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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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 SDR 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 REPASDR 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 GMSDR 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 57SDR 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 SDR 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 SDR 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 SDR 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 REPSDR 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 SDR 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 SPOILESDR 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 COMPLETEDSDR 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 0SDR 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 GMMSDR 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 GMMSDR 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 SDR 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 0SDR 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-42648SDR 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 PANESDR 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 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 PANESDR 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 PANSDR 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 REVSDR 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 SDR 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 MISDR 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. 7SDR 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 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-42SDR 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-RSDR 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-4264SDR 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-REQSDR 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:ASDR 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 COMPLETEDSDR 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.SDR IPXA2024041980188Roller · damagedFOUND L1 ENTRY DOOR LATCH ROLLER DAMAGED AT FWD - UPPER SIDE. (REPLACE). OPENSDR IPXA2024030725989Panel · delaminated*SDR FILED OPEN* FOUND DELAMINATION ON VERTICAL STABILIZER PANELSDR 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.SDR 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.SDR 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.SDR 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 COMPELTEDSDR 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 SATISFACTORYSDR IPXA2024012299859Access Panel · damaged**SUPPLEMENTAL SDR**FAULT - RIGHT OUTBD ELEVATOR ACCESS PANEL 344LBR, PANEL SKIN ONE HOLE (REPAIR) REVIEWEDSDR IPXA2024011299859Unknown · unknown*SDR FILED OPEN* FAULT - RIGHT OUTBD ELEVATOR ACCESS PANEL 344LBR, PANEL SKIN ONE HOLE (REPAIR) OK TO WORKSDR 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 CARGSDR 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 CARGSDR IPXA2024012239212Beam · cracked**SUPPLEMENTAL SDR**FAULT - CRACK WEB L/H WING CTR FXD LE CAVITY NOSE BEAM , ILES 692. (REPAIR) C/W REVIEWSDR IPXA2024010939212Unknown · unknownCRACKED WEB L/H WING CTR FXD LE CAVITY NOSE BEAM , ILES 692. (REPAIR)SDR 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.REVIEWEDSDR IPXA2024012204223Skin Panel · cracked**SUPPLEMENTAL SDR**FAULT - CRACK - SKIN PNL, LH WING INBD TE UPPER FIXED PNL WBL 235 (REPAIR) REVIEWEDSDR IPXA2024012204170Skin · debonded**SUPPLEMENTAL SDR**FAULT - DISBOND - SKIN, EXTERNAL FORWARD UPPER SIDE PNL OF NO.1 PYLON TO WING (REPAIR) REVIEWEDSDR IPXA2024012204105Skin · gouged**SUPPLEMENTAL SDR**FAULT - GOUGE - SKIN, RH WING INBD MID FLAP COVE PANEL LWR SURFACE (REPAIR) REVIEWED
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