPAIR) REPAIR IAW: (REV. 100) SRM 51-70-10-2R-2 AND 51-70-10-2R-0 PER SRM 57-20-01-2R-1 (DETAIL I). REPAIR CLASSIFICATION: MAJOR REPAIR PER GMMay 2, 2024 · N575UP · Boeing 74744AF · SpoilersSDR IPXA2024051272835Skin · dentedLEFT WING NR 3 SPOILER UPPER SURFACE FOUND DENT, 1.DIA:0.64",DEPTH:0.008",16.25" FROM T/E,14" FROM INBD EDGE, 2.DIA:0.52",DEPTH:0.007",11.75" FROM T/E,19" FROM INBD EDGE (REPAIR) REPAIR I/A/W: B747-400F (REV. 100) SRM 51-70-10-2R-2 AND 51-70-10-2R-0 PER SRM 57May 2, 2024 · N575UP · Boeing 74744AF · SpoilersSDR IPXA2024051272791Skin · dentedLEFT WING NR 3 SPOILER UPPER SURFACE FOUND DENT, 1. DIA: 0.81", DEPTH: 0.009", 21.5" FROM T/E, 4.5" FROM OUTBD EDGE. (REPAIR) REPAIR I/A/W: B747-400F (REV. 100) SRM 51-70-10-2R-2 AND 51-70-10-2R-0 PER SRM 57-20-01-2R-1 (DETAIL I). REPAIR CLASSIFICATION: MAJOR May 2, 2024 · N575UP · Boeing 74744AF · SpoilersSDR IPXA2024051272773Skin · dentedLEFT WING NR 3 SPOILER UPPER SURFACE FOUND DENT, 1.DIA:0.65",DEPTH:0.012",12" FROM T/E,15" FROM OUTBD EDGE, 2.DIA:0.66" DEPTH:0.008",14.75" FROM T/E,11.5" FROM OUTBD EDGE. (REPAIR) REPAIR I/A/W: B747-400F (REV. 100) SRM 51-70-10-2R-2 AND 51-70-10-2R-0 PER SRM May 2, 2024 · N575UP · Boeing 74744AF · SpoilersSDR IPXA2024051272720Skin · dentedLEFT WING NR 3 SPOILER UPPER SURFACE FOUND DENT, 1. DIA:0.55", DEPTH:0.006", 12.75" FROM T/E, 36.5" FROM INBD EDGE. (REPAIR) REPAIR I/A/W: B747-400F (REV. 100) SRM 51-70-10-2R-2 AND 51-70-10-2R-0 PER SRM 57-20-01-2R-1 (DETAIL I). REPAIR CLASSIFICATION: MAJOR May 2, 2024 · N575UP · Boeing 74744AF · SpoilersSDR IPXA2024051272686Skin · dentedLEFT WING NR 3 SPOILER UPPER SURFACE FOUND DENT, 1. DIA:0.61", DEPTH:0.009", 2" FROM T/E, 19.25" FROM OUTBD EDGE. (REPAIR) REPAIR I/A/W: B747-400F (REV. 100) SRM 51-70-10-2R-2 AND 51-70-10-2R-0 PER SRM 57-20-01-2R-1 (DETAIL I). REPAIR CLASSIFICATION: MAJOR REPMay 2, 2024 · N575UP · Boeing 74744AF · SpoilersSDR IPXA2024051372644Spoiler · dentedLEFT WING NR 4 SPOILER UPPER SURFACE FOUND DENT, 1.DIA:0.9", DEPTH:0.011", 9.5" FROM T/E,26.25" FROM INBD EDGE, 2.DIA:0.83",DEPTH:0.011",9.5" FROM T/E,31.5" FROM INBD EDGE.(REPAIR) REPAIR I/A/W: B747-400F (REV. 100) SRM 51-70-10-2R-2 AND 51-70-10-2R-0 PER SRM May 2, 2024 · N575UP · Boeing 74744AF · SpoilersSDR IPXA2024051474404Skin · dentedFAULT- DENT- SKIN, R/H WING NO.10 SPOILER UPPER SURFACE FOUND DENT, DIA:1.19", DEPTH:0.016", 23.5", FROM T/E, 40" FROM INBD EDGE 2.DIA:1.62", DEPTH:0.011", 23.5" FROM T/E, 35" FROM INBD EDGE (REPAIR).REPAIR 2 EA DENT WITH EXISTING BLENDEN AREAS ON NO.10 SPOILEMay 2, 2024 · N575UP · Boeing 74744AF · SpoilersSDR IPXA2024052675124Seat Track · crackedFAULT - CRACK - FOUND MAIN DECK SEAT TRACK CRACK AT BETWEEN STA 1700-1720, LBL 11. (REPAIR). REPAIR DAMAGE AREA I.A.W SRM 53-00-52-2R-12 REPAIR 12 REV. 100 AND ACCOMPLISHED UPS EO-90480-REQ1 REV.1. REVIEW COMPLETEDMay 2, 2024 · N575UP · Boeing 74744AF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2024051258395Skin · dentedLEFT WING NO.1 SPOILER SURFACE FOUND DENT, DIA:1", DEPTH:0.0125", 26.5" FROM T/E, 3" FROM OUTBD EDGE (REPAIR) REPAIR I/A/W: B747-400F (REV. 100) SRM 51-70-10-2R-2 AND 51-70-10-2R-0 PER SRM 57-20-01-2R-1 (DETAIL I). REPAIR CLASSIFICATION: MAJOR REPAIR PER GMM 0May 1, 2024 · N575UP · Boeing 74744AF · SpoilersSDR IPXA2024051258381Skin · dentedLEFT WING NO.1 SPOILER SURFACE FOUND DENT, DIA:1.3", DEPTH:0.0215", 7.5" FROM T/E, 18" FROM OUTBD EDGE (REPAIR) REPAIR I/A/W: B747-400F (REV. 100) SRM 51-70-10-2R-2 AND 51-70-10-2R-0 PER SRM 57-20-01-2R-1 (DETAIL I). REPAIR CLASSIFICATION: MAJOR REPAIR PER GMMMay 1, 2024 · N575UP · Boeing 74744AF · SpoilersSDR IPXA2024051258367Skin · dentedL/H WING NO.1 SPOILER SURFACE FOUND DENT, DIA:1.15", DEPTH:0.0145", 12" FROM T/E, 29.5" FROM INBD EDGE (REPAIR) REPAIR I/A/W: B747-400F (REV. 100) SRM 51-70-10-2R-2 AND 51-70-10-2R-0 PER SRM 57-20-01-2R-1 (DETAIL I). REPAIR CLASSIFICATION: MAJOR REPAIR PER GMMMay 1, 2024 · N575UP · Boeing 74744AF · SpoilersSDR IPXA2024051258332Skin · dentedL/H WING NO.1 SPOILER SURFACE FOUND DENT, DIA:1.33", DEPTH:0.02", 23" FROM T/E, 9.25" FROM OUTBD EDGE (REPAIR) REPAIR I/A/W: B747-400F (REV. 100) SRM 51-70-10-2R-2 AND 51-70-10-2R-0 PER SRM 57-20-01-2R-1 (DETAIL I). REPAIR CLASSIFICATION: MAJOR REPAIR PER GMM May 1, 2024 · N575UP · Boeing 74744AF · SpoilersSDR IPXA2024051258277Skin · dentedL/H WING NO.1 SPOILER SURFACE FOUND DENT, DIA:0.88", DEPTH:0.01", 33" FROM T/E, 7.5" FROM OUTBD EDGE (REPAIR) REPAIR I/A/W: B747-400F (REV. 100) SRM 51-70-10-2R-2 AND 51-70-10-2R-0 PER SRM 57-20-01-2R-1 (DETAIL I). REPAIR CLASSIFICATION: MAJOR REPAIR PER GMM 0May 1, 2024 · N575UP · Boeing 74744AF · SpoilersSDR IPXA2024051423415Floor Panel · brokenFAULT - BROKEN - FOUND MAIN DECK FLOOR PANEL BROKEN, PNL NO. 232FF. ( P/N : 141U5877-136 ) (REPAIR) I.A.W AMM 53-21-02-404-006 REV.110 INSTALL MAIN DECK FLOOR PANEL.JOB COMPLETED AND CONDITION CHECK SATISFACTORY. 1.FABRICATE A NEW FLOOR PANEL I.A.W. SREO-42648Apr 29, 2024 · N575UP · Boeing 74744AF · Fuselage Floor PanelSDR IPXA2024051422773Floor Panel · brokenFAULT - BROKEN - FOUND MAIN DECK FLOOR PNL NO.251NF BROKEN AT STA 1540 NEAR LBL 35 ( P/N : 146U5817-155 ) (REPAIR) I.A.W AMM 53-21-02-404-006 REV.110 INSTALL MAIN DECK FLOOR PANEL. 6. JOB COMPLETED AND CONDITION CHECK SATISFACTORY. 1.FABRICATE A NEW FLOOR PANEApr 29, 2024 · N575UP · Boeing 74744AF · Fuselage Floor PanelSDR IPXA2024051422498Floor Panel · brokenFAULT - BROKEN - FOUND MAIN DECK FLOOR PNL NO.251PF BROKEN AT STA 1580, NEAR LBL 78 ( P/N : 146U5880-5 ) (REPAIR) I.A.W AMM 53-21-02-404-006 REV.110 INSTALL MAIN DECK FLOOR PANEL. 6. JOB COMPLETED AND CONDITION CHECK SATISFACTORY. 1.FABRICATE A NEW FLOOR PANELApr 29, 2024 · N575UP · Boeing 74744AF · Fuselage Floor PanelSDR IPXA2024051422807Floor Panel · brokenFAULT - BROKEN - FOUND MAIN DECK FLOOR PNL NO.252NF BROKEN AT STA 1540 NEAR RBL 35 ( P/N : 146U5817-154 ) (REPAIR) I.A.W AMM 53-21-02-404-006 REV.110 INSTALL MAIN DECK FLOOR PANEL. 6. JOB COMPLETED AND CONDITION CHECK SATISFACTORY. 1.FABRICATE A NEW FLOOR PANEApr 29, 2024 · N575UP · Boeing 74744AF · Fuselage Floor PanelSDR IPXA2024051422502Floor Panel · brokenFAULT - BROKEN - FOUND MAIN DECK FLOOR PNL BROKEN AT BETWEEN STA 2260 ~ 2280, RBL 33 ( P/N : 146U5880-29 ) (REPAIR) I.A.W AMM 53-21-02-404-006 REV.110 INSTALL MAIN DECK FLOOR PANEL. 6. JOB COMPLETED AND CONDITION CHECK SATISFACTORY. 1.FABRICATE A NEW FLOOR PANApr 29, 2024 · N575UP · Boeing 74744AF · Fuselage Floor PanelSDR IPXA2024051422433Floor Panel · brokenFAULT - BROKEN - FOUND MAIN DECK FLOOR PNL NO.251RF BROKEN ( P/N : 146U5817-117 ) (REPAIR) I.A.W AMM 53-21-02-404-006 REV.110 INSTALL MAIN DECK FLOOR PANEL.JOB COMPLETED AND CONDITION CHECK SATISFACTORY. 1.FABRICATE A NEW FLOOR PANEL I.A.W. SREO-42648-REQ1 REVApr 29, 2024 · N575UP · Boeing 74744AF · Fuselage Floor PanelSDR IPXA2024050922962Skin · dentedFAULT - DENT - SKIN, R/H WING NO.9 SPOILER UPPER SURFACE FOUND DENT, DIA:0.65", DEPTH:0.003", 29.5" FROM T/E, 12" FROM OUTBD EDGE (REPAIR) INSTALL THE DOUBLER WITH FILM ADHESIVE AND CURED AT 250°F FOR150 MINTES WITH MINIMUM VACUUM OF 20 IN/HG I.A.W. 747-400F Apr 29, 2024 · N575UP · Boeing 74744AF · SpoilersSDR IPXA2024050922952Skin · dentedFAULT - DENT - SKIN, R/H WING NO.9 SPOILER UPPER SURFACE FOUND DENT, DIA:0.8", DEPTH:0.002", 25" FROM T/E, 15.5" FROM INBD EDGE (REPAIR) MAJOR REPAIR PER GMM 05.04.01.02 REV.7A. INSTALL THE DOUBLER WITH FILM ADHESIVE AND CURED AT 250°F FOR 150 MINUTES WITH MIApr 29, 2024 · N575UP · Boeing 74744AF · SpoilersSDR IPXA2024050922934Skin · dentedFAULT - DENT - SKIN, R/H WING NO.9 SPOILER UPPER SURFACE FOUND DENT, L:1.47", W:1", DEPTH:0.007", 15.5" FROM T/E, 12" FROM INBD EDGE (REPAIR) INSTALL THE REPAIR PARTS WITH FILM ADHESIVE AND CURED AT 250°F FOR150 MINTES WITH MINIMUM VACUUM OF 20 IN/HG I.A.W. 7Apr 29, 2024 · N575UP · Boeing 74744AF · SpoilersSDR IPXA2024051423417Floor Panel · damagedFAULT - FLOOR PANEL DAMAGE - FOUND FLOOR PANEL SCREW HOLE WORN OUT, PNL NO. 212RF. ( P/N : 141U5876-99 ) (REPAIR) I.A.W AMM 53-21-02-404-006 REV.110 INSTALL MAIN DECK FLOOR PANEL. 6. JOB COMPLETED AND CONDITION CHECK SATISFACTORY. 1.FABRICATE A NEW FLOOR PANELApr 29, 2024 · N575UP · Boeing 74744AF · Fuselage Floor PanelSDR IPXA2024051423435Floor Panel · brokenFAULT - BROKEN - FOUND MAIN DECK FLOOR PANEL BROKEN, PNL NO. 211DF. ( P/N : 141U5876-55 ) (REPAIR) I.A.W AMM 53-21-02-404-006 REV.110 INSTALL MAIN DECK FLOOR PANEL. 6. JOB COMPLETED AND CONDITION CHECK SATISFACTORY. 1.FABRICATE A NEW FLOOR PANEL I.A.W. SREO-42Apr 29, 2024 · N575UP · Boeing 74744AF · Fuselage Floor PanelSDR IPXA2024051423470Floor Panel · crackedFAULT - CRACK - FOUND MAIN DECK FLOOR PANEL CRACK, PNL NO. 231EF. ( P/N : 141U5877-134 ) (REPAIR) I.A.W AMM 53-21-02-404-006 REV.110 INSTALL MAIN DECK FLOOR PANEL.JOB COMPLETED AND CONDITION CHECK SATISFACTORY. 1.FABRICATE A NEW FLOOR PANEL I.A.W. SREO-42648-RApr 29, 2024 · N575UP · Boeing 74744AF · Fuselage Floor PanelSDR IPXA2024051423429Floor Panel · crackedFAULT - CRACK - FOUND MAIN DECK FLOOR PANEL CRACK, PNL NO. 272NF. ( P/N : 146U5884-11 ) (REPAIR) I.A.W AMM 53-21-02-404-006 REV.110 INSTALL MAIN DECK FLOOR PANEL. 6. JOB COMPLETED AND CONDITION CHECK SATISFACTORY. 1.FABRICATE A NEW FLOOR PANEL I.A.W. SREO-4264Apr 29, 2024 · N575UP · Boeing 74744AF · Fuselage Floor PanelSDR IPXA2024051423426Floor Panel · crackedFAULT - CRACK - FOUND MAIN DECK FLOOR PANEL, PNL NO. 212JG. ( P/N : 141U5876-104 ) (REPAIR) I.A.W AMM 53-21-02-404-006 REV.110 INSTALL MAIN DECK FLOOR PANEL. 6. JOB COMPLETED AND CONDITION CHECK SATISFACTORY. 1.FABRICATE A NEW FLOOR PANEL I.A.W. SREO-42648-REQApr 29, 2024 · N575UP · Boeing 74744AF · Fuselage Floor PanelSDR IPXA2024052345715Hinge Fitting · damagedFOUND R/H WING NO.10 SPOILER INBD NO.1 HINGE BOLT HOLE ENLARGE.COMPLETED MACHINING THE HINGE FITTING I.A.W. EI NO.F2024A57M-1178 REV.0 SEQUENCE:AApr 24, 2024 · N575UP · Boeing 74744AF · SpoilersSDR IPXA2024052590591Shear Tie · crackedFAULT - CRACK, DURING PERFORM EO-80332-JIC001 FOUND SHEAR TIE CRACK AT STA 1000, LBL 33.99. (REPLACE). ACCOMPLISH REPAIR PER EO-90397-REQ1 . ACCOMPLISHED EO-80332-JIC006 REV2. REVIEW COMPLETEDApr 20, 2024 · N575UP · Boeing 74744AF · Fuselage Internal Mounting StructureSDR IPXA2024051780188Roller · damagedFOUND L1 ENTRY DOOR LATCH ROLLER DAMAGED AT FWD - UPPER SIDE. (REPLACE). I.A.W AMM 52-11-01-735-080 REV 110 REPLACED L1 ENTRY DOOR LATCH ROLLER.Apr 19, 2024 · N575UP · Boeing 74744AF · Passenger/Crew DoorsSDR IPXA2024041980188Roller · damagedFOUND L1 ENTRY DOOR LATCH ROLLER DAMAGED AT FWD - UPPER SIDE. (REPLACE). OPENApr 19, 2024 · N575UP · Boeing 74744AF · Passenger/Crew DoorsSDR IPXA2024030725989Panel · delaminated*SDR FILED OPEN* FOUND DELAMINATION ON VERTICAL STABILIZER PANELMar 6, 2024 · N573UP · Boeing 74744AF · Vertical Stabilizer, Plate/SkinSDR IPXA2024040862295Shear Tie · crackedDURING PERFORM EO-80332-JIC001 FND SHEAR TIE CRACK AT LBL 33.99 STA 1000. (REPLACE) REMOVE DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.100. INSTALL NEW PARTS I.A.W. UPS EO-80332-JIC006 REV.2.Mar 2, 2024 · N574UP · Boeing 74744AF · Fuselage Internal Mounting StructureSDR IPXA2024022999856Door · inoperativeFOUND L1 DOOR AFT SIDE NOT FLUSH WHEN CLOSED, DOOR JAMMED, EXCESSIVE FORCE TO OPEN, SUSPECT DOOR OUT OF RIG. PICTURES ATTACHED ADJUSTED LOWER L1 DOOR HINGE FITTING IAW 747AMM 52-11-01. OPS CHECK AND FIT OF DOOR OPERATION GOOD IAW 747 AMM 52-11-00.Feb 28, 2024 · N576UP · Boeing 74744AF · Passenger/Crew DoorsSDR IPXA2024041455734Skin · dentedNUMBER 14 INBOARD MOST RIGHT WING KRUGER FLAP HAS 2 DENTS VERIFIED CORRECT CLEARANCES AND OPS CHECK OF THE #14 KRUEGER FLAP IAW AMM 27-81-01. ALL CHECKS GOOD AT THIS TIME.Feb 25, 2024 · N572UP · Boeing 74744AF · Leading Edge DevicesSDR IPXA2025022634582Skin · damagedWHILE REMOVING LH I/B FOREFLAP, THE LEADING EDGE WAS DAMAGED NEAR O/B HINGE FITTING. 1.INSTALLED L/H WING INBD FORE FLAP TOP PANELS I.A.W SRM 51-40-02-0G REV 100 AND AMM 20-51-01-912-008 REV 110 . 2. JOB COMPLETED. REVIEW COMPELTEDFeb 17, 2024 · N575UP · Boeing 74744AF · Trailing Edge FlapsSDR IPXA2024020595863Anti-Ice Valve · warning message*DIVERSION* NAI VALVE 3 EICAS MSG FOLLOWED BY BLD 3 OVHT/PRV, DID NOT RESET VIA QRH PROC. DURING ACCOMPLISHMENT OF THE OPS TEST OF THE PRV/ PRVC / HPSOV WHILE ENGINES RUNNING, CARRIED OUT OPS TEST OF THE NAI IAW AMM 30-21-00-710-801-001, ALL FOUND SATISFACTORYFeb 4, 2024 · N577UP · Boeing 74744AF · Ice/Rain Protection SystemSDR IPXA2024012299859Access Panel · damaged**SUPPLEMENTAL SDR**FAULT - RIGHT OUTBD ELEVATOR ACCESS PANEL 344LBR, PANEL SKIN ONE HOLE (REPAIR) REVIEWEDJan 12, 2024 · N570UP · Boeing 74744AF · Elevator, Plate/SkinSDR IPXA2024011299859Unknown · unknown*SDR FILED OPEN* FAULT - RIGHT OUTBD ELEVATOR ACCESS PANEL 344LBR, PANEL SKIN ONE HOLE (REPAIR) OK TO WORKJan 12, 2024 · N570UP · Boeing 74744AF · Elevator, Plate/SkinSDR IPXA2024012239172Seal Depressor · damagedFAULT - FWD CARGO DOOR FWD UPPER CORNER SEAL DEPRESSOR DAMAGE. (REPLACE). I.A.W AMM 20-51-01-912-008 REV.109 INSTALL SEAL DEPRESSOR. I.A.W AMM 53-21-02-004-001 REV 109 INSTALL MAIN DECK FLOOR PANEL 2EA. I.A.W AMM 25-58-02-404-126 REV.109 INSTALL MAIN DECK CARGJan 9, 2024 · N570UP · Boeing 74744AF · Fuselage Main, StructureSDR IPXA2024012239192Seal Depressor · damagedFAULT - FWD CARGO DOOR AFT UPPER CORNER SEAL DEPRESSOR DAMAGE. (REPLACE). I.A.W AMM 20-51-01-912-008 REV.109 INSTALL SEAL DEPRESSOR. I.A.W AMM 53-21-02-004-001 REV 109 INSTALL MAIN DECK FLOOR PANEL 2EA. I.A.W AMM 25-58-02-404-126 REV.109 INSTALL MAIN DECK CARGJan 9, 2024 · N570UP · Boeing 74744AF · Fuselage Main, StructureSDR IPXA2024012239212Beam · cracked**SUPPLEMENTAL SDR**FAULT - CRACK WEB L/H WING CTR FXD LE CAVITY NOSE BEAM , ILES 692. (REPAIR) C/W REVIEWJan 9, 2024 · N570UP · Boeing 74744AF · Wing Main, Frame StructureSDR IPXA2024010939212Unknown · unknownCRACKED WEB L/H WING CTR FXD LE CAVITY NOSE BEAM , ILES 692. (REPAIR)Jan 9, 2024 · N570UP · Boeing 74744AF · Wing Main, Frame StructureSDR IPXA2024021902794Skin · dented*SUPPLEMENTAL SDR* FAULT- SECTION 46 FUSELAGE SKIN REPAIR DOUBLE ONE DENT , STA1920-1940, S-31~S32R.(EVALUATE) 1.MEASURE DENT DIMENSION LENGTH:2.4", WIDTH:1.35", DEPTH:0.034, A/Y:39.7 AND PERFORMED EO-89159-REQ1 REV.1. 2.JOB COMPLETED.REVIEWEDJan 6, 2024 · N570UP · Boeing 74744AF · Fuselage Main, Plate/SkinSDR IPXA2024012204223Skin Panel · cracked**SUPPLEMENTAL SDR**FAULT - CRACK - SKIN PNL, LH WING INBD TE UPPER FIXED PNL WBL 235 (REPAIR) REVIEWEDJan 6, 2024 · N570UP · Boeing 74744AF · Wing, Plate/SkinSDR IPXA2024012204170Skin · debonded**SUPPLEMENTAL SDR**FAULT - DISBOND - SKIN, EXTERNAL FORWARD UPPER SIDE PNL OF NO.1 PYLON TO WING (REPAIR) REVIEWEDJan 6, 2024 · N570UP · Boeing 74744AF · Nacelle/Pylon, Plate/SkinSDR IPXA2024012204105Skin · gouged**SUPPLEMENTAL SDR**FAULT - GOUGE - SKIN, RH WING INBD MID FLAP COVE PANEL LWR SURFACE (REPAIR) REVIEWEDJan 6, 2024 · N570UP · Boeing 74744AF · Wing, Plate/Skin
Back to Boeing 747-44AF