Boeing 747-206B
Service difficulty reports · 34
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 = '747206B' 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 = '747206B' 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 Q2SA748010Engine · malfunctionedDURING CLIMBOUT OF FL130 FROM SCEL THERE WAS VIBRATION FOLLOWED BY A LOUD BANG, ACCOMPANIED BY YAW AND HIGH EGT ON NUMBER 3 ENGINE. THE EGT LIGHTS FOR NR 3 CAME ON AND THE GAUGE INDICATION, PEGGED OUT. ENGINE SHUTDOWN RECALL ITEMS AND THE SEVERE DAMAGE CHECKSDR Q2S2010F00018Frame · crackedNR 4 PYLON UPPER TORQUE BOX NAC STA 270 BLKHD INBD FRAME UPPER SECTION FOUND CRACKED.SDR Q2S2010F00017Doubler · damagedEAO NR 4753086R1 (SB 747-63-2474) EXISTING FASTENER HOLE (16 EA) FOUND ENLARGED TO .2500". ORIGINAL FASTENER HOLE SIZE IS .1875".SDR Q2S2010F00016Frame · crackedNR 1 PYLON FRONT SPAR OTBD FRAME UPPER END FOUND CRCKED.SDR Q2S2010F00011Doubler · damagedEAD NR 4753086 R1 (SB 747-53-2473) EXISTING FASTENER STATED IN SB REV 2 FLAG, 8 COUNTERSINK ON FWD SIDE HAS DISCREPANCY. REPAIR CARRIED OUT IAW EN NR 350-09.SDR Q2S2010F00014Doubler · damagedEAO NR 4753086R1 (SB 747-53-2473) EXISTING FASTENER HOLE WHICH REQUIRES NDT INSP IN SB NOT FOUND. REPAIR CARRIED OUT IAW EN NR 350-09.SDR Q2S2010F00013Doubler · crackedEMPENNAGE HFEC OPEN HOLE CARRIED OUT AT STA 2598 RT BULKHEAD AND FOUND 2 EA HOLE CRACK INDICATION AT DOUBLER. REPAIR CARRIED OUT IAW EN NR 355-09.SDR Q2S2010F00012Doubler · damagedEMPENNAGE WHILE CARRIED OUT MODIFICATION AT STATION 2598 RT BULKHEAD IAW SB 747-53-2473, REV 2, FOUND 6 EA EXISTING HOLES IAW DWG 624U0061 FASTENERS TO BE INSTALLED (.1875) HILOKS. REPAIR CARRIED OUT IAW EN NR 355-09.SDR Q2SA746012Rectifier · failedDURING CLIMBOUT OF OHSJ, CREW SMELLED ELECTRICAL SMOKE, RAN CHECKLIST AND FOUND SMOKE COMING FROM ESSENTIAL TRANSFORMER RECTIFIER. COCKPIT PORTABLE FIRE EXTINGUISHER USED AS PRECAUTION. CREW EXECUTED A SAFE AIR TURNBACK TO DEPARTURE AIRPORT OHSJ.SDR Q2SA746011Fairing · inflt separationON POST-FLIGHT INSPECTION, FOUND SECTION 44 UPPER RT WING-TO-BODY FAIRING PANEL (NR 292DR) MISSING, WITH BROKEN ATTACH BRACKETS ON ACFT STRUCTURE. REPLACED DAMAGED PANEL AND SUPPORT BRACKETS IN ACCORDANCE WITH B747 SRM 51-30-02 AND 51-20-01.SDR Q2SA748009Door · crackedDURING CRUISE INBOUND TO KMIA, CREW REPORTED MAIN DECK WINDOW 850R SOUNDED LIKE AIR LEAK. FURTHER INSPECTION ON GROUND REVEALED 9 INCH CRACK IN MAIN ENTRY DOOR 2R SIDE FRAME. DOOR ASSEMBLY REMOVED AND REPLACED IN ACCORDANCE WITH AMM 52-11-01/PG 401.SDR Q2SA746010Slide · unwanted deployINADVERTENTLY DEPLOYED LEFT UPPER DECK SLIDE WHILE AIRCRAFT WAS ON GROUND AT KMIA. REMOVED SLIDE IN ACCORDANCE WITH AMM 25-68-02. TRANSFERRED TO DEFERRED MAINTENANCE ITEM NR 18822 PER MEL 25-11 (3). PLACARD INSTALLED.SDR Q2SA748008Wire Harness · chafedON TAXI-OUT AT SKBO, WIND SHEAR LIGHT CAME ON WHEN THROTTLE ADVANCED. MULTIPLE FAILURES, WIND SHEAR LIGHT FLICKERED AND WENT OFF, THEN SMOKE CAME UP THROUGH THROTTLE QUADRANT; LOST GEAR DOWN GREEN LIGHT, AND ANTI-SKID LIGHT ILLUMINATED ON FWD PANEL; LOST ANTISDR Q2SA748007Battery Pack · dischargedDURING PRE-FLIGHT FROM KMIA, FOUND FORWARD AND AFT UPPER DECK EMERGENCY EXIT SIGNS INOPERATIVE. REMOVED AND REPLACED BATTERY PACKS IN ACCORDANCE WITH AMM 33-51-04.SDR Q2SA746009Panel · detachedON TOP OF CLIMB-OUT, CREW EXPERIENCED AIRFRAME VIBRATION, SUBSEQUENTLY PERFORMING FUEL DUMP (30,000 LBS) AND AIR TURN BACK TO KMIA. ON INSPECTION AFTER LANDING, FORE AND MID-FLAP DAMAGE WAS FOUND ON RIGHT WING, RESULTING FROM RIGHT WING FLIGHT PANEL HAVING DESDR Q2SQ746008Brake Assy · overheatedACFT LANDED (KDFW) WITH OVERHEATED BRAKES (725 - 800 DEGREES F) AT NR 4, NR 7, NR 9, NR 10, NR 11, NR 15, NR 16 WHEEL POSITIONS. FLASH FIRE AT NR 7 BRAKE ASSEMBLY. INSPECTED IN ACCORDANCE WITH AMM 05-51-26 AND AMM 32-41-15. R&R NR 7 MAIN WHEEL ASSEMBLY AS PSDR Q2SA748005Precooler · leakingON TAKEOFF FROM KMIA, UNABLE TO OBTAIN NECESSARY N1 OF 113.6 PERCENT FOR NR 2 ENG. AT N1 OF 109.0 PERCENT, RED WARNING CAME ON AND N1 MAINTAINED INDICATION AT 109.0 PERCENT. ON CLIMBOUT FROM KMIA, BOTH CHANNEL A & B NACELLE TEMPERATURE INDICATIONS WERE 5.0. SDR Q2S2008F00002Engine · failedDURING TAKEOFF, THE NR 3 ENGINE FIRE WARNING INDICATIONS (VISUAL/AURAL) WENT OFF AT 1,500 FT. PULLED BACK THE THROTTLE, INDICATIONS WENT OUT. ENGINE SHUT DOWN AND RETURNED TO LAGOS, NIGERIS (DNMM). FUEL WAS NOT DUMPED AS AIRCRAFT WAS NOT LOADED WITH CARGO ASDR Q2S2008F00000Fire Warning · illuminatedIN FLIGHT ON CLIMBOUT, NR 4 ENGINE FIRE WARNING LIGHT ILLUMINATED, ACCOMPLISHED AIRCRAFT OPERATING MANUAL (AOM) (SAI OP-523) PROCEDURES. FIRE INDICATIONS WENT OUT WHEN ENGINE SHUTDOWN. NO FIRE BOTTLES BLOWN. NR 4 ENGINE CENTER LOWER ACCESS DOOR FOUND OPEN AFSDR Q2SA746006Pitot Tube · defectiveON DEPARTURE, CAPTAIN AND FIRST OFFICER'S ALTIMETER SPLIT 500 FEET, AIRSPEED SPLIT 30 KTS. WHEN ALTERNATE STATIC SELECTED ON CAPTAIN'S SIDE, ALL INSTRUMENTS MATCHED UP. DURING ILS FLIGHT, ALTITUDE SHOWED 1800 FEET AT 6.3 DME (SHOULD HAVE BEEN 1600 FEET). RESDR Q2SA746005Indicator · inaccurateERRONEOUS ALTITUDE INFORMATION AND AIRSPEED FROM FLIGHT OFFICER'S INDICATORS. AT 11,000 FEET, 600 FEET DIFFERENCE. AT 240 KTS, IT WAS 30 KTS FAST. COMPLETED LEAK CHECK AND STATIC CHECK ON PITOT STATIC SYSTEM IN ACCORDANCE WITH AMM 34-11-01. COULD NOT DUPLISDR Q2SA746003Slide · unwanted deployINADVERTENTLY DEPLOYED LEFT UPPER DECK SLIDE WHILE AIRCRAFT WAS ON GROUND AT KMIA. REMOVED SLIDE IN ACCORDANCE WITH AMM 25-68-02. TRANSFERRED TO DI NR 14742 PER MEL 25-11. PLACARD INSTALLED. SLIDE DEPLOYED WITHOUT ANY PROBLEMS.SDR Q2SA748003Indicator · erraticEGT'S ALL READING ERRATIC DURING CLIMB-OUT FROM KMIA. OFF FLAGS FOR NR 2 COMES ON ERRATICALLY, NO LIGHTS COME ON. OPERATIONAL NORMAL AT ENGINE START AND CRUISE FLIGHT. RETURNED TO KMIA. NO FUEL DUMPED. REMOVED AND REPLACED VERTICAL SCALE EGT INDICATOR IN SDR 746004Slide · unwanted deployUPPER DECK LEFT ESCAPE SLIDE INADVERTENTLY DEPLOYED. REMOVED SLIDE ASSEMBLY AND TRANSFERRED TO DEFERRED ITEM.SDR 748002Access Panel · looseNOSE LANDING GEAR DOOR OPEN LIGHT ILLUMINATED IN FLIGHT. COMPLETED DOOR OPEN LIGHT PROCEDURES IAW QRH. FOUND LOOSE ACCESS PANEL AND PARTS BAG OBSTRUCTING RIGHT HAND DOOR HINGE. SECURED PANEL AND OPERATIONALLY CHECKED NOSE GEAR DOOR SYSTEM WITH NO FURTHER DISDR 748001Slide · unwanted deployINADVERTENTLY DEPLOYED RIGHT SIDE UPPER DECK SLIDE WHILE AIRCRAFT WAS PARKED AT KMIA. REMOVED SLIDE IN ACCORDANCE WITH AMM 25-68-07. TRANSFERRED TO DI LOG #12408 IN ACCORDANCE WITH MEL 25-11. PLACARD INSTALLED. SLIDE DEPLOYED WITHOUT ANY MALFUNCTION.SDR 746003Manifold · failedAFTER TAKE OFF FROM RKSI, NR 3 ENGINE FIRE WARNING CAME ON. PERFORMED QRH PROCEDURE. DUMPED 176,000 LBS OF FUEL AND SHUTDOWN THE ENGINE. RETURNED TO RKSI. FOUND LEFT CDP TUBE FLEX JOINT FAILED. REPLACED FAILED CDP TUBE IN ACCORDANCE WITH AMM 75-25-00. LESDR Q2SA746002Connector · looseDEPARTED KLAX AND FOUND NR 1 PACK SYSTEM INOPERATIVE. NO PRESSURIZATION. RETURNED TO KLAX. NO FUEL WAS DUMPED. FOUND NR 1 PACK CONTROL VALVE CONNECTOR LOOSE. SECURED NR 1 PACK CONTROL VALVE CONNECTOR. OPERATIONAL CHECK GOOD IN ACCORDANCE WITH AMM 21-00-0SDR Q2SA746001Actuator · unlatchedNOSE GEAR DOOR OPEN LIGHT ILLUMINATED AND REMAINED ILLUMINATED WHEN GEAR LEVER SELECTED OFF. ACCOMPANIED BY VIBRATION AND AIR NOISE. AIRCRAFT RETURNED TO KDFW. REMOVED AND REPLACED NOSE GEAR DOOR ACTUATOR PER AMM 32-34-14, OPERATIONAL AND LEAKS CHECKS GOOD.SDR 05009Garlock Seal · failedPRECAUTIONARY ENG SHUTDOWN ON NR 1 ENG DUE TO LOW OIL QTY. REMOVED AND REPLACED CONSTANT SPEED DRIVE GARLOCK SEAL IAW MM 72-61-07. REMOVED AND REPLACED TRANSFER TUBE "O" RINGS IAW MM 72-61-15 DUE TO BROKEN "O" RING. REMOVED AND REPLACED NR 1 CONSTANT SPEED SDR 746002Engine · failedON TAKEOFF, NR 4 ENGINE EXPERIENCED A COMPRESSOR STALL. CREW SHUT DOWN ENGINE, DUMPED FUEL AND RETURNED TO BASE. ENGINE BOROSCOPED WITH NO DEFECTS NOTED. FOUND METAL IN TAILPIPE. ENGINE IS BEING REPLACED AT THIS TIME.SDR 2004F00425Spar · crackedDURING REPLACEMENT OF THE WING REAR SPAR LOEWR CHORD SPLICE PLATE FITTING H-11 BOLTS AS P[ER BOEING SB 747-57A2309, CRACK WAS FOUND COMMON TO THE RIGHT WIND REAR SPAR LOWER CHORD ONLY AT FASTENER CODE 'C' LOCATION. HOLE 'C' REAMED TO 1.316 INCH DIAMETER. NDTSDR TWAA9615401Csd Seal · leakingCDG - DURING CRUISE SHUT DOWN NR 3 ENGINE, S/N 4299, DUE TO LOSS OF OIL. FOUND CSD DRIVE SEAL, MFG P/N 2-138V0884-75, LEAKING. REPLACED CSD DRIVE SEAL, ENGINE OPERATION AND LEAK CHECKS NORMAL. (M)SDR 96ZZZX5920Wire · openSTL - FLT 1 - DURING PRE-FLIGHT, UPPER DECK EGRESS LIGHTS WERE INOPERATIVE. FOUND OPEN WIRE 21070-19796-20 TO CONNECTOR D3272J. ACCOMPLISHED AIRWORTHY REPAIR TO WIRING. EGRESS LIGHT SYSTEM OPERATION CHECKED NORMAL. CHECK C-1 - 4-13-96 - SBA.
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