Boeing 747-341
Service difficulty reports · 174
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 = '747341' 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 = '747341' 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 UIEA201000048Beam · crackedFUSELAGE - BS 570-580, RBL 25 LONGITUDINAL BEAM CRACK REPAIR SRM 53-10-05 FIG 5. REPEAT REQ: PERMANENT.SDR UIEA201000052Skin · dentedFUSELAGE - BS 700 - 720, S46-47R SKIN DENT REPAIR 8100-9 SRM 51-40-03 OR 51-40-04, SRM 53-10-21, FIG 25, DETAIL XII. REPEAT REQ: 2ND STAGE 22,000 TFC.SDR UIEA201000050Skin · corrodedFUSELAGE - BS 1960-2180, S46L LAP JOINT SKIN CORROSION REPAIR SRM 53-10-01 FIG 1, DETAILS I AND II. REPEAT REQ: PERMANENT.SDR UIEA201000047Stringer · corrodedFUSELAGE - BS 760, S47R STRINGER CORROSION REPAIR SRM 53-10-03 FIG 1, REPEAT REQ: 1-20,000TFC R-6,000 FC.SDR UIEA201000046Frame · crackedFUSELAGE - BS 1540, S5;-S6L FRAME CRACK REPAIR. 8100-9 SRM 53-10-04 FIG 1, 2ND STAGE 25,000 TFC.SDR UIEA201000045Skin · crackedFUSELAGE - BS 1860-1880, S-41-42L SKIN CRACK REPAIR. REPAIRED PER SRM 53-30-00 FIG 1, DETAIL 1. REPEAT REQUIREMENT: PERMANENT.SDR UIEA201000044Skin · crackedFUSELAGE - BS 780-800, S-46L SKIN CRACK. REPAIRED PER SRM 53-30-00, FIG 1, DETAIL 1. REPEAT REQUIREMENT: PERMANENT.SDR UIEA201000043Door · damagedDOOR - RT BODY GEAR DOOR DAMAGE. REPAIRED PER SRM 52-80-01, FIG 3, SH 6 ITEM 3, SRM 51-40-02, SRM 51-40-03. REPEAT REQUIREMENT: PERMANENT.SDR UIEA201000042Doubler · damagedDOOR - AFT CARGO DOOR LWR AFT AND FWD CORNER DOUBLER. REPAIRED PER 8110-9 SRM 52-30-06, FIG 1, DET III. REPEAT REQUIREMENT: 1ST STAGE APPROVAL.SDR Q2SA789003Unknown · odorDURING DESCENT INTO PAED EQUIPMENT COOLING SMOKE LIGHT ILLUMINATED FOR ABOUT 10 SECONDS WHEN PASSING FL230 AND FOR ABOUT 5 SECONDS WHEN PASSING 14000FT. CREW SMELLED FUMES BUT DID NOT NOTICE ANY VISIBLE SIGN OF SMOKE. CREW CONTINUED NORMAL DESCENT AND LANDEDSDR Q2SA789002Vent · obstructedON DESCENT INTO KORD CREW SMELLED SMOKE IN THE COCKPIT AND EQUIPMENT COOLING "SMOKE" LIGHT CAME ON FIVE MINUTES AFTER SMOKE ODOR STARTED. EQUIPMENT COOLING SYSTEM PREVIOUSLY ENTERED ON DMI PER MEL 21-33. CREW CONTINUED DESCENT AND LANDED SAFELY. UPON INVESTSDR UIEA200900056Panel · delaminatedRT WING FIXED UPPER L/E PANEL AT ILES 700.72 AND 30.0 INCHES FROM FRONT OF PANEL HAS AN AREA OF A PREVIOUS REPAIR 22.00 BY 15.0 INCHES OF DELAMINATION. PERMANENT REPAIR ACCOMPLISHED IAW SRM 51-40-09 SHEET 2 AND 5, PREPREG 250 DEGREES F CURE IAW SRM 51-40-12.SDR UIEA200900055Beam · severedNR 4 PYLON LT SPRING BEAM FORWARD JOURNAL END SEVERED. NR 4 ENGINE REMOVED FOR FERRY FLIGHT TO ROW. ALL REQUIRED INSPECTIONS ACCOMPLISHED. AS PER RECOMMENDATIONS AS PER SB 747-54A2214 AND SB 747-54A2182.SDR UIEA200900001Apu · leakingON TAXI IN APU OIL CONSUMPTION WAS HIGH AND THERE WAS A STRONG ODOR OF OIL WHEN USING THE APU. THE APU WAS PLACED ON MEL DEACTIVATED PER 49-01.SDR Q2SA789001Compressor · stalledEN ROUTE FROM SPIM TO KMIA DURING CLIMB AND CRUISE, NR 2 ENGINE EXPERIENCED HIGHER EGT READING (70 DEG) THAN OTHER ENGINES. REDUCED THRUST SETTINGS ON NR 2 ENGINE LOWERED HIGHER EGT READING TO 30 DEG ABOVE OTHER ENGINES, WITH NO ROUGHNESS OR APPARENT ENGINE ISDR UIE2008F00037Relief Valve · failedAIR TURN BACK. DURING CLIMB AT APPROX FL 230, NR 3 ENGINE FIRE HANDLE ILLUMINATED. ACCOMPLISHED FHB ENGINE FIRE PROCEDURES. LIGHT EXTINGUISHED AFTER THRUST LEVER SET TO IDLE. INCREASE IN NACELLE TEMP INSPECTION CARRIED OUT IAW AMM. FOUND PRESSURE RELIEF AT FAUSDR UIEA200800298Panel · crackedRT WING FORWARD LEADING EDGE PANEL HAS A 2.5" CRACK LOCATED AT ILES 208.81 AND IS 18.25" FROM TOP EDGE OF PANEL. PERMANENT REPAIR ACCOMPLISHED AS PER B747-300 SRM 57-30-04 FIG. 2, SHEETS 1,2 & 3. ALSO, REFERENCE ATLAS AIR EO NO. 4757A459.SDR UIE2008F00028Panel · crackedR/H WING UPPER SURFACE LEADING EDGE PANEL HAS A 3" CRACK LOCATED AT ILES 818.5 AND 9" FROM LEADING EDGE OF PANEL. ALSO, REFERENCE ATLAS AIR EO NO. 4757A458. UIEA200800297.SDR UIEA200800090Beam · corrodedFORWARD CARGO DOOR INNER WEB LOWER BEAM FOUND SURFACE LEVEL ONE CORROSION AT RT STATION 560-670 STRINGER 40R. CLEANED CORROSION PER SRM 51-30-02 AND BOEING DRAWING 65B04697.SDR UIEA200800089Beam · corrodedAFT CARGO DOOR INNER WEB LOWER BEAM FOUND SURFACE LEVEL ONE CORROSION AT RT STATION 1810-1920 STRINGER 40R. LOWER BEAM WEB REMOVED AND REPLACED AS PER SRM 51-30-02 AND BOEING DRAWING 65B04719.SDR UIEA200800088Bushing · crackedNOSE LANDING GEAR TRUNNION FITTING LEFT SIDE BUSHING CRACKED. REPLACED BUSHING IAW ATLAS EO 4753B122.SDR UIEA200800087Bushing · wornNOSE LANDING GEAR TRUNNION FITTING RIGHT SIDE BUSHING WORN. REPLACED BUSHING IAW ATLAS EO 4753B122.SDR UIEA200800086Seat Track · corrodedMAIN DECK STA 1720 TO 1740 RBL 11 SEAT TRACK FOUND LEVEL 1 CORROSION. CORROSION REMOVED IAW SRM 51-10-01.
SDR UIEA200800078Structure · crackedNR 11 KRUEGER FLAP OUTBOARD END INNER FACE CRACKED. DAMAGE TRIMMED OFF AND REPAIR CARRIED OUT WITH FIBERGLASS AS PER SRM 51-40-14 PARA 4H.
SDR UIEA200800077Seat Track · corrodedMAIN DECK STA 2040 TO 2060 LBL 90 SEAT TRACK HAS CORROSION. SEAT TRACK REPAIRED PER SRM 53-10-05 FIG 1A.SDR UIEA200800076Seat Track · brokenMAIN DECK STA 1840 TO 1900 LBL 11 SEAT TRACK FOUND BROKEN. SEAT TRACK REPAIRED PER SRM 53-10-05.SDR UIEA200800075Structure · corrodedMAIN DECK STA 1680 TO 1700 RBL 11 BEAM UPPER CHORD HAS LEVEL 1 CORROSION. CORROSION REMOVED AND TREATED IAW SRM 51-10-01.SDR UIEA200800074Seat Track · corrodedMAIN DECK STA 1680 TO 1700 RBL 11 SEAT TRACK HAS LEVEL 1 CORROSION. CORROSION REMOVED AND TREATED IAW SRM 51-10-01.SDR UIEA200800073Floorbeam · crackedMAIN DECK STA 2020 RBL 62 FLOORBEAM CRACKED. REPLACED FLOORBEAM LOWER SUPPORT FITTING IAW SRM 51-10-01.SDR UIEA200800072Seat Track · corrodedMAIN DECK STA 1640 TO 1690 LBL 33 SEAT TRACK HAS LEVEL 1 CORROSION. CORROSION REMOVED AND TREATED IAW SRM 51-10-01.SDR UIEA200800070Seat Track · corrodedMAIN DECK STA 1700 LBL 75 SEAT TRACK HAS LEVEL 1 CORROSION. CORROSION REMOVED AND TREATED IAW SRM 51-10-01.SDR UIEA200800084Door Frame · crackedMAIN DECK L5 DOOR CUTOUT FWD UPPER REVEAL PANEL FOUND CRACKED. REPAIRED PER SRM 53-10-04.SDR UIEA200800083Frame · crackedMAIN DECK L4 DOOR AFT LOWER CORNER FRAME CRACKED. CRACKED AREA REPAIRED PER SRM 52-10-02.SDR UIEA200800080Skin · corrodedLEFT WING UPPER SKIN REAR SPAR CORRODED LEVEL 1. CORROSION CLEANED UP AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.SDR UIEA200800079Structure · crackedNR 6 SPOILER LOWER FACE DOUBLER CRACKED NEAR ACTUATOR FITTING. DAMAGED SPOILER REMOVED AND REPLACED WITH SERVICEABLE SPOILER IAW AMM 27-62-01.SDR UIEA200800082Spar · corrodedRIGHT WING STA 610 TO WING STA 615 UPPER FACE REAR SPAR LEVEL 1 CORROSION EVIDENT. CORROSION CLEANED UP AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.SDR UIEA200800081Stringer · crackedCABIN AND FLIGHT DECK UPPER DECK STA 480 STRINGER S-10 R FOUND CRACKED. REPAIRED STRINGER PER BOEING SERVICE BULLETIN 747-53A2484.SDR UIEA200800007Unknown · unknownDURING CLIMB WITH AUTOTHROTTLES ENGAGED AND CLIMB THRUST SET AT APPROX FL10.5 NR 4 ENGINE ROLLED BACK TO IDLE THRUST AFTER ABOUT 10 SECONDS NR 4 ENGINE RETURNED TO CLIMB THRUST. THE THRUST LEVER NEVER MOVED. THE ENGINE OPERATED NORMAL FOR THE REMAINDER OF THSDR UIEA200700500Tension Tie · crackedTENSION TIE LOCATED AT FUSELAGE STATION 1220 LT SIDE AT STRINGER 9 LOCATION HAS A CRACK. INTERIM REPAIR ACCOMPLISHED AS PER B747-300 SRM 53-10-11, FIG 1 AND BOEING MESSAGE NUMBER 1-711332103-6 AND FORM 8100-9. ALSO, REFERENCE ATLAS AIR XEO NO. 53-121307.SDR UIEA200700502Frame · crackedFRAME AT STATION 1140 RT HAS A CRACK AT STRINGER 10 AND 10A LOCATION. CRACK AT STR 10A 0.500 INCH LONG AND STR 10 IS 0.750 IN LONG. PERMANENT REPAIR ACCOMPLISHED AS PER B747-300 SRM 53-10-04 FIG 123 AND BOEING MESSAGE NUMBER 1-711332103-6 AND FAA FORM 8100-9SDR UIEA200700501Frame · crackedFRAME AT STATION 1140 LT HAS A CRACK AT STRINGER 10 AND 10A LOCATION. CRACK AT STR 10A 0.875 INCH LONG AND STR 10 IS 0.760 INCH LONG. PERMANENT REPAIR ACCOMPLISHED AS PER B747-300 SRM 53-10-04 FIG 123 AND BOEING MESSAGE NUMBER 1-711332103-6 AND FAA FORM 8100SDR UIEA200700489Structure · crackedLT WING GEAR INBOARD STRUT DOOR HAS FORWARD EDGE COMPOSITE CRACK. PERMANENT REPAIR ACCOMPLISHED AS PER B747-300 SRM 51-40-09, FIG 12, SHEETS 1, 2 AND 3.SDR UIEA200700325Skin · delaminatedON WALKAROUND AFTER FLIGHT OF GT5421, FOUND NR 11 L/E DEVISE DELAMINATED AT AFT I/B CORNER. PERFORMED INTERIM REPAIR PER XEO57-082707. REPETITIVE INSPECTIONS FOR CONDITION AND SECURITY TO BE ACCOMPLISHED EVERY OTHER FLIGHT CYCLE UNTIL PERMANENT REPAIR OR PARSDR UIEA200700312Starter · failedBLOCK TURN BACK, NR 2 ENGINE STARTER WOULD NOT GIVE INDICATION OF ROTATION. THE PYLON BLEED VALVE AND STARTER VALVE LIGHT WERE ON. REPLACED STARTER, OPS CHECKED OKAY.SDR UIEA200700273Door · delaminatedMATERIAL SEPARATING ON FORWARD EDGE OF LT WING GEAR INBOARD DOOR. AREA IS 15.0 INCH LONG BY 1.0 INCH WIDE. PERMANENT REPAIR ACCOMPLISHED AS PER B747-300 SRM 51-40-09, FIG 12, SHEETS 1, 2, AND 3, TABLE II, 250*F CURE AND SRM 51-40-12, REFERENCE ATLAS AIR XEO SDR UIEA200700274Fairing · crackedRT WING GEAR INBOARD STRUT DOOR FAIRING HAS A COMPOSITE CRACK AT AFT SIDE TOP SKIN AND CHAFE STRIP DAMAGED. PERMANENT REPAIR ACCOMPLISHED AS PER B747-300 SRM 51-40-09, FIG 12, SHEETS 1, 2, AND 3, TABLE I, 250*F CURE AND SRM 51-40-12, CHAFE STRIP REPLACED AS PSDR UIEA200700231Fire Warning · false activationAPU FIRE LIGHT AND BELL IN FLIGHT. COMPLIED WITH FHB SECTION 3. INSPECTED APU NIL FAULTS FOUND. REMOVED AND REPLACED FIRE BOTTLE AND SQUIB ASSY PER AMM 26-22-01 SQUIB TEST OKAY.SDR UIEA20070067Skin · corrodedRIGHT WING LOWER SKIN FOUND WITH CORROSION JUST INBOARD OF OUTBOARD MIDSPAR FUSE PIN FITTING OF NR 4 PYLON. CORROSION ON SAID WING LOWER SKIN REMOVED PER SRM 51-10-00. HFEC ACCOMPLISHED, NO DEFECTS. SKIN SHOT PEENED AND REPROTECTED.SDR UIEA200700045Stringer · crackedSTRINGER FOUND CRACKED AT STATION 500 STR 10L. STRINGER AT STATION 500 STRINGER 10L REPAIRED PER SB 747-53A2484 FIGURE 20 AND DEVIATION PER 8100-9.SDR UIEA200700064Flap Track · gougedNR 5 FLAP TRACK FORWARD FITTING OUTBOARD SURFACE FOUND WITH GOUGE. REPAIRED GOUGED AREA, BLENDED AND SMOOTHED PER SRM 51-10-00. DETAIL VISUAL AND HFEC INSPECTED. FOUND NO DEFECTS. AREA PROTECTED AND PAINTED. FOUND WITHIN SERVICEABLE LIMITS.
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