JASC 7260
Service difficulty reports · 1,098
Reports filed under 7260 · Turbine Engine Accessory Drive, newest first.
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 jasc_code = '7260' 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 jasc_code = '7260' 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 HALA2008111400849Adapter · crackedRT ENGINE GEAR BOX STARTER MOTOR ADAPTER PLATE CRACKED HORIZONTALLY IN TWO POSITIONS ACROSS TOP AND BOTTOM OF ADAPTER. POSSIBLE FATIGUE CAUSED BY IMBALANCE OF STARTER FAILURE. REPLACED IAW ENGINE MANUAL, SUBTASK 72-61-00-430-061.SDR 2008FA0000721Relay · intermittentTHE PILOT REPORTED THAT AFTER TURNING ON TO THE RUNWAY FOR TAKEOFF AND APPLYING POWER THE ENGINE CHIP LIGHT CAME ON AND STAYED ON. POWER WAS REDUCED, AND TOWER APPROVED A RETURN BACK TO THE RAMP. THE AIRCRAFT NEVER APPROACED TAKEOFF SPEED. THE AIRCRAFT WAS SDR UALA2008111306196Gearbox · damagedNR 1 ENG ANGLE GEAR BOX (AGB) AFT END HAS LOOSE BOLTS AT 12:00 AND FLANGE EAR IS BROKEN AT 1:00. REPLACED NR 1 ENGINE. ENGINE WAS SUBSEQUENTLY FIELD REPAIRED. THE ANGLE GEARBOX (AGB), HORIZONTAL DRIVESHAFT, AND CP07 FUEL TUBE WERE REPLACED.SDR 2008UALA06196Flange · brokenNR 1 ENG ANGLE GEAR BOX AFT END HAS LOOSE BOLTS AT 12:00 AND FLANGE EAR IS BROKEN AT 1:00.SDR UALA2008111305581Bearing · failedNR 2 ENGINE IFSD. FLIGHT DIVERTED. REPLACED ENGINE PRIOR TO FURTHER FLIGHT. SHOP TEARDOWN REVEALED THAT THE MAIN GEARBOX (MGB) HAD A FAILURE OF THE MB7 BEARING, THE MB8 BEARING, AND DRIVESHAFT ASSEMBLY. ROOT CAUSE FOR THIS FAILURE, AND CORRECTIVE ACTION, ASDR CA080828005Spur Gear · damaged(CAN) FRONT GEAR CASE ON ENG REMOVED FOR TORQUE RING REPLACEMENT. PITTING FOUND ON SPUR AND HELICAL GEAR ASSY. CONSULTATION WITH ENGINE OVERHAUL FACILITY IS ON GOING.SDR VNAA0808012Gearbox · failedCREW REPORTED THE LT ENGINE FAILED ON CLIMBOUT. CREW ELECTED TO DIVERT TO IAD LANDING WITHOUT INCIDENT. MX INSPECTED ENGINE AND FOUND THE LT GEARBOX FAILED. GEARBOX WAS R&R. CHECKS WERE COMPLETED AND NO DEFECTS NOTED. ACFT WAS RELEASED FOR SERVICE.SDR AALA200802042Gearbox · failedTUL INFLIGHT T1009/08AUG SDF TO DFW. CREW REPORTED NR 2 ENGINE VIBRATIONS AND ENGINE PRESSURE RATION FLUCTUATION FOLLOWED BY NR 2 ENGINE UNCOMMENTED SHUTDOWN. LANDED TOOL WITHOUT INCIDENT. REPLACED NR 2 ENGINE ON 10 AGUE AT TOOL DUE TO GEAR BOX FAILURE. SYSDR CA080806007Gearbox · defective(CAN) DURING FLIGHT, CREW NOTICED THEY LOST THE NR1 ENGINE OIL INDICATION AND GOT THE RED LED. SHUTDOWN ENGINE AND MADE AN UNEVENTFUL LANDING. CREW NOTICED A PUDDLE OF OIL UNDER THE NR1 ENGINE AFTER LANDING. DURING THE TROUBLESHOOTING, THEY REMOVED THE DRAINSDR CA080806003Gearbox · disconnected(CAN) DURING FINAL APPROACH, THE ENGINE FLAMED OUT. RELIGHT ATTEMPT WAS UNSUCCESSFUL. AN UNEVENTFUL SINGLE ENGINE LANDING FOLLOWED. POST EVENT TROUBLESHOOTING, FOUND THAT THE ENGINE COULD NOT BE RE-STARTED. ACCESSORIES GEARBOX DE-COUPLE IS CONFIRMED. THE AFFECSDR DL764080769Cover · missingLEFT ENG SHUTDOWN AT 15000 FT DUE TO LOW OIL PRESSURE AND QUNTITY DURING CLIMBOUT. INFO DURING CHECKLIST AND SUBSEQUENT SHUTDOWN ENG WAS RUN AT 8 PSI FOR LESS THAN 30 SEC AT CRUISE POWER AND APPROX 3-4 MIN AT IDLE, PLS CHECK FOR TIME ACCURACY. OPENED LT ENG SDR 2009FA0000421Chip Detector · looseCHIP DETECTOR CAME OUT OF ENGINE IN FLIGHT OVER OCEANANIC AIRSPACE, CAUSING OIL PRESSURE FLUCTUATION THEN CAUSING OIL PRESSURE LOSS. ACFT DECLARED AN EMERGENCY. THE ACFT LANDED IN CANADA AND WAS INSPECTED BY A SENIOR DUTY ENGINEER. IN HIS WORK REPORT HE STATESDR DL76L080569Gearbox · making metalMETAL FOUND ON THE NR 2 ENGINE CHIP DETECTOR. DURING INVESTIGATION FOUND TO BE METAL FROM GEARBOX. WILL REPLACE NR 2 ENG.SDR C8GA20080012Helicoil · damagedFLT 708 FROM MCI TO PHX - DURING CRUISE OPERATION THE CAPTAIN WAS NOTIFIED THAT THE NR 1 ENGINE OIL QUANTITY WAS DECREASING. THE NR 1 ENGINE WAS SHUT DOWN AND EMERGENCY WAS DECLARED, THE AIRCRAFT DIVERTED TO ABQ WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT SDR 2008UALA01004Bearing · failedFOUND EXCESSIVE BLACK METAL COVERING CHIP DETECTOR HEAD, AT NR 2 ENG MAIN OIL TANK (MCD). FOUND GEARBOX (MCD) FULL OF METAL CONTAMINATION. ENGINE REPLACED AT ORD. THE MB-7 AND MB-8 BEARINGS IN THE MAIN GEARBOX WERE FOUND TO HAVE FAILED. PRATT & WHITNEY HAS RSDR CHQA200800020Seal · leakingIAH TO SRQ - DURING CLIMB, THE CREW RECEIVED A WARNING FOR E1 OIL PRESSURE. E1 OIL PRESSURE WAS NOTED TO FLUCTUATE FROM BELOW 25PSI TO 40PSI. CREW FOLLOWED THE QRH AND REDUCED THRUST ON E1, AFTER WHICH IT WAS NOTED THAT THE OIL PRESSURE HAD STABILIZED AT THESDR CA080205007Bearing · worn(CAN) TACH/GEN IDLER ASSY DUAL SPUR GEAR, CENTER ANTI FRICTION BEARING FOUND WITH AN UNUSUALLY HIGH AMOUNT OF RADIAL PLAY AND WAS EXTREMELY ROUGH WHEN TURNED OVER BY HAND. THE ENGINE WAS REMOVED DUE TO CARBON STEEL PLATELETS FOUND IN THE OIL SAMPLE.SDR CA080124005Nut · backed out(CAN) A/C CAME IN TO THE MAINT HANGER DUE TO HAVING A CHIP LIGHT COME ON IN THE COCKPIT. INSP FROM MAINT NOTICED THAT THERE WAS METAL ON THE CHIP DETECTOR OF ENGINE P-54121. AT THAT TIME THE ENGINE WAS FORWARDED TO THE ENGINE SHOP FOR FURTHER INSP. THE ENGINE SDR DL757071588Chip Detector · looseAT CRUISE ALT NR 2 ENGINE OIL PRESS WAS IN THE RED AND HAD A LOSS OF OIL QTY, CREW WENT THRU CHECKLIST AND SHUT ENGINE DOWN. OPENED RT ENG FAN COWL. FOUND NR 5 CHIP DETECTOR NOT COMPLETELY SEATED IN CHIP DETECTOR HOUSING. CREW FILLED OUT LOSS OF FLAME REPORSDR C8GA20070012Helicoil · damagedFLT 708 FROM TOL TO MCI - DURING CRUISE OPERATION AT FLT LEVEL 320, THE NR 3 ENGINE LOW OIL PSI LIGHT ILLUMINATED. OIL QUANTITY WAS OBSERVED TO BE DECREASING FOLLOWED BY A DECREASE IN OIL PSI. THE NR 3 ENGINE WAS SHUT DOWN AND THE AIRCRAFT DIVERTED TO STL WHSDR HCM2007F00002Chip Detector · faultyAPPROX 1 HR AFTER TAKEOFF ON A TOUR FLIGHT, THE ENGINE CHIP LIGHT ILLUMINATED. THE PILOT MADE A PRECAUTIONARY LANDING. UPON INSPECTION BY MAINT, NO METAL WAS FOUND ON THE ENGINE ELECTRICAL CHIP PLUGS OR ON THE ENGINE MAGNETIC PLUGS. SMALL CARBON DEPOSIT WASSDR HEER117772Alternator · failedENGINE WAS REMOVED DUE TO METAL IN OIL. UPON DISASSEMBLY FOUND METAL UNDER PERMANENT MAGNET ALTERNATOR. APPEARS TO BE BEARING FAILURE IN PERMANENT MAGNET ALTERNATOR. PART WILL BE SENT TO VENDOR FOR POSSIBLE REPAIR.SDR CA070911012Stud · dislodged(CAN) DURING CRUISE, THE NR 2 OIL QUANTITY SLOWLY DECREASED TO ZERO. WHEN THE OIL QUANTITY WENT BELOW THE GREEN ARC THE FLIGHT CREW SHUTDOWN THE ENGINE USING THE APPROPRIATE CHECKLIST AND AN EMERGENCY WAS DECLARED INTO AIRFIELD. THE AIRCRAFT LANDED WITHOUT FURSDR A1019131Gear Shaft · fracturedENGINE WAS SENT FOR REPAIR DUE TO GENERATING METAL. UPON DISASSEMBLY FOUND THAT THE SHAFT ON THE FORWARD SIDE OF THE CENTRIFUGAL BREATHER GEAR WAS FRACTURED IN THE AREA OF THE RADIUS WHERE THE SHAFT JOINS THE GEAR. THE RELATIVE MOTION BETWEEN THE SHAFT AND TSDR A101913Gear · fracturedENGINE WAS SENT FOR REPAIR DUE TO GENERATING METAL. UPON DISASSEMBLY FOUND THAT THE SHAFT ON THE FORWARD SIDE OF THE CENTRIFUGAL BREATHER GEAR WAS FRACTURED IN THE AREA OF THE RADIUS WHERE THE SHAFT JOINS THE GEAR. THE RELATIVE MOTION BETWEEN THE SHAFT AND TSDR CA070628003Bolt · failed(CAN) ENGINE S/N PCE 97543 WAS REMOVED SUBSEQUENT TO IN-FLIGHT SHUTDOWN AFTER THE ENGINE OIL PRESSURE DROPPED TO (0) IN FLIGHT. METAL WAS FOUND IN THE OIL FILTER AND RGB DURING GROUND CHECKS PRIOR TO ENGINE REMOVAL. DURING INVESTIGATION DISMANTLE OF THE POWESDR CA070410001Case · cracked(CAN) ON MARCH 28TH/07 IT WAS REPORTED AN OIL LEAK ON NR 2 ENGINE. THE OIL LEVEL WHEN DOWN 2L IN 5.55 HOURS OF FLIGHT TIME. THE PROPELLER ASSY AND THE LT SIDE OF THE ENGINE WAS REPORTED TO HAVE BEING WASHED WITH OIL AND BOTH THEY WERE INSPECTED FOR LEAKAGE. NOSDR QXEA200700442Carbon Seal · unknownPDX FLIGHT NR 2156 EN ROUTE EUG TO SEA, JUST PASSING PDX, CAPTAIN AND FO SMELLED SMOKE, FLIGHT ATTENDANT MENTIONED HAZE IN THE CABIN, ESPECIALLY NEAR THE REAR OF THE AIRCRAFT. RAN APPROPRIATE CHECKLIST. BLEED NR 1 ON AND BLEED NR 2 OFF SEEMED TO CLEAR SMOKE.SDR C8GA20070004Gearbox · leakingFLT 715 FROM HRL TO MEM. DURING CRUISE OPERATION NR 2 LOW OIL PSI LIGHT ILLUMINATED FOLLOWED BY A DECREASE IN OIL PSI AND OIL QUANTITY. PERFORMED APPROPRIATE CHECKLIST AND SHUT DOWN NR 2 ENGINE. AIRCRAFT DIVERTED TO IAH WHERE IT LANDED WITHOUT INCIDENT. POSSDR SA07019Packing · cutCLT - FLT 864 EN-ROUTE TPA TO PIT. DURING CRUISE, AND APPROXIMATELY 50 MILES SOUTH OF CLT, THE FLIGHT CREW REPORTED THAT THE LEFT ENGINE OIL QUANTITY WAS AT 2 QUARTS. OIL PRESSURE WAS FOUND NORMAL. THE FLIGHT DIVERTED TO CLT AND DECLARED AN EMERGENCY. THE SDR HSYA200700001Rotor Shaft · shearedUPON REACHING ALTITUDE THE RT ENGINE LOST OIL AND FUEL PRESSURE AND THE ENGINE SHUTDOWN. THE AIRCRAFT RETURNED TO DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT. THE NR 2 ENGINE WAS REMOVED AND SENT FOR TEARDOWN TO DETERMINE CAUSE OF THE FAILURE. ON TEARDOWN TSDR CA070215002Housing · broken(CAN) ACCESSORY DRIVE HOUSING BOTTOM CASE DRAIN THREADED MOUNTING BOSS DISCOVERED BROKEN. ENGINE REMOVED AND LOANER ENGINE INSTALLED. (TC NR 20070215002)SDR CA070314011Shaft · damaged(CAN) THE ENGINE EXPERIENCED AN UNCOMMANDED POWER REDUCTION IN CRUISE AND WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED ACCESSORY DRIVE TOWER SHAFT DAMAGE. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE DETERMINED. (TC NR 20070314011)SDR CA070209013Gear · damaged(CAN) THE ENGINE FLAMED OUT IN CRUISE. SUBSEQUENT INVESTIGATION REVEALED DAMAGED TOWERSHAFT DRIVE BEVEL GEARS. (TC NR 20070209013)SDR CA070209012Drive Gear · damaged(CAN) THE ENGINE FLAMED OUT ON DESCENT. SUBSQUENT INSPECTION REVEALED DAMAGE TO THE ANGLE DRIVE GEARBOX GEARING. (TC NR 20070209012)SDR WRNA200600041Housing · crackedDURING CRUISE, AT 33,400 FEET, NR 3 ENGINE OIL QUANTITY AND OIL PRESSURE DROPPED RAPIDLY TOWARDS -0- PERFORMED PRECAUTIONARY SHUTDOWN. FLIGHT CONTINUED TO DESTINATION AND MADE A SAFE LANDING. INVESTIGATION REVEALED RADIAL DRIVE LEAKING, REPLACED RADIAL DRIVESDR HCM2007F00000Chip Detector · activatedSHORTLY AFTER TAKEOFF OF A TOUR FLIGHT FROM AIRPORT, THE (ENGINE CHIP) WARNING LIGHT ILLUMINATED. PILOT PERFORMED A PRECAUTIONARY LANDING. INSP REVEALED 1 SMALL METAL SLIVER FOUND ON THE ENGINE FULL FLOW ELECTRICAL CHIP DETECTOR, ALL OTHER ENG DETECTORS INSPSDR CA070115011Planetary Gear · damaged(CAN) UPON DOING A OIL SAMPLE, METAL WAS NOTED IN THE OIL FILTER. THE ENGINE P-63235C WAS REMOVED. ENGINE WAS FORWARDED TO THE ENGINE SHOP FOR INSPECTION OF THE METAL AND FOUND THAT 1 PLANETARY GEAR WITH THE INNER RACE PEELING METAL AND 3 PLANETARY GEARS WITH SDR AALA20061100Gearbox · failedORD APPROXIMATELY 25 MINUTES OUT OF ORD LEFT ENGINE OIL QUANTITY BEGAN TO DECREASE. OIL QUANTITY WENT TO ZERO IN ABOUT THREE MINUTES. OIL PRESSURE SUBSEQUENTLY DECREASED TO ZERO. CREW SHUT LEFT ENGINE DOWN. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. SINSDR AALA20061099Towershaft · brokenRDU - LEFT ENGINE FAILED ON TAKEOFF. NO OTHER INDICATIONS. RETURNED TO RDU AND LANDED WITHOUT INCIDENT. AIRCRAFT TAKEN OUT OF SERVICE FOR EVALUATION. EVALUATION INDICATES BROKEN TOWER SHAFT. GEARBOX DECOUPLED. STARTER SPINS ENGINE 50 PERCENT. REPLACED NSDR 2006FA0001085Bearing · spalledVISIBLE LINE FOUND ON 2.5 BEARING ROLLERS MATCHING SPALLING FOUND ON SAG SHAFT (SDR DATED 3/NOV/2006). GEARBOX INSTALLED 6/SEPT/2006. TIME IN SERVICE FOR GEAR BOX, 105.1 HOURS. 2.5 BEARING INSTALLATION TIMES NUT SHOWN ON ENGINE CARDS. 2.5 BEARING IS A PMA SDR MASA200601964Gearbox · failedASH 7112 DSM - CREW ABORTED TAKEOFF AND RTG. NR 1 ENGINE LOST N2 SPEED WITH A LOW OIL PRESSURE CAUTION ON TAKEOFF ROLL. ENGINE SHUTDOWN UNCOMMANDED. MAINTENANCE REMOVED AND REPLACED AGB AND LUBED SCAVENGE PUMP.SDR DL738060610Gearbox · making metalNR 1 ENGINE SHUTDOWN DUE TO OIL FILTER BYPASS LIGHT ON AND WOULD NOT EXTINGUISH WITH THROTTLE AT IDLE. T/S LT ENG OIL FILTER BYPASS LITE IAW FIM FOUND NO FILTER DEB. REMOVED CHIP DETECTOR AND FOUND METAL ON FWD DETECTOR 537332005. REMOVED AGB IAW ESM 72-SDR DL738060572Gearbox · failedFILTER BYPASS LIGHT FLICKERED THEN BECAME STEADY AT CRUISE THROTTLE WAS RETARDED LIGHT STAYED ILLUM. ENGINE WAS SHUTDOWN PER QRH. REPLACED NR 2 ENGINE ACCESSORY GEARBOX PER ESM 72-00-63. ENG REQUIRES TEST 3B. ENGINE LEAK CHECK AND TEST 3B C/W, NO LEAK NOTESDR 917133O-Ring · cutWHILE IN CRUISE FLT AT FL 340, NOTICED OIL PRESSURE ON RT ENGINE DROP INTO YELLOW. IT CONTINUED TO DROP 1 PSI EVERY 2 TO 4 MINUTES AND EVENTUALLY ENDED UP IN THE RED AT 17 PSI BEFORE SHUTTING ENGINE DOWN ON THE GROUND. OIL TEMP WAS 67 DEGREES C, OIL QUANTITY SDR CA060627004Bearing · failed(CAN) THE FRONT SCAVENGE PUMP DRIVE GEAR SHAFT SHEARED IN THE SCAVENGE PUMP, DUE TO THE SCAVENGE PUMP BUSHING THAT SEIZED FROM OIL STARVATION AND METAL CONTAMINATION CAUSED BY THE TORQUE SENSOR BEARING. THE OIL PRESSURE PUMP SHAFT AND BUSHING ALSO HAVE WEAR ONSDR 2006FA0000679Chip Detector · contaminatedAC EXPERIENCED NR 1 ENG CHIP LIGHT. MASTER CAUTION WAS EXTINGUISHED, LIGHT WENT OUT. ABOUT 2 SECONDS LATER LIGHT CAME BACK ON WITH MASTER CAUTION, WAS AGAIN EXTINGUISHED, WENT OUT THEN CAME BACK ON. PILOT ELECTED RETURN TO BASE. AFTER LIGHT CAME ON AGAIN FSDR UIEA200600121Seal · damagedACCOMPLISHED AIR TURNBACK DUE TO LOSS OF ALL OIL IN ENGINE NR 1, DURING CLIMBOUT. FOLLOWED SHORTLY BY A DROP IN OIL PRESSURE INTO THE MID TO LOWER AMBER BAND. FOUND NR 1 ENGINE HYD PUMP SHAFT SEAL CAVITY LEAKING OIL DURING IDLE RUN. HYD (EDP) PUMP SHAFT SEASDR MASA200601350Gearbox · malfunctionedASH 7005 RDU. CREW COMMANDED NR 2 ENGINE SHUT DOWN DUE TO LOW OIL PRESSURE IN FLIGHT. AC FERRIED TO CLT WHERE MX REPLACED ENGINE AGB.SDR KBM2006F00189Magnetic Seal · leakingENGINE BLOWING OIL OUT OF THE ENGINE GEARBOX VENT LINE. REMOVED AND REPLACED. (K)
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