Boeing 747-4J6
Service difficulty reports · 133
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 = '7474J6' 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 = '7474J6' 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 UIEA2010122200235Cargo Track · wornWEAR - MAIN DECK CARGO RAIL SURFACE HAD WEAR CONDITION WAS FOUND AT RT SIDE STA 1200- 1366. (REMOVE DAMGE IAW EO 4425A201 FIG 2 AND FIG 6 AND EI NO T2010A538-2993, REV 00, REV 01.)SDR UIEA2010122200234Cargo Track · wornWEAR - MAIN DECK CARGO RAIL SURFACE HAD WEAR CONDITON WAS FOUND AT LT SIDE, STA 1270- 1366. (REMOVE DAMAGE IAW EO 4425A201 FIG 2 AND FIG 6, REV A. EI NO T2010A53B-2993, REV 00, REV 01)SDR UIEA2010122200233Cargo Track · wornWEAR - MAIN DECK CARGO RAIL SURFACE HAD WEAR CONDITON. WAS FOUND AT RT SIDE, STA 1230 - 1270. (REMOVE DAMAGE IAW EO 4425A201 FIG 2 AND FIG 6, REV A AND EI NO T2010A53B-2993, REV 00 - REV 01.)SDR UIEA2010122200232Cargo Track · wornWEAR - MAIN DECK CARGO RAIL SURFACE HAD WEAR CONDITON WAS FOUND AT RT SIDE, STA 770-870. (REMOVED DAMAGE IAW EO 4425A201, FIG 2 AND FIG 6, REV A AND EI NR T2010A53B-3144, REV 00, REV 01.)SDR UIEA2010122200230Cargo Track · wornWEAR - MAIN DECK CARGO RAIL SURFACE HAD WEAR CONDITION WAS FOUND AT LT SIDE, STA 770-870. (REMOVED DAMAGE IAW EO 4425A201 FIG 2 AND FIG 6, REV A. AND EI NO T2010A53B-3144, REV 00.)SDR UIEA2010122200229Cargo Track · wornWEAR - MAIN DECK CARGO RAIL SURFACE HAD WEAR CONDITION WAS FOUND AT RT SIDE, STA 670-770 (REMOVED DAMAGE IAW EO 4425A201 FIG 2 AND FIG 6, REV A AND EI NO T2010A53B-3144 REV 00 AND REV 01.)SDR UIEA2010122200228Cargo Track · wornWEAR - MAIN DECK CARGO RAIL SURFACE HAD WEAR CONDITON WAS FOUND AT LT SIDE, STA 670 - 770. (REMOVED DAMAGE IAW EO 4425A201 FIG 2 AND FIG 6, REV A AND EI NR T2010A53B-3144 REV 00 AND REV 01.)SDR UIEA2010122200227Cargo Track · wornWEAR - MAIN DECK CARGO RAIL SURFACE HAD WEAR CONDITION WAS FOUND AT LT SIDE STA 660- 670. (REMOVED DAMAGE IAW EO 4425A201 FIG 2 AND FIG 6, REF A AND EI NO T2010A53B-3144 REV 00 AND REV 01 & NBSP;)SDR UIEA2010122200226Cargo Track · wornWEAR - MAIN DECK CARGO RAIL SURFACE HAD WEAR CONDITION WAS FOUND AT RT SIDE, STA 990 -1070. (REMOVED DAMAGE IAW EO 4425A201, FIG 2 AND FIG 6, REV A AND EI NO T2010A53B-3129 REV -- REV 01 REV 02.)SDR UIEA2010122200225Cargo Track · wornWEAR MAIN DECK CARGO RAIL SURFACE HAD WEAR CONDITION WAS FOUND AT RT SIDE, STA 870-990. (REMOVED DAMAGE IAW EO 4425A201, FIG 2 AND FIG 6 REV A. AND EI NO T2010A53B - 3129 - REV 00 00/01).SDR UIEA2010122200224Cargo Track · wornWEAR - MAIN DECK CARGO RAIL SURFACE HAD WEAR CONDITION WAS FOUND AT LT SIDE, STA 990 - 1070. (REMOVE DAMAGE IAW EO 4425A201, FIG 2 AND FIG 6, REV A AND EI NR T2010A53B-3129, REV 00, REV 01, REV 02.)SDR UIEA2010122200223Skin · chafedREPAIR - BROKEN AND CHAFING ON UNDER FAIRING SKIN AT STA 1253.5, RBL 77.65. (REPAIR IAW T2010A53B-3068, REV 00 & NBSP;)SDR UIEA2010122200213Skin · chafedOTBD AFT FLAP UPPER SURFACE CHAFED ON EXISTING REPAIR DOUBLER. (REPAIR IAW EGAT EI NR T2010A57B-3117, REV 00 AND REV 01)SDR UIEA2010122200212Unknown · misrepairedDEVIATION DURING PERFORM EO NR 4421A060, SHORT EDGE MARGIN INTERFERENCE OVERSIZE HOLE. (IAW EI NR T2010A21B-3142, REV 00 AND REV 01.)SDR UIEA2010122200208Cargo Track · wornWEAR - MAIN DECK CARGO RAIL SURFACE HAD WEAR CONDITION WAS FOUND AT LT SIDE, STA 1990 - 2050. (REMOVED DAMAGE IAW EO 4425A201, FIG 2 AND FIG 6 REV A AND EI, NO T2010A53B - 3147, REV 00, REV 01.)SDR UIEA2010122200200Cargo Track · wornWEAR MAIN DECK CARGO RAIL SURFACE HAD WEAR CONDITION WAS FOUND AT LT SIDE STA 1490 - STA 1590 (REMOVED DAMAGE IAW EO 4425A201, FIG 2 AND FIG 6, REV A AND EI NO T2010A53B-3126, REV 00, REV 01).SDR UIEA2010122100222Seal · chafedCHAFING - DEPRESSOR SEAL . LT WING INBD MID FLAP OTBD SIDE WBL 443 (TRIM OUT DAMAGE AREA IAW EI NO T2010A57B - 3077 REV 00).SDR UIEA2010122100217Skin · crackedCRACK ON AFT CARGO DOOR LOWER SKIN PANEL ON STA 1816 S-39R. (REPAIR IAW EI T2010A52B-3067 REV 00 AND REV 01.02)SDR UIEA2010122100216Fairing · crackedCRACK FWD NR1 PYLON OTBD SIDE T/E FAIRING DOOR REPAIR DOUBLER CRACK. (REPAIR CRACK NR 1 ENG OTBD STRUT DOOR SKIN EXISTING DOUBLER OUTER SURFACE IAW EI NO T2010A54B - 2994, REV 00 AND REV 01.)SDR UIEA2010121800220Fitting · chafedFWD NR 5 CARRIAGE FITTING CHAFING (RT INBD T/E MID FLAP SPAR) (IAW EI NO T2010A57B-3125, REV 00).SDR UIEA2010121800219Fitting · chafedFWD NR 4 CARRIAGE FITTING CHAFING (LT INBD T/E MID FLAP SPAR) (IAW EI NO T2010A57B - 3125, REV 00).SDR UIEA2010121700218Fairing · crackedCRACK - FWD FUSELAGE STA 1375 LT LONGERON BOX FAIRING SKIN CRACK AND SUPPORT CRACK. ( REPLACED WITH NEW SUPPORT IAW SRM & NBSP;53-40-02 REV 16. REPAIR DAMAGED SKIN IAW SRM 53-00-70, REF 51-70-07, REV 16 & NBSP;)SDR UIEA2010120900215Support Angle · crackedANGLE FUSELAGE, STA 1325, RT LONGERON BOX SUPPORT CRACKED. REMOVED EDGE CRACK AREA IAW 747-400 SRM 53-40-05, FIG 101, DETAIL IN REV 16.SDR UIEA2010080900136Structure · crackedRT WING OTBD MID FLAP, T/E COVE PANEL CTR BY SUPPORT LINKS 2 EA CRACKS, (1) CRACK ABOUT 13" LONG AND SECOND CRACK ABOUT 6" LONG. (REPAIRED IAW SRM 57-53-01, FIG 201, REPAIR 3.)SDR UIEA2010080800135Skin · puncturedTHE PURPOSE OF THIS EO IS TO DOCUMENT A MAJOR REPAIR. DURING INSP PHASE OF SCHEDULE MX CHECK, PUNCTURE DAMAGE WAS DISCOVERED ON THE LT WING INBD AFT FLAP T/E - LOWER SURFACE (REF FIG 1). THE PUNCTURE IS 0.25 IN. DIAM. (2.0 IN. AFTER DAMAGE REMOVAL). (PERMANENSDR EIA2008002Floorbeam · bentBODY STATION 1780, LBL 29, WL 118 FLOORBEAM UPPER CHORD HAS AFT FLANGE BENT. REMOVED DAMAGED FLANGE UPPER CHORD. FABRICATED AND INSTALLED REPAIR PER B747 SRM 51-70-12 PAGES 201-207 AND 51-40-02 PAGES 1-3.SDR EIA2008006Floorbeam · gougedFLOORBEAM WEB HAS DEEP GOUGE AT BS 1780, LBL 16, WL 105. REMOVED DAMAGED SECTION OF WEB FABRICATED AND INSTALLED REPAIR PER B747 SRM 53-00-07 PAGES 201-202 AND 51-40-02 PAGE 1-3.SDR EIA2008004Skin · dentedSECTION 48 TAIL CONE STATION 2700 RT SIDE DENTED 2 PLACES JUST AFT OF APU INLET DOOR. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER B747 SRM 53-00-01 FIGURE 201 SHEET 5 TABLE III.SDR EIA2008001Stringer · crackedBS 296 STRINGER 30R CRACKED. CUTOUT DAMAGE STRINGER SECTION. NDT AREA, FABRICATED AND INSTALLED REPAIR PER B747 SRM 53-00-03 PAGES 201-202 AND PAGES 206-207.SDR EIA2008005Floorbeam · puncturedFLOORBEAM WEB PUNCTURED BODY STATION 1800, LBL 53, WL 108. REMOVED DAMAGED AREA OF WEB, FABRICATED AND INSTALLED REPAIR PER ENGINEERING DISPOSITION LETTER ITEM 1 AND 2 DATED 12-21-07 AND B747 SRM 53-00-07 PAGES 201-203.SDR EIA2008003Floorbeam · bentBODY STATION 1780, RBL 18, WL 118 FLOORBEAM UPPER CHORD HAS AFT FLANGE BENT. CUT OUT DAMAGED CHORD, FABRICATED AND INSTALLED REPAIR PER B747 SRM 51-70-12 PAGE 202 FIGURE 201, 51-70-12 PAGES 201-206 AND 51-40-02 PAGE 1.SDR EIA2007201Fmu · malfunctionedON FINAL EICAS MSG "ENG 4 FAIL". PERFORMED FAULT ISOLATION MANUAL PROCEDURES TASK 71-00-919 DUE TO NR 4 CONTROL MESSAGE 74077, OPS CHECK GOOD PER FAULT ISO MANUAL. REMOVED AND REPLACED FMU PER B747-400 AMM 73-21-01. ACCOMPLISHED POWER PLANT TEST NR 3 PER B7SDR EIA2007189Controller · malfunctionedON CLIMB AT 240 WIINDOW R1 ARCING WITH APPROX 3 FOOT CRACK ON OUTER PANE. REMOVED AND REPLACED R1 FWD WINDSHIELD HEAT CONTROL UNIT PER MM 30-41-01 AND R1 WINDSHIELD PER MM 56-11-01 WINDOW HEAT SYSTEM. OPS CHECKED GOOD PER MM 30-41-01. (GOOD MODEL)
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