Boeing 747-4H6F
Service difficulty reports · 30
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 = '7474H6F' 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 = '7474H6F' 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 UIEA2026031600090Not Reported · not reportedDEVIATION FOUND DURING PERFORMING SB-747-54A2245 ON BOTH SIDES ON NR 1 & 4 PYLON. PERFORM EI T2026A54M-360 REV 0. 2) ACCOMPLISH IAW EI T2026A54M-360 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR UIEA2025122001354Adc · faultedIAS DISAGREE EICAS MSG AFTER T/O & ALT DISAGREE EICAS MSG AT 7000 FT. REMOVED AND REPLACED L/H AIR DATA COMPUTER IAW AMM 34-12-01. PITOT STATIC LEAK CHK OK IAW AMM 34-11-00. ALTIMETER SYSTEM ACCURACY TEST OK IAW AMM 34-41-00. REMOVED AND REPLACED LEFT UPPER PSDR UIEA2025092101242Pump · illuminatedHYD PRESS SYS 1 EICAS CAUTION; HYD QTY LOW EICAS CAUTION, HYD OVHT SYS 1 EICAS, GEAR DOOR CAUTION - BODY GEAR RIGHT DOOR. R & R THE NLG DOOR ACTUATOR PER AMM 32-34-14. OPS & LK CHK GOOD PER AMM 32-34-14. INSTALLED NEW EDP IAW AMM 29-11-05 & IPC 29-11-05-02B.SDR UIEA2025090401160Fmc · faultedONE HOUR, THREE MINUTES INTO FLIGHT, BOTH ND'S HAVE YELLOW MAP FAULT DISPLAYED. NO ROUTE OR MAGENTA LINE SHOWN, EIU SOURCE SEL AND CTR C/B CYCLED. REPLACED LT FMC PER AMM 34-61-01, TESTED GOOD IAW AMM 34-61-00 & IPC 34-61-01.SDR UIEA2025090201151Window · leakingR2 WINDOW HAS HIGH WIND NOISE. THE HIGHER THE AIRCRAFT CLIMBS, THE LOUDER THE NOISE BECOMES(<P>APPLIED FILLER TO LOWER LH AND RH WINDOW FRAME CORNER ON R2 POSITION PER AMM 20-30-01, BOEING TLS 25-0574-02B AND BOEING EID 65B07610 SHEET 5. INSTALLED NEW R2 WINDOSDR UIEA2025080501090Manifold · damagedFLIGHT CREW REPORTED MOMENTARY FIRE WARNING MESSAGE ON EICAS. FOUND DAMAGE TO THE 8TH STAGE MANIFOLD. REPLACED 8TH STAGE MANIFOLD IAW AMM 36-11-01/401 PER 114 & IPC 36-11-05-01B REV 89. PERFORMED NR 2 ENG PNEUMATIC LEAK TEST IAW AMM 71-00-00-705-002-N00. LESDR UIEA2025062500801Connector · damagedPACK 1 EICAS ADVISORY MESSAGE AFTER TAKEOFF. ORH 224 DID NOT CORRECT PACK 1 SELECTED OFF. PACK 1 STATUS AFTER RETURN TO SUU.(<P>REMOVED AND REPLACED RAM INLET DOOR ACTUATOR CONNECTOR IAW B747-400 WDM 21-62-11 ON PACK #1 AND STANDARD WIRING WIRING PRACTICES 20-SDR UIEA2025041400476Display · inoperativeAFTER TAKE OFF AT 400FT AGL, ALL 6 EFIS/EICAS SCREENS BLANK & CDU SCREEN BLANK 5 TO 10 SECONDS, ALL CAME BACK.(<P>PER MCC REQUEST, PERFORMED ENGINE RUNS FOR MIN 20-MIN. RAN ENGINES PER AMM 71-00-00. PERFORMED POWER TRANSFER REF AMM 24-22-00 COULD NOT DUPLICATESDR UIEA2025031400334Bulkhead Web · crackedDURING ACCOMPLISH EO 4453C449_CS LH CLOSEOUT PANEL REPLACEMENT FOUND I/B SIDE CANTED PRESSURE BULKHEAD WEB FASTENER HOLE CRACKED.(<P>WORK ACCOMPLISHED <SPAN>7075T6-0.125" & 7075T6-0.063" </SPAN><SPAN>IAW EN 1014-25 REV 0.</SPAN></P>)SDR UIEA2025031900357Seat Track · corrodedCABIN STA 1000 LBL 33 FOUND SEAT TRACK CORROSION AS MARKED.(<P>CABIN STA 1000 LBL 33 SEAT TRACK REPAIR CARRIED OUT IAW B747-400F SRM 53-00-52 FIG 201 REV 103 AND EN# 1020-25 REV 0. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025031900358Stiffener · corrodedFWD CARGO COMP STIFFENER AT STA 1000 LBL 26 BWL 110 FOUND CORRODED.(<P>WORK ACCOMPLISHED IAW EN# 1021-25 REV 0. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025031900359Longeron · crackedDURING HFEC INSPECTION, FOUND CRACK AT LONGERON EXTENSION FITTING STA 1480 LHS & RHS APPROX CRACK LENGTH = 0.6" RHS AND 0.4" LHS AS MARKED.(<P>WORK ACCOMPLISHED IAW EN# 1018-25 REV 0. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025031900360Support Fitting · obstructedDURING ACCOMPLISH EO 4454A215_CS NACELLE STRUT PW4000 NO.1 & NO.4 OUTER SPRING BEAM SUPPORT FTG. WHILE LOCATE FILLE P/N: 321U2400-5602 AT FASTENER CODE A LOCATION. FOUND TOO CLOSE TO EXISTING BULKHEAD.(<P>WORK ACCOMPLISHED IAW EN# 1013-25 REV 0. NO FURTHER DEFSDR UIEA2025031900362Rub Strip · obstructedDURING PERFORMING LH AND RH RUB STRIP INSTALLATION PER SB 747-53A2721R3/ AD 2013-26-12, FOUND AFT RUB STRIPS INTERFERING WITH EXISTING PROTUDING HEAD FASTENERS ON FUSELAGE SKIN AT BS2517 TO 2628 LH AND RH(<P>WORK ACCOMPLISHED IAW EN# 1019-25 REV 0. NO FURTHER SDR UIEA2024113001138Window · damagedRH UPPER DECK CTR SIDE WINDOW DAMAGED(<P>R/R WINDOW IAW AMM 56-21-01. OPS & LEAK CHK OK.</P>)SDR UIEA2024081500831Skin · dentedDENT AT RH WING FLAP LOWER SURFACE 58" FROM INBD END(<P>INSTALLED FABRICATED DOUBLER AT RH WING FLAP LOWER SURFACE 58" FROM INBD END AND 27" FROM LOWER T/E IAW SRM 51-70-10-2R-0. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024081500830Skin · dentedSEVERAL DENTS AT LH WING INBD MID FLAP LOWER SURFACE(<P>INSTALLED, FABRICATED DOUBLER ON LH WING MID FLAP IAW SRM 51-70-10-212-0 PAR 20B TABLE 208. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024081600835Rub Strip · gougedLH WING #5 SPOILER LOWER SKIN T/E RUB STRIP GOUGED(<P>ACCOMPLISHED PERMANENT REPAIR ON #5 SPOILER LOWER SKIN IAW B747 SRM 51-70-10-2R & 57-70-02-2R-1. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024080400787Actuator · faultedEICAS MSG "GEAR TILT" ON TAKE-OFF. REPLACED RH BODY GEAR TILT ACTUATOR AND RH BODY GEAR TRUCK POSITIONING FUSE AND OPS CHECKS NORMAL PER AMM 32-13-15, 32-13-24, 32-32-00, 32-34-00 AND IPC 32-13-15-02A.SDR UIEA2024080200775Actuator · no testDURING BLG ALTERNATE EXTENSION TEST, FOUND R/H BLG ROTARY ACTUATOR FUNCTION FAIL. IAW AMM 32-35-01-004-001 REV 110 AND AMM 32-35-01-404-007 REV 110 R/R RH BLG ROTARY ACTUATOR. 2. IAW AMM 32-35-00-715-059 REV 110 PFM OPERATION TEST, TEST RESULT WAS SATISFACTOSDR UIEA2024080200774Seat Track · crackedCRACK - FOUND M/D SEAT TRACK CRACK AT STA 1700 AND STA 1760, LBL 11.33.</SPAN></SPAN>(<P>1. REMOVED AFFECTED FASTERNERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 101 2. REPAIR DAMAGE AREA IAW EI NO: T2024A53M-1802 REV 1 3. INSTALLED FASTERNERS IAW SRM 51-40-02-0SDR UIEA2024080200773Seat Track · crackedFOUND M/D STA 1860, RBL 98.58 SEAT TRACK CROWN CRACK. REMOVED AFFECTED FASTERNERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 101 2. REPAIR DAMAGE AREA IAW W/S #40566 (SRM 53-00-52-2R-6 REV=101) AND EI T2024A53M-1791 REV 1. 3. INSTALLED FASTERNERS IAW SRM 51-40-0SDR UIEA2024080200772Cargo Track · crackedCRACK - FOUND TRACK - SUBSTITUTE WAS CRACK AT M/D STA 1700, LBL 75.(<P>1. REMOVED AFFECTED FASTERNERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 101 2. REPAIR DAMAGE AREA IAW W/S #40562 (SRM 52-00-52-2R-13 REV 101) 3. INSTALLED FASTERNERS IAW SRM 51-40-02-0G-0 RESDR UIEA2024080200771Cargo Track · crackedCRACK - FOUND TRACK - SUBSTITUTE WAS CRACK AT M/D BETWEEN STA 980 ~ STA 1000, LBL 75.(<P>1. REMOVED AFFECTED FASTERNERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 101 2. REPAIR DAMAGE AREA IAW W/S #40561 (SRM 53-00-52-2R-13 REV 101) 3. INSTALLED FASTERNERS IAW SRSDR UIEA2024080200770Cargo Track · crackedCRACK - FOUND M/D TRACK - SUBSTITUTE CRACK AT STA 995 RBL 75.92.(<P>1. REPAIR DAMAGE AREA IAW W/S #40565 (SRM 53-00-52-2R-13 REV 101) 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2024080200769Tension Tie · crackedCRACK - PERFORM OPEN HOLE INSPECTION FOUND TENSION TIE HAS CRACK AT R/H STA 760. PERFORM EO 4453A301 PART 1-2 REV 12. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR UIEA2024080200768Tension Tie · crackedCRACK - PERFORM OPEN HOLE INSPECTION FOUND TENSION TIE HAS CRACK AT L/H STA 740. PERFORM EO 4453A301 PART 1-2 REV 12. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR UIEA2024080200767Tension Tie · crackedCRACK - PERFORM OPEN HOLE INSPECTION FOUND TENSION TIE HAS CRACK AT L/H STA 720. PERFORM EO 4453A301 PART 1-2 REV 12. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR KCSA202205161052Fitting · corrodedLH INBOARD ELEVATOR ACTUATOR O/B FITTING HAS EVIDENCE OF CORROSION.SDR KCSA11021Engine · leakingSMOKE IN FLT DECK & CABIN DURING CRUISE. DECLARED EMERGENCY AND DIVERTED TO EDDF. PERFORMED FIM TASK 21-00 TASK 810 & 71-03 TASK 854. FOUND OIL (ENG) IN TAIL PIPE. REMOVED & REPLACED THE NR 4 ENG IAW B747-400 MM 71-00-02, PERFORMED ENG TEST NR 7 IAW B747-4
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