Boeing 747-2D7B
Service difficulty reports · 726
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 = '7472D7B' 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 = '7472D7B' 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 UIEA99086Stringer · misdrilledDURING ACCOMPLISHMENT OF SB 747-53A2390 FIG 19, DETAIL L, OVERSIZING HOLES AT STRINGER 39 LEFT AND RIGHT SIDES FROM .25 INCH BY .375 INCH WOULD CAUSE UNACCEPATABLE EDGE DISTANCE. PER TELEX TLS-AMS-99-00033H, PERFORMED HFEC OPEN HOLE INSPECTION, OVERSIZED HOLESDR UIEA99085Bulkhead · crackedWHILE ACCOMPLISHING SB 747-53A2390, HFEC INSPECTION OF BS 1480 HOLE NR 19 REVEALED A CRACK IN THE WEB PANEL ONLY. PER SB 747-53A2390 HOLE WAS OVERSIZED TO .5625 INCH WEB PANEL ONLY. INSTALLED FREEZE PLUG. FABRICATED SEPARATE BUSHING FOR THE WEB SPLICE PLATESDR UIEA99084Doubler · crackedL1 DOOR HINGE CUTOUT DOUBLER, PREVIOUSLY INSTALLED, AT THE LOWER CUTOUT FOUND CRACKED. REPLACED DOUBLER ON DOOR HINGE CUTOUT PER SB 747-52-2144. (M)SDR UIEA99083Doubler · crackedR1 DOOR HINGE CUTOUT DOUBLER CRACKED, PREVIOUSLY INSTALLED AT UPPER CUTOUT. REPLACED DOOR HINGE CUTOUT DOUBLER PER SB 747-52-2144. (M)SDR UIEA99082Fitting · crackedDURING HFEC INSPECTION OF BS 1480, FOUND LEFT OUTERCHORD SPLICE FITTING CRACKED BETWEEN HOLES NR 14 AND NR 15. REPLACED SPLICE FITTING IAW SB 747-53A2390. (M)SDR UIEA99081Fitting · crackedDURING ROUTINE INSPECTION, FOUND NR 6 SUPPORT ACTUATOR SUPPORT FITTING CRACKED ON SPOILER SUPPORT BEAM. REPLACED SUPPORT FITTING PER SRM 51-30-02. (M)SDR UIEA9975Ignitor · erodedFLT 2087 - ANC-KIX - DURING DESCENT THROUGH 4000 FT, NR 1 ENGINE FLAMED OUT. FLIGHT CRWE DID NOT ATTEMPT TO RE-START ENGINE. AIRCRAFT LANDING AT KIX UNEVENTFUL. MAINTENANCE PERFORMED TROUBLESHOOTING AS PER MM 71-00-42. NO FAULTS FOUND. BOTH IGNITERS WERE SDR UIEA99074Fitting · crackedNR 6 SPOILER SUPPORT FITTING CRACKED AT LOWER LEFT SIDE ATTACHING FLANGE APPROXIMATELY 2 INCHES BETWEEN AND OUT OF SECOND AND THIRD RIVET HOLE. FITTING ATTACHED TO THE AFT SIDE OF WING GEAR AFT SUPPORT BEAM. FITTING REPLACED DURNIG CURRENT C-CHECK AT KLM. (SDR UIEA99062Bolt · failedBOLTS SHEARED AT BODY STATION 1241 LBL 110 AND LBL 118. INSPECTED AREA, FOUND NO DEFECTS. PERFORMED HFEC INSPECTION PER D6-7170 51-00-00 PART 6, FOUND NO CRACKS. REPLACED BOLTS. TORQUED BOLTS PER 20-51-00. (M)SDR UIEA99061Bolt · failedAFT PRESSURE BULKHEAD HAS SHEARED BOLT AT STRINGER 14 RT SIDE. INSPECTED AREA FOUND ON DEFECTS. REPLACED BOLT. TORQUED PER MM 20-51-00. (M)SDR UIEA99060Bolt · failedRT WING GEAR FORWARD TRUNNION OUTBOARD SIDE SUPPORT FITTING HAS SHEARED BOLT ON OUTBOARD UPPER ATTACHMENT. INSPECTED AREA, FOUND NO DAMAGE. REPLACED BOLT PER DRAWING 65B010222 FR 2 10-2480. REPLACED SHEARED BOLT WITH P/N BACB30US7K20. (M)SDR UIEA9934Duct · crackedJFK/MIA - FLT GT870 - NR ENGINE FLAME-OUT AT TOP OF DESCENT. UNABLE TO RE-LIGHT. MAINTENANCE CHECKED THE FOLLOWING AND NO DISCREPANIES NOTED (INLET AND EXHAUST, VISUAL CHECK UNDER COWL, BLEW OUT CDP LINE. CHECKED CHIP DETECTORS, FUEL FILTER FOUND CLEAN, SUSDR UIEA9931Structure · damagedFLT GT363 - ON ARRIVAL, GROUND OPERATIONS FOUND WHEN THE REAR LOWER LOBE CARGO DOOR WAS OPENED, [ALLET POSITION NR 9 HAS SHIFTED AFT GOING OVER THE END STOPS. THERE WAS STRUCTUAL DAMAGE TO THE BRACE POST ON BOTH SIDES OF THE COMPARTMENT THAT SEPARATE THE BULSDR UIEA9930Gcu · inoperativeTPE/ANC - FLT GT386 - AFTER TAKEOFF, NR 2 GENERATOR FIELD AND MAIN BREAKER TRIPPED FOLLOWED BY NR 2 BUS TIE BREAKER TRIP. ONE MINUTE LATER, NR 1 GENERATOR FIELD AND MAIN GEN BREAKER TRIPPED. COULD NOT RESTORE EITHER GENERATOR. RESET NR 2 BTB AND THE NR 1 BTSDR UIEA9920Map Light · smokingFLT EK9880 - AMS/DXB - APPROXIMATELY 5 HOURS IN CRUISE, CAPTAIN NOTICED SMOKE COMING FROM AREA OF CAPTAINS MAP LIGHT ASSEMBLY. THIS WAS A MOMENTARY CONDITION. THE FLIGHT CONTINUED FOR ANOTHER 4 HOURS UNEVENTFULLY. DXB MAINTENANCE INSPECTED ALL WIRING BEHINDSDR UIEA9923Ins · malfunctionedFLT AZ9204 - MXP/JFK - ATB - ALL THREE INS SYSTEMS MALFUNCTIONED. ALL PREFLIGHT FUNCTIONS WERE NORMAL, INS ALIGNED AND LOADED PROPERLY. AFTER DEPARTURE FROM MXP, UPDATED NR 1 INS USING LSA (VOR) AND GVA FOR NR 2 INS, UPDATE PROPERLY OBTAINED. A SECOND UPDATSDR UIEA9913Panel · missingDURING WALKAROUND, FOUND 6 INCH BY 12 INCH PIECE OF RIGHT WING FUSELAGE PANEL MISSING. NO OTHER ABNORMALITIES NOTED. REPLACED PANEL P/N 65B067212. (M)SDR UIEA9905Pdu · defectiveFLT 1358 - ANC/LAX - ATB - AFTER TAKEOFF, DURING FLAP RETRACTION, RIGHT NR 1 LEADING EDGE FLAP WOULD NOT RETRACT. TRIED TO USE ALT SYSTEM BUT LE FLAP DRIVE C/B TRIPPED. RESET CIRCUIT BREAKER AND TRIED AGAIN BUT NOT HELP. DUMPED 6,000 KILOS OF FUEL AND RETURSDR UIEA9904Card · looseFLT C1366 - ATO-AUH - AT APPROX 90 KNOTS, ENGINE FIRE BELL SOUNDED AND REJECTED TAKEOFF PROCEDURES ACCOMPLISHED. NO ENGINE OR APU FIRE LIGHTS 'ON'. COULD NOT SILENCE BELL USING NORMAL RESET. HIT COVER ON FIRE WARNING CONTROL MODULE AND BELL SILENCED. DURINSDR UIEA9903Airspeed · defectiveFLT TG891 - BTB - DURING TAKEOFF ROLL, F/O'S AIRSPEED INDICATOR DID NOT MOVE AND CAPTAINS AIRSPEED INDICATOR JUMPED FROM 70 TO 80 KNOTS. RETURNED TO BLOCKS AND DURING TROUBLESHOOTING CONFIRMED THAT BOTH AIRSPEED INDICATORS WERE DEFECTIVE. REPLACED CAPTAINS ASDR UIEA9902Turnbuckles · failedDURING LANDING WITH REVERSE ACTIVATED, NR 3 THRUST REVERSER LEVER SNAPPED FORWARD AND NR 3 ENGINE STAYED IN FULL REVERSER. UNABLE TO REDUCE TO IDLE REVERSE. ENGINE SHUT DOWN. FOUND THE TURNBUCKLES FOR PUSH PULL CONTROL CABLE AT T3A-4 AND T3B-4 HAD COME APARSDR UIEA9804Nlg · malfunctionedANC - DURING APPROACH, 'NOSE GEAR DID NOT EXTEND NORMALLY - MANUAL EXTENSION OK'. CHECKED RIGGING OF NOSE GEAR SEQUENCE VALVE LOCK MECHANISM AND ACTUATOR AND FOUND SAME TO BE NORMAL. PERFORMED GEAR EXTENSION/RETRACTION CHECK PER MM 32-34-00, AND NO DEFECTS FSDR UIEA9801Air Distribution · odorFRA/SHJ - FLT TG891 - AFTER TOP OF DESCENT, A STRONG ELECTRICAL SMELL WAS NOTED. FLIGHT DECK FAN WAS ON AT THE TIME FOR APPROX 10 MINUTES. FAN SWITCHED OFF. P6 CIRCUIT BREAKER PANEL (FRONT, BACK, AND UNDER F/E TABLE) WERE CHECKED FOR SMOKE AND ODORS. THE SSDR UIEA9704Engine · failedCREW REPORTS: ABORTED TAKEOFF FLT SK5086/06, SHJ/GOT...DURING TAKEOFF, FLIGHT CREW REPORTED A LOUD BANG AT 90-100 KNOTS AND ABORTED TAKEOFF DUE NR 1 ENGINE FAILURE (SN 528419). INSPECTION OF ENGINE REVEALED AFT CENTERBODY DEPARTED AIRCRAFT. LPT BLADE PENETRSDR UIEA9703Coupling · failedATB, MIA/EZE - FLT 7425/16 - 'AFTER TAKEOFF AT 1800 FEET, NR 4 ENGINE EGT JUMPED UP ABOUT 50 DEGREES, IMMEDIATELY FOLLOWED BY A FIRE WARNING...FIRE WARNING CEASED AFTER FUEL SHUT OFF TO ENGINE. COMPLETED PROCEDURES'. FOUND CLAMP ON TUBE ASSY (AFT AIR SUPPLY)SDR 97ZZZX4572Seat Track · brokenDURING A-CHECK, FOUND SEAT TRACK BROKEN AT STA 1810 TO STA 1850 ON MAIN CARGO DECK AND FLOOR FITTING DAMAGED. FLOOR FITTING REPLACED AND SEAT TRACK REPLACED PER SRM 53-10-05, FIG 33, SHEET 4.
Back to Boeing 747-2D7B