Boeing 747-400
Service difficulty reports · 275
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 = '747400' 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 = '747400' 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 IPXA2016112611003Battery Pack · dischargedFOUND LT EMERGENCY BATTERY PWR SUPPLY INOP. R&R LT POWER SUPPLY BATTERY PACK AS PER AMM 33-51-04/201. OPS TEST NORM P/N ON OFF :9008-3-5AB S/N ON/OFF 50596/50688 IPC 33-51-04-21SDR UIEA2016112800906Actuator · failedFND RH WING LANDING GEAR ALTERNATE MOTOR FUNCTION FAIL. REPLACED THE RT WING ALT ELECTRIC ACTUATOR IAW AMM 32-36-01-004-001 REV 87 AND AMM 32-36-01-404-009 REV 87. CONDITION CHECK NORMAL.SDR UIEA2016112200850Feeder Cable · chafedFOUND POWER FEEDER CABLE W5022-013-00 CHAFING WITH CEILING SCREW AT FWD CARGO. REPAIRED THE FEEDER CABLE IAW SWPM 20-30-14, 20-30-13 REV63 AND WDM 24-21-11 REV19 AND CONDITION CHECKED NORMAL. PERFORMED ECU STATIC TEST AND THE RESULT WAS SATISFACTORY IAW ASDR SAJF2016110205021Plate · corrodedDURING MAINTENANCE CHECK, CORROSION WAS FOUND AT FUSELAGE LONGERON PLATE LOCATED ON STA 2362 S-23R. THIS AREA ORIGINAL INSP PLAN WAS FOLLOW 53-916-01. THE BLEND OUT SIZE IS 5" X 2.5" WITH MINIMUM REMAINING THICKNESS 0.049". FUSELAGE LONGERON PLATE LOCATED OSDR IPXA2016101709514Floor Panel · damagedINSPECTION TYPE:N/A, FLOOR PANEL AT STA 1236 AND RBL 91 HAS HOLE. 1" HOLE DAMAGE TO BOTH SKINS. REPAIR PER SRM 53-00-50-2R.SDR 2016F00180Starter · damagedAIRCRAFT WAS BEING PREPARED FOR DEPARTURE. APU WAS STARTED AND APPROXIMATELY 5 MINUTES LATER, THE APU FIRE INDICATION ACTIVATED AND THE FLIGHT CREW PULLED THE APU FIRE
T-HANDLE. THE APU FIRE BOTTLE HAD ALREADY AUTOMATICALLY ACTIVATED. UPON INSPECTION OF THSDR WRNA2016F00149Controller · inoperativeDURING CRUISE, UPPER CABIN AND ALL DECKS TEMPERATURE EXCEEDED 60 DEGREES C. RETURNED TO DEPARTURE. EMERGENCY NOT DECLARED. TROUBLESHOOTING FOUND A DEFECTIVE ZONE TEMPERATURE CONTROLLER. CONTROLLER WAS REMOVED AND REPLACED, OPERATIONAL SYSTEM CHECK SATISFACSDR IPXA2016060204156Skin · damagedDAMAGE TO AFT LOWER CARGO DOOR SKIN, FWD LOWER CORNER REPAIR IAW EO B747-5230-60772-B.SDR IPXA2016051403344Lens · brokenFOUND EMERGENCY LIGHT LENS WAS BROKEN AT FLT DECK. REPLACED DOME LIGHT LENS IAW MM 33-51-07. PERFORMED OPS TEST OF EMERGENCY LIGHTS. OPS CHECKED GOOD IAW MM 33-51-07, STEP E.SDR IPXA2016042602638Attach Fitting · crackedRT WING LOWER AFT PANEL ATTACH FITTING CRACKED BS 515 FABRICATED NEW FITTING IAW DWG 65B08016, EO B747-5750-60589-A, REF PO SP1969419.SDR IPXA2015112796170Battery Pack · inoperativeEMERGENCY LIGHT INOPERATIVE. R & R THE BATTERY IAW AMM 33-51-04 & SSM 33-51-01.SDR BJNA20151125001Window · crackedENROUTE, ON CLIMBOUT- APPROXIMATELY FL220, F/O'S WINDOW CRACKED, SHATTERED. OPS IAW QRH, OK TO CONTINUE LAND W/NO FUTURE ISSUE. REMOVED NR 1 WINDOW IAW AMM 56-11-11. INSPECTED WINDOW FRAME AND HARDWARE AS REQUIRED. INSTALLED F/O WINDOW IAW AMM 56-11-11. PESDR WRNA201510290031Engine · shutdownNR 1 ENGINE LOST POWER, ALL OF ITS PARAMETERS DISPLAYED IDLE ON ECIAS. POWER RECOVERED IMMEDIATELY. MINUTES LATER SAME ENGINE LOST POWER AGAIN DURING CLIMB OUT. ALL ENGINE PARAMETERS DISPLAYED IDLE ON ECIAS BUT THIS TIME POWER WAS NOT RECOVERED. ENGINE CHECSDR SAJF20151014018Ballast · inoperativeZONE A CEILING LIGHTS INOPERATIVE. FOUND P414 H17 CB POPPED OUT. PFM WIRING CHECKED & FOUND SEAT 3A CEILING LIGHT BALLAST M8468, PLUG & WIRING DAMAGED. AFFECTED BALLAST M8468 DAMAGED PLUG & WIRES HAS INSOLATED. THE P414 H17 CB RESET NORMAL, ZONE AN AREA CESDR IPXA2015091893655Transmitter · malfunctionedNR 3 ENGINE OIL STATUS MESSAGE ANNUNCIATED AT CRUISE. NR 3 ENGINE OIL QTY IN MAGENTA AT 7 QTS, NR 3 ENG OIL CONTINUED TO DECREASE TO 1 QT AFTER APPROXIMATELY 1.6 HRS OF OPERATION. PRECAUTIONARY SHUTDOWN OF NR 3 ENGINE ACCOMPLISHED1. REPLACED PACKING AT AGB SDR IPXA2015091193397Evas Unit · inoperativeCAPTAIN`S EVAS FAILED ON OPS TEST. R & R CAPTAIN`S EVAS IAW 25-60-00-001, ITEM 7. OPS TESTED SATISFACTORY,SDR SAJF2015091104043Gearbox · failedON SEPT 10 2015 B-18202 FLIGHT 062, INFLIGHT AROUND 9 HOURS, CREW FOUND ENG 3 OIL SUDDENLY DROPPED TO 0, OIL TEMP MAX 210 DEGREE C, & OIL QTY RETURNED TO 21 AT 02:54 10. FOLLOWING QRH, CREW PERFORMED ENG 3 IFSD. AIRCRAFT ARRIVED UNEVENTFUL AT 06:31. EC 2 INISDR IPXA2015083192904Floor Panel · gougedMAIN CARGO DECK FLOOR PANEL HAS TWO GOUGES THRU FACE SHEET INTO CORE. FABRICATED A NEW FLOOR PANEL IAW EO B747-5320-58442-A.SDR IPXA2015082992862Skin · dentedRIGHT WING INBD AFT FLAP LOWER SKIN DENTED. REPAIRED IAW EO B747-5750-57795-B.SDR IPXA2015082492647Floor Panel · crackedINSPECTION TYPE: C, MCD FLOOR PANEL BS 780 CRACKED. REPAIRED IAW SRM 53-00-50-2R-1, REV 74, REPAIR CLASSIFIED AS MAJOR.SDR IPXA2015062990630Handle · missingACCESS DOOR TO EMERGENCY SLIDE HANDLE MISSING ON RT UPPER DECK. REPLACED MISSING COVER IAW MM 52-23-02.SDR IPXA2015051789152Floor Panel · puncturedMAIN CARGO DECK FLOOR PANEL PUNCTURED ON UPPER FACE SHEET. FABRICATED A NEW FLOOR PANEL IAW EO B747-5320-57485-A.SDR IPXA2015051789149Floor Panel · damagedMCD FLOOR PANEL DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B747-5320-57483-A.SDR IPXA2015051789148Floor Panel · crushedMCD FLOOR PANEL HAS CRUSHED SKIN AND CORE AT EDGE. FABRICATED A NEW FLOOR PANEL IAW EO B747-5320-57482-A.SDR IPXA2015032687436Engine · leakingNR 2 ENGINE LEAKING OIL DURING CRUISE. CREW DETERMINED NR 2 ENG LOSING 1 QT OIL EVERY 30 MINS. R & R NR 2 ENGINE IAW TC 71-000-00-01. OPS & LEAK CHECKED GOOD.SDR IPXA2015020685585Skin · delaminatedINSPECTION TYPE:C, LT INBD ELEVATOR UPPER SURFACE DELAMINATED FIBERGLASS PREPREG LAY UP, REPAIR PERFORMED IAW SRM 51-70-07, PAR 5A, 1, FIG 5, REV 71.SDR WRNA20150029Radar · malfunctionedAFTER TAKEOFF ALL SYSTEMS WERE NORMAL. ONCE A RT TURN HEADING 120 DEGREES WAS INITIATED, THE CREW RECEIVED A "RADAR FAIL" MESSAGE WHILE IN THE TURN. AFTER A CLIMB OF 10,000 FT, THE CREW WAS UNSUCCESSFUL IN FIXING THE PROBLEM. AFTER DISCUSSING THE DUAL RADAR SDR IPXA2014112484924Floor Panel · damagedSMALL HOLE IN FLOOR PANEL APPROXIMATELY BS 1453, LBL 20. REPAIRED IAW SRM 53-00-50-2R (4C).SDR IPXA2014092684437Battery Pack · inoperativeINSPECTION D, UPPER DECK EMERGENCY LIGHTS POWER SUPPLY FOUND INOPERATIVE. BATTERY PACK REPLACED, LIGHTS TESTED NORMAL.SDR WRNA201409040022Wire · chafedTHE CREW REPORTED THAT AFTER TAKEOFF, ATTEMPTED TO RAISE THE GEAR AND AN EICAS MESSAGE "GEAR TILT" DISPLAYED. FOLLOWED THE QRH PROCEDURES, LANDED WITHOUT ANY FURTHER INCIDENT. REPAIRED CHAFED WIRE AT LT WING LANDING GEAR JUNCTION BOX. OPS CHECKED NORMAL.SDR IPXA2014050582863Skin · damagedLEFT INBD MID FLAP COVE ARE LOWER SKIN DAMAGED. REPAIRED IAW EO B747-5750-54256-A.SDR IPXA2014031782303Floor Panel · damagedBS 1990 FLOOR PANEL HAS A HOLER. FABRICATED NEW FLOOR PANEL IAW EO B747-5320-52750-A.SDR IPXA2014032182375Splice Plate · crackedINSPECTION C, BS 400, S44R, A .5 INCH DIA HOLE FOUND ON BS 400 BULKHEAD FRAME LOWER ATTACH SPLICE PLATE. SPLICE PLATE REPLACED IAW RI-53-11-10489, REV A & EO B747-5330-53796-A.SDR SAJF2014031103002Slide · malfunctionedB-18710 WHEN PERFORMED 12Y SLIDE DEPLOYMENT TEST ON RT DOOR IN UD OF B-18710 ON 02/07/2014, FOUND THE DEPLOYMENT OF THE SLIDE ASSEMBLY WAS ABNORMAL. IN THE INITIAL PERIOD OF DEPLOYMENT, THE FUNCTION OF SLIDE WAS SMOOTH, HOWEVER, WHEN SLIDE CONTINUED TO MIDDLESDR IPXA2014020581778Channel · damagedINSPECTION C, LT WING REFUELING PANEL 521CB INBD LATCH ATTACH CHANNEL FOUND CORRODED & CRACKED. LATCH ATTACH CHANNEL REPLACED IAW SRM 51-10-02 AND 51-40-02, REV 27.SDR SAJF201401103001Slide · defectiveB-18709 THE UD SLIDE FAILED TO DEPLOY DURING ROUTINE TEST IAW AMP 52-023-01 ON 01/01/2014. THE SLIDE STUCK IN MIDDLE TRAVEL ROUTE AROUND 180 DEGREES & NO MORE MOVING. FINALLY, CHI STAFF PULL T HANDLE TO MANUAL RELEASE THE SLIDE & INFLATION SUCCESSFULLY WITHISDR SAJF201401102031Engine · overspeedB-18205 CREW INFORMED DURING SPEED RECOVERY ENG 1/2/3 N2 & ENG 4 N1 OVER SPEED WERE RECORDED. CHECK ENG EXCEEDED REPORT FOUND ENGINE 1 N2 MAX 105.6 LASTING 7 SEC, ENG 2 N2 MAX 105.6 LASTING 3 SEC, ENG 3 N2 MAX 105.6 LASTING 7 SEC, ENG 4 N1 MAX 111.5 LASTING 2SDR UIEA2013112500570Shutoff Valve · inoperativeEICAS MESSAGE BLEED 4, NACELLE ANTI-ICE INOPERATIVE. REPLACED NR 4 HPSOV, OPS CHECKS NORMAL.SDR UIEA2013100700511Battery Pack · inoperativeEMERGENCY BATTERY PACK, AT BS 717 INOPERATIVE. R & R BATTERY. OPS CHECKED GOOD IAW AMM 33-51-04-902-001-001.SDR SAJF201311102028Float Valve · obstructedAIRCRAFT GND TURN BACK DUE TO FUEL LEAK FROM RT WING SURGE TANK VENT PORT. THE FLOATING VLV IN MAIN TANK FAILED TO CLOSE, RESULTING FUEL OVERFLOW TO SURGE TANK THROUGH VENTING SYS & SPILL OUT FROM SURGE TANK VENT PORT. APPLIED MEL 28-15-02-02C TO DEACTIVATE SDR IPXA2015032700495Shear Tie · damagedFUSELAGE FRAME SHEAR TIE DAMAGE BETWEEN STA 2140 & STA 2120 AND S-50C AND S-50R SUPPLEMENTAL: REPAIRED IAW EO B747-5330-51511.SDR IPXA201307229437Skin · puncturedRIGHT WING INBD FLAP LOWER T/E PUNCTURE DAMAGED. REPAIRED IAW EO B747-5750-51514-A.SDR IPXA201307229433Skin · puncturedRT INBD MID FLAP LWR SURFACE PUNCTURE 1.4" FROM INBD EDGE. REPAIRED IAW EO B747-5750-51513-A.SDR SAJFCALS102023Actuator · malfunctionedB-18720 INITIAL INVESTIGATION R & R LT BODY LANDING GEAR, BLG WW DOOR STRUCTURAL, RETRACTING ACTUATOR, HYD TUBE. REPLACED DOWNLOCK SEQ VLV, DOOR SEQ VLV, UPLOCK SEQ VLV, DOWNLOCK ACTUATOR & DOWNLOCK BUNGEE FOR ISOLATING OF THE POSSIBLE RO?2 DOWNLOCK ACTUATOR SDR IPXA13B78726Wedge · puncturedINSPECTION TYPE:3C, RT WING INBD FOREFLAP T/E WEDGE LOWER SURFACE FOUND PUNCTURE COMPOSITE HOT BOND REPAIR CARRIED IAW SRM 51-70-07, PAR 5A(1), FIG 5, REV 66.SDR IPXA13B77023Skin · dentedLEFT OTBD AFT FLAP UPPER SURFACE DENT, REF EO B747-5750-48519-B FOR REPAIR.SDR IPXA13B77013Skin · dentedRT OTBD AILERON DENTED .5 DIA 24 INCHES FROM INBD EDGE AND 24 INCHES FROM T/E. REPAIRED IAW EO B747-5750-49752-A.SDR IPXA12B75817Floor Panel · damagedMAIN DECK FLOOR PANEL HAS 1 INCH DIA HOLE TO THE TOP SURFACE PAN. REPAIRED REF SRM 53-00 50 2R-1, PAR4C.SDR IPXA2B75268Channel · crackedINSPECTION TYPE: D, MAIN DECK BS 740 TENSION TIE FWD CHANNEL TWO HOLES FOUND CRACKED. REPAIRED IAW SRM 53-20-30-2R REPAIR 1 REV 63, HX RS R-53-25-37443-A & EO B747-5310-48484-A, ORIG MATL: BAC1494-206-2024T42, CLASSIFIED AS A MAJOR REPAIR, ACCOMPLISH INITSDR IPXA12B74522Bulb · burned outINSPECTION TYPE: PS, EMERGENCY EXIT LIGHT ON CEILING OF MAIN CARGO DECK JUST FWD OF STAIRS INOPERATIVE. RELAMPED IAW AMM 33-51-07-962-001. OPS CHECKED GOOD.
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