Boeing 747-47UF
Service difficulty reports · 3,116
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 = '74747UF' 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 = '74747UF' 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 UIEA200800358Intercostal · crackedBS 1220 LBL 106 BELOW FLOOR WEB CRACKED. FLOORBEAM INTERCOSTAL WEB REPAIRED AS PER 51-70-13 AND EO 4453A229.SDR UIEA200800357Door Frame · crackedL1 DOOR FORWARD UPPER FRAME CRACKED. L1 DOOR UPPER FORWARD FRAME REPAIRED AS PER SRM 51-70-06.SDR UIEA200800356Skin · crackedNR 7 VC FLAP EXTERIOR SURFACE CRACKED. NR 7 VC FLAP REPLACED IAW 27-81-02. RIGGING AND OPS CHECKED IAW 27-81-00.SDR UIEA200015Circuit Card · multiple failACFT DIVERTED. STATUS MESSAGE POWER SUPPLY. MULITIPLE CORRELATED MESSAGES DISPLAYED. REPLACED POWER SUPPLY "A" CARD AND SYSTEM OPERATED NORMAL. POWER SUPPLY "B" CARD REPLACED AND OPERATES NORMAL.SDR UIEA200900014Blower · failedPRIOR TO DEPARTURE A BURNING SMELL, VERY STRONG IN THE COCKPIT WITH VISIBLE SMOKE FROM BEHIND THE INSTRUMENT PANEL. MAINTENANCE FOUND THE EQUIPMENT COOLING SUPPLY BLOWER WITH EXCESSIVE OIL DEPOSITS ON THE INSIDE. MX REPLACED THE BLOWER FAN.SDR UIEA200800353Skin · gougedBS 1765 STRINGER 34-35R SKIN GOUGED. GOUGE REPAIRED AS PER BOEING MESSAGE 1-1165-0369-47-2 AND EO4453A227.SDR UIEA200800352Structure · dentedNR 1 LEADING EDGE DEVICE BULLNOSE DENTED. REPAIRED AS PER SRM 57-43-02SDR UIEA200800351Skin · dentedNR 10 VC FLAP BULLNOSE HAS DENT. REPAIRED AS PER SRM 57-43-02.SDR UIEA200800355Skin · looseLEFT WING LEADING EDGE FAIRING AT OUTBOARD OF LANDING LIGHT FOUND LOOSE RIVETS. LEADING EDGE REPAIRED AS PER SRM 57-41-01-2R-5 REPAIR 5 FIG 201.SDR UIEA200800354Skin · looseRIGHT WING LEADING EDGE FAIRING AT OUTBOARD OF LANDING LIGHT FOUND LOOSE RIVETS. LEADING EDGE SKIN REPAIRED AS PER SRM 57-41-01-2R-5 REPAIR 5 FIGURE 201.SDR UIEA200900006Warning System · false activationCREW REPORTED EQUIPMENT SMOKE STATUS MESSAGE DISPLAYED AFTER LANDING. EXISTING FAULTS REVIEWED , NO RELATED FAULTS NOTED. EQUIPMENT TEST WITH NO FAULTS RESULTS. ACFT WAS RELEASED WITH NO FURTHER MESSAGES.SDR UIEA200900007Engine · seizedENGINE 2 FAILED IN FLIGHT. AUTO SHUTDOWN, UNABLE TO AIR START ENG. FLIGHT LEVEL 380. NORMAL FLUID QUANTITIES AND ENGINE INDICATIONS AT THE TIME JUST BEFORE SHUTDOWN. MASTER CHIP DETECTOR FOUND CLEAN. FOUND ENGINE WOULD NOT TURN. REMOVED AND REPLACE ENGINE.SDR UIEA200900004Drive Assy · failedAIR TURN BACK, CREW PHONE PATCHED THAT THEY LOST NR 1 WX RADAR SYSTEM. NR 2 WX RADAR SYSTEM WAS ALREADY ON DEFERRAL. CREW RETURNED TO BKK. MAINTENANCE REMOVED AND REPLACED RADAR DRIVE ALL SYSTEMS, OPS CHECKED OK.SDR UIEA200800346Structure · damagedWHILE AIRCRAFT WAS TAXING, THE AIRCRAFT STRUCK ANOTHER AIRCRAFT THAT WAS PARKED CAUSING DAMAGE TO RIGHT WINGLET. RIGHT WINGLET REMOVED PER CDL, AREA VISUALLY INSPECTED AND AIRCRAFT RELEASED. ACFT AWAITING PERMANENT REPAIRS. OPENSDR UIEA200800344Panel · departedON SHORT FINAL APPROACH, THE AIRCRAFT WAS ADVISED BY DXB ATC THAT THERE WAS A HOLE IN THE LEFT WING. DXB SAFETY RECOVERED AND BOUGHT PANEL THAT LIBERATED ITSELF FROM THE AIRCRAFT TO THE DXB MAINTENANCE OFFICE. REPLACED PANEL AND PERFORMED RIB REPAIR PER SB 7SDR UIEA200800341Skin · puncturedAT DEPARTURE FOUND TAIL PUNCTURED THRU FUSELAGE EXTERNAL SKIN JUST FORWARD OF STA 2598 AT 6 O`CLOCK POSITION APPROX 11.5" BY 16". CUT OUT FUSELAGE SKIN DAMAGE AND LOWER CHORD AT STA 2598 AS PER SRM 53-00-01 AND 51-70-12. PERFORMED REPAIR IAW ATLAS EO NR 4453SDR UIEA2008341Skin · puncturedAT DEPARTURE FOUND TAIL PUNCTURED THRU FUSELAGE EXTERNAL SKIN JUST FWD OF STA 2598 AT 6 O'CLOCK POSITION APPROX 11.5 FT BY 16 INCHES. CUTOUT FUSELAGE SKIN DAMAGE AND LOWER CHORD AT STA 2598 AS PER SRM 53-00-01 AND 51-70-12. REPAIR NOT COMPLETED AT THIS TIME.SDR UIEA200800326Skin · damagedAIRSTAIRS TRUCK STRUCK AIRCRAFT AFTER BLOCK IN WITH STRUCTURAL DAMAGE FORWARD AND BELOW L-1 DOOR. REPAIR ACCOMPLISHED IAW EO 4453A213 PART 2 INITIAL AND REPEAT INSPECTION. HFEC INSPECTION PRIOR TO ACCUMULATION OF 250 FLIGHT CYCLES OR NEXT "A" CHECK. REPEAT SDR UIEA200800327Radar · failedRIGHT WEATHER RADAR FAILED APPROX 1 HOUR INTO FLIGHT. LEFT RADAR FAILED WHEN SELECTED. PERFORMED AIR TURNBACK. REMOVED DRIED AND REINSTALLED THE WAVE GUIDE DUE TO WATER CONDENSATION. REPLACED RADAR ANTENNA MOUNT AND RADAR CONTROL PANEL. WEATHER RADAR CONTSDR UIE2008F00035Shim · migratedSHIM MIGRATION AT RT BODY GEAR W/W FUSELAGE LONGERON STRUCTURE STATION 1468-1480. SHIM REPLACED IAW SRM 51-20-08, REV 48, SR ID NR 1-937881538 AND EO NR 4453A203. (K)SDR UIE2008F00034Skin · damagedDURING PFM J/C: MCIA016, REPLACE 6 BLIND FASTENER FOUND DEVIATION FOR STA 380, 440, S-1R MISS DRILLING HOLE. ACCOMPLISHED THE SEA DOUBLER HOLES ON SKIN COMMON TO THE STRAP AT BS 380, 440, AND 480 BETWEEN S1R AND A2R. (K)SDR UIE2008F00033Fairing · damagedFOUND NR 4 ENGINE SKIRT FAIRING SUPPORT BRACKET ATTACHED BOLT IB SIDE HOLE ENLARGED NEAR FAIRING DOOR NR 4 HINGE. REPAIR ACCOMPLISHED IAW SR ID NR 1945402461 AND EO NR 4464A066. (K)SDR UIE2008F00032Skin · crackedFOUND NR 3 ENGINE RT CORE COWL LOWER FACE CRACKED. 0.3 INCH AT NAC STA 288. REPAIRED IAW FORM NR E8207.4. (K)SDR UIE2008F00031Skin · dentedDENT WAS FOUND AT THE AFTER LOWER CORNER OF BULK CARGO DOOR. INSPECTED IAW SRM 51-10-00 AND SR ID NR 1949639862. (K)SDR UIE2008F00030Web · canningAFT CARGO COMPARTMENT FOUND FRAME WEB ALL CAN AT STA 1800, LBL 17 INCHES, S:60L. REPAIRED FRAME WEB OIL CAN AREA AT AFT CARGO COMPARTMENT STA 1800, LBL 16 TO LBL 20S:50L, FABRICATED IAW SRM 63-00-07, REV 48 AND SRM 51-40-02 REV 48 AND EO NR 4453A207. (K)SDR UIE2008F00029Stringer · corrodedFOUND RT FUSELAGE INNER STRINGER CORROSION AT STA 2580, S46R. REPAIRED RT FUSELAGE INNER STRINGER AT STA 2588, S-46R, IAW 747-400F SRM 53-00-03, FIG 201 REV 48 AND EO NR 4463A209. (K)SDR UIEA200800271Skin · damagedDURING WALKAROUND DAMAGE FOUND AT TAIL POST AREA BS 2618 STRINGER 46R. PART 1 INTERIM REPAIR ACCOMPLISHED IAW EO 4453A139. PART 2 INITIAL HFEC AT NEXT "A" CHECK. PART 3 REPEAT INSPECTION DVI AT EVERY "A" CHECK. PART 4 PERMANENT REPAIR AT NEXT "C" CHECK. (SDR P5CA0801571Structure · damagedDURING GROUND HANDLING THE TAIL JACK STRUCK THE TAIL SECTION OF THE AIRCRAFT NEAR THE TAIL POST FITTING IN SECTION 48 AT BS 2602. ACCOMPLISHED INTERIM REPAIR ACCORDING TO EO 4453A189, SRM 53-00-01 FIG 201, REPAIR 11. INITIAL AND REPEAT INSPECTIONS TO BE SCHESDR UIEA200800266Circuit Card · failedMASTER CAUTION/ FIRE WARNING BELL ON GROUND. NO EICAS MESSAGE (NO OTHER LIGHTS OR WARNINGS). REPLACED A15 CARD AT THE M5206 MODULE. OPS CHECKED OK. (S)SDR UIE2008F00000Fire Warning · false activationREF: LOG PAGE 362049; TWICE DURING CRUISE, MOMENTARY ILLUMINATION OF MASTER WARNING LIGHTS WITH ASSOCIATED FIRE WARNING BELL. NO EICAS MESSAGE. ACCOMPLISHED CMC GROUND TEST FIRE PROTECTION SYSTEM. (TEST PASS) NO FAULTS IN CMC FAULT HISTORY, MM26-10-00. (K)SDR AIEA200800263Fairing · damagedDURING ARRIVAL WALKAROUND INSPECTION FOUND LOWER RT AFT OF BODY GEAR FUSELAGE FAIRING DAMAGED. ACCOMPLISHED TIME LIMITED REPAIR AS PER EO 4453A188 DATED 7/8/08 ENTERED NON MEL DMI N08-037 FOR REPEAT INSPECTION OF PANEL AT EVERY A-CHECK. (A)SDR AIEA200800262Tire · failedDURING ARRIVAL WALK AROUND INSPECTION FOUND NR 11 TIRE SEPARATION. REPLACED NR 11 AND 12 WHEEL ASSEMBLIES. ALSO ACCOMPLISHED TIRE TREAD LOSS CONDITIONAL INSPECTION AS PER 05-51-34-202-001. (A)SDR AIEA200800260Engine · oil consumptionENGINE NR 3 OIL QTY WENT TO 0 (3 HOURS AFTER TAKEOFF). ENGINE SHUT DOWN PRECAUTIONARY. FIM 79-00-00 FOLLOWED. INSPECTED FOR OIL LEAK. NO WETTING FOUND. REPLENISHED 22 QTS OIL AND LEAK AND OPS CHECK PERFORMED. NO LEAK FOUND. IDG AND STARTER DRAIN LINE CASDR UIE2008F00004Panel · puncturedAFT CARGO COMPARTMENT TORQUE BOX TOP PANEL AT STA 1660 TO 1680 RT SIDE FOUND PUNCTURED AT 2 LOCATIONS. TORQUE BOX TOP PANEL REPAIRED IAW EO. (K)SDR UIE2008F00010Engine · power lossON TAKEOFF ROLL POWER WAS ADVANCED TO 70 PERCENT. N1 ENGINE 1,3, AND 4 ADVANCED NR 2 LAGGED SIGNIFICANTLY BEHIND, TAKEOFF ROLL ABORTED AT 40 KNOTS, AIRCRAFT TAXIED TO RUNUP AREA WHERE ENGINE RUN UP WAS PERFORMED AND NR 2 WAS NOW NORMAL. (K)SDR UIE2008F00008Skin · delaminatedFOUND DURING A-CHECK. REPAIR THE DAMAGE FOUND ON L/E OF LEFT OB FOREFLAP MEASURING 12 INCHES LONG BY 2 INCHES WIDE IAW SRM 51-70-07. REPAIR CARRIED OUT IAW EO 4457A145. (K)SDR UIE2008F00015Connector · looseDURING CLIMB EICAS "FIRE WARNING". FOUND CONNECTOR LOOSE AND RETIGHTENED SAME. OPS AND INDICATION NORMAL ON THE GROUND IAW AMM 26-10-01. (K)SDR UIE2008F00011Frame · crackedMAIN DECK CARGO COMPARTMENT RT AFT SIDEWALL CRACKS FOUND ON FRAME INNER FLANGE AT STA 1740 AND 1780. JUST ABOVE FRAME SPLICE AT BETWEEN STRINGER 11R AND 12R. REPAIRED IAW EO 4463A178. (K)SDR UIE2008F00014Wire · chafedDURING CRUISE, EICAS ADVISORY "HYD PRESS ENGINE 1" ON HYD SYNOPTIC. NR EDP AND DEMAND PUMPS RUNNING. THEN NOTED EDP INTERMITTENT AND IAW CHECKLIST EDP SWITCH OFF, BUT PUMP DID NOT SWITCH OFF. (EDP CONTINUED RUNNING INTERMITTENTLY AND DEMAND PUMP RUNNING). LASDR UIEA200800217Fire Warning · false activationEICAS MESSAGE "APU" PULLED APU FIRE SWITCH IAW QRH. INSPECTED APU COMPARTMENT. NO DEFECTS NOTED. RESET FIRE HANDLE APU, OPS NORMAL PER MM 49-11-00. OK FOR CONTINUED SERVICE.SDR UIEA200800216Brake · fireNR 1 BRAKE CAUGHT FIRE AFTER AIRCRAFT ON BLOCKS. FIRE EXTINGUISHED IMMEDIATELY, NO MORE THAN 10 SECONDS. BRAKE TEMP IN NORMAL BAND 3 UNITS. OVERHEAT INSPECTION CARRIED OUT IAW MM TASK 5-51-10-202-001 AS A PRECAUTION ONLY. REF LOG PAGE 373339 FOR BRAKE AND SDR UIEA200800171Duct · damagedAFTER TAKEOFF UNABLE TO PRESSURIZE AIRCRAFT. FOUND CONDITIONED AIR CHECK VALVE CRACKED AND FOUND HOLE ON FORWARD CARGO COMPARTMENT AIR SUPPLY DUCT. REMOVED AND REPLACED CHECK VALVE AND ACCOMPLISHED LEAK CHECK IAW 21-28-08. AIR DUCT REMOVED AND FORWARDED FORSDR UIEA200800170Dump Valve · failedLOUD BANG FOLLOWED BY RAPID RISE IN CABIN ALTITUDE WITH "CABIN ALT" EICAS MESSAGE. FOUND NR 1 PACK DUMP VALVE AT FAULT. DEACTIVATED VALVE IN CLOSED POSITION. TRANSFERRED TO MEL M08-058 REF MEL 21-51-10 CAT C.SDR UIEA200800176Actuator · burnedDURING THE "A"4 CHECK PDU 6R STEERING ACTUATOR WAS DISCOVERED TO HAVE BURN MARKS. DEACTIVATED THE PDU AND PLACED ON DEFERRAL. REF MEL 25-53-01 CAT D, DMI M08-036. THIS ITEM IS CONSIDERED OPEN UNTIL THE PDU IS REPLACED.SDR UIEA200800112Fan Blade · dentedNR 4 ENGINE 2 EACH FAN BLADES WITH DAMAGE WITH DENT. DYE PENETRANT CHECK OF BLADES FOUND DENTS WITHIN LIMITS OF TASK 72-31-02-206-001-J00. NO CRACKS FOUND.SDR UIEA200800111Warning Message · illuminatedABORTED TAKEOFF DUE TO ENGINE 4 REVERSER EICAS MESSAGE APPEARED AT 70 KNOTS ON TAKEOFF ROLL. REJECTED TAKEOFF EICAS MESSAGE REPLACED WITH STATUS MESSAGE. DEACTIVATED THE REVERSER AND PLACED ON DMI PER MEL 78-31-01.SDR UIEA200800096Panel · delaminatedLT WING UPPER SURFACE FLYING PANEL AT T/E CLOSEST TO FUSELAGE HAS DELAMINATION AT OUTBOARD EDGE APPROX 18 INCHES INBOARD FROM NR 6 SPOILER. DELAMINATION REPAIRED IAW ATLAS EO NR 4457A137 AND SRM 51-70-07.SDR UIEA200800095Skin · damagedLT OUTBOARD T/E FORE FLAP SURFACE DAMAGE ON BULLNOSE AREA AT OUT BOARD END. REPAIRED PER SRM 51-70-07 AND ATLAS EO 4457A135.SDR UIEA200800094Rub Strip · wornRT WING INBOARD AILERON UPPER SURFACE HAS RUB STRIP WORN THROUGH. REPAIRED RUB STRIP IAW ATLAS EO 4457A136 AND SRM 57-60-01 FIG 201 AND SRM 51-70-09 AND 51-70-10.SDR P5CA0801550Gimbal Joint · brokenDURING ROUTINE INSPECTION OF NR 3 THRUST REVERSER FOUND LT LOWER ACTUATOR MOUNTING BRACKET GIMBAL BROKEN. REMOVED THE NR 3 ENGING LOWER LT ANGLE GEARBOX HOUSING AND BALLSCREW ACTUATOR AS PER AMM 78-31-22, PERFORM DVI INSPECTIONS PER EO NR 4478A065 PRIOR TO EA
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