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 AU990483Gear · wrong part(AUS) ENGINE ACCESSORY GEARBOX 2.5 BEARING INCORRECTLY POSITIONED DUE TO THE INCORRECT FITMENT OF THE HELICAL GEAR. THE GEAR HAD BEEN INSTALLED IN THE REVERSE POSITION. THE GEARBOX HAD JUST BEEN RECEIVED FROM THE OVERHAUL FACILITY FOLLOWING REPAIRS AND WAS BSDR HEED064545Seal · leakingMAG SEAL LEAKS. ORDERED REPLACEMENT.SDR HEED064543Seal · leakingMAG SEAL LEAKS. ORDERED REPLACEMENT.SDR 99ZZZX1914Spacer · failedVISUAL AND BINOCULAR INSPECTION OF THE SPACER REVEALED SOME ENTRAPPED COPPER-COLORED METALLIC DEBRIS IN THE SLOTTED RECESS ON THE SIDE FACE FLAT. FINE GRIT-LIKE PARTICLES WERE ALSO OBSERVED IN THE BORE ANNUAL RECESS. THE ANODIZED SURFACES EXHIBITED A MOTTLESDR AU990430022Housing · cracked(AU) DURING PRE-FLIGHT, A SMALL OIL LEAK WAS DISCOVERED ON NR 2 ENGINE. FURTHER INSPECTION FOUND A 2 INCH CRACK IN THE ACCESSORY GEARBOX HOUSING. THE CRACK IS IN THE BODY OF THE HOUSING, ADJACENT TO THE ACCESSORY DRIVE PAD. THIS IS THE AIR CONDITIONING PADSDR AU990454Bearing · failed(AUS) LEFT ENGINE NR 1 ACCESSORY GEAR BEARING LOCATED IN THE ACCESSORY GEARBOX FAILED.SDR CA990330021Filter · loose(CAN) ON TAKEOFF ROLL, NR 2 ENGINE OIL FILTER BYPASS LIGHT CAME ON FOLLOWED BY OIL QUANTITY AND OIL PRESSURE LOSS. TAKEOFF REJECTED. POST-FLIGHT INSPECTION OF THE GEARBOX FOUND ONE OF THE FOUR HELICOILS THAT HOLD THE OIL FILTER COVER ON, TO HAVE PULLED OUT OSDR MALA976395Chip Detector · contaminatedON CLIMBOUT FROM DTW, THE RIGHT CHIP DETECT LIGHT CAME ON, COMPLIED WITH QRH. ALL ENGINE PARAMETERS WERE NORMAL. AIRCRAFT RETURNED TO DTW. MAINTENANCE FOUND ONE SLIVER HAIR LIKE PIECE ON CHIP DETECTOR. CLEANED CHIP DETECTOR AND SCAVANGE SCREENS. GROUND RASDR 99ZZZX1466Nut · looseDURING STRIP OF THIS SUB-ASSEMBLY, NOTED THERE WAS LITTLE OR NO TORQUE ON THE RETAINING NUT, ALLOWING SHAFT TO SPIN IN RELATION TO THE THRUST BEARING.SDR 99ZZZX1417Housing · damagedTHREADS FOR FITTING OF AFT OIL SCAVENGE PUMP LINE, IN ACCESSORY/GEAR HOUSING, STRIP OUT CAUSING OIL LEAK.SDR CA990308010Gearbox · making metal(CAN) DURING REMOVAL OF THE ALTERNATOR, FERROUS METAL WAS FOUND IN THE ALTERNATOR AREA. THE GEARBOX WAS REPLACED.SDR ASOA99025SDrive Shaft · failedEN ROUTE ATL-CRW AT FL230, THE LEFT ENGINE 'ENGINE CONTROL' AND 'OIL PRESSURE' AURAL WARNINGS CAME ON. CREW NOTED THAT THE OIL PRESSURE, NH AND TORQUE ALL READ ZERO, WITH AN OIL PRESSURE LIGHT ON THE MAP. CREW SHUT DOWN THE LEFT ENGINE, DECLARED AN EMERGENCY, SDR AU990148Seal · failed(AUS) NR 2 ENGINE AUXILIARY GEARBOX OUTPUT SHAFT SEAL LEAKING. ENGINE HAD SUFFERED A PREVIOUS AUXILIARY GEARBOX DRIVESHAFT FAILURE WHICH MAY HAVE CONTRIBUTED TO THE DEFECT.SDR AU990266Bearing · failed(AUS) ENGINE ACCESSORY GEARBOX BEARING FAILED ALLOWING LOSS OF DRIVE TO THE FCU FUEL PUMP AND THE ENGINE OIL PUMP. PART TC: 18,523.SDR RAIA990209Gearbox · failedFLT 7782 - JFK - OIL PRESSURE DROPPED BELOW RED LINE ALONG WITH TORQUE DROP ON RIGHT ENGINE. ENGINE WAS SHUTDOWN IN FLIGHT. MAINTENANCE REPLACED RIGHT ENGINE GEARBOX. (M)SDR DL72S990248Gearbox · leakingON APPROACH INTO CVG PASSING THROUGH APPROX 9000 AGL, NR 2 LOW OIL PRESS LIGHT ILLUMINATED. OIL QTY WAS AND NOW OBSERVED TO DECREASE, OIL TEMP NORMAL, INCREASED ABOVE 105 DEG C. ENGINE SHUT DOWN PER POM PROCEDURES. FOUND NR 2 ENG GEARBOX LEAKING AT 6 O'CLOCSDR R7MA0000579Magnetic Seal · leakingSTARTER SEAL LEAKING ON NR 2 ENGINE. (X)SDR CA990129023Seal · ruptured(CAN) ON FINAL,THE NR 2 ENGINE OIL PRESSURE SHOWED ON THE ECAIS. FOLLOWING THE CHECK LIST, THE NR 2 ENGINE WAS SHUTDOWN. POST-FLIGHT INSPECTION FOUND A RUPTURED RING MATING SEAL ON THE AXIS BETWEEN THE IDG AND THE ACCESSORY GEARBOX, WHICH CAUSED THE LOSS OF SDR 99ZZZX1168Valve · inoperativePILOT REPORTED SMOKE IN CABIN. AIRCRAFT RETURNED TO ITS STARTING POINT (ORF). PROBLEM ISOLATED TO GEARBOX BREATHER VALVE STUCK CLOSED. UNIT REPLACED AND OPERATIONAL CHECK GOOD.SDR CA990125014Gearbox · cracked(CAN) ENGINE OIL WAS VISIBLE ON HI-POWER RUN-UP. INSPECTION FOUND OIL COMING FROM A 0.400 INCH LONG LINE ON THE ACCESSORY GEARBOX . NO VISIBLE CRACK DETECTED. FURTHER REPORT TO FOLLOW. PART TC: 9.SDR CLCA9901Filler · failedFLT 96 - SEQU TO CLO - ON T/OF ROLL AT 0010Z. ON ROUTINE NORMAL T/O AT APPROX 75 KNOTS A/C BEGAN TO MAKE VIOLENT BANGING NOISE AND ABNORM EXTREME SHUDDERING FOLLOWED BY A MODERATE YAW TO THE LT. THE REJECTED T/O PROCEDURE WAS INITIATED AND A/C STOPPED ON RUNSDR PLGA990109Chip Light · illuminatedLGA - FLT 6553 - AFTER TAKEOFF, THE LEFT ENGINE CHP DETECTOR LIGHT ILLUMINATED INTERMITTENTLY. AIRCRAFT RETURNED TO LGA AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED REQUIRED CHIP DETECTOR AND SCAVENGE SCREEN INSPECTIONS PER GE MM AND FOUND NO DEBRIS. SDR VTZA99007Pipe · failedFLT 6247 - IAD-BGM - DURING CRUISE, MADE AN UNSCHEDULED LANDING DUE TO RIGHT ENGINE OIL FLUCTUATION. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED OIL SUCTION LINE. OIL PRESSURE TRANSDUCER AND OIL PRESSURSDR VTZA99006Chip Detector · dirtyFLT 6267 - IAD-BRV - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RIGHT ENGINE OIL CONTAMINATION WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED, CLEANED AND REINSTALLED. MAINTESDR CA990430055Bevel Gear · stripped(CAN) ON CLIMB-OUT AT FL 220, THE NR 2 ENGINE GENERATOR LIGHT CAME ON AND THE ENGINE SURGED, THE ENGINE THEN ROLLED BACK TO IDLE FOR 3-5 SECONDS BEFORE FLAMING OUT. THE ENGINE WAS SECURED AND THE AIRCRAFT DIVERTED. POST-FLIGHT AN ENGINE START WAS ATTEMPTED SDR 99ZZZM38Seal · leakingOIL LEAK FROM RIGHT ENGINE ACCESSORY SECTION. INVESTIGATION AND INSPECTION FOUND FUEL CONTROL UNIT GARLOCK SEAL LEAKING. REPLACED WITH NEW GARLOCK SEAL. (M)SDR 99ZZZM191Gear Box · leakingWHILE CLIMBING THROUGH 1,500 FT OIL QUANTITY GAUGE ON NR 1 ENGINE WAS IDENTIFIED AS LOSING OIL. CLIMBED TO 5,000 (CLEAN CONFIGURATION) DECLARED AN EMERGENCY WITH ATC. TURNBACK TO MIA. ENGINE WAS SHUTDOWN, ALL AOM PROCEDURES COMPLIED WITH. REPLACED GARLOCK SDR 99ZZZM192Gear Box · leakingWHILE CLIMBING THROUGH 13,000 FEET OIL QUANTITY GAUGE ON NR 1 ENIGNE WAS IDENTIFIED AS LOSING OIL. TURNBACK TO MIA, PRIOR TO TURNBACK SWAPPED OIL GAUGES TO VERIFY OIL LOSS. ENGINE SHUT DOWN ALL AOM PROCEDURES COMPLIED WITH. FOUND OIL RETURN LINE TO GEAR BOXSDR CA990115031Bearing · failed(CAN) THE ENGINE HAD AN UNCOMMANDED SHUTDOWN AT 9,000 FEET. THE ENGINE WAS SENT FOR INVESTIGATION AND IT WAS DETERMINED THE ENGINE SHUTDOWN WAS A LOSS OF FUEL FLOW AS A RESULT OF LOSS OF DRIVE TO THE ACCESSORY GEARBOX. THIS WAS A RESULT OF A FAILURE OF THE USDR 99ZZZX536T Drive · leakingENGINE T-DRIVE (THIS UNIT MOUNTS THE ENGINE FUEL PUMP AND PROP GOVERNOR ONTO A SINGLE ACCESSORY PAD) DEVELOPED A LEAK. UNIT REMOVED AND SENT FOR OVERHAUL. UNIT WAS CERTIFIED AND RE-INSTALLED ONLY TO FIND THE GOVERNOR DRIVE GEAR TO BE THE WRONG ONE. UNIT REWSDR CA990219008Seal · worn(CAN) DURING FLIGHT, THE CREW NOTICED A SMALL BUT STEADY DECREASE IN THE OIL QUANTITY ON NR 1 ENGINE. THE AIRCRAFT WAS DIVERTED AND A POST-FLIGHT INSPECTION FOUND THE STARTER DRIVE PAD CARBON SEAL LEAKING. THE CARBON SEAL WAS REPLACED AND GROUND CHECKED SERSDR 99ZZZX336Chip Collector · failedCHIP COLLECTOR ON RIGHT ENGINE, NR 4 BEARING SCAVENGE LINE, CHIP COLLECTOR MAGNETIC PROBE EJECTED FROM CHIP COLLECTOR BODY. ENGINE OIL DRAINED FROM ENGINE IN-FLIGHT. ANALYSIS DETERMINED THE INTERNAL CHECK VALVE OF CHIP COLLECTOR WAS STUCK IN THE OPEN POSITIOSDR CA990311028Shaft · worn(CAN) THE ENGINE WAS MAKING GRINDING SOUND EMITTING FROM THE AGB SECTION. INSPECTION FOUND THE CLIP ON THE STARTER /GENERATOR GEAR SHAFT THAT LOCKS THE IMPELLER TO THE SHAFT WAS NOT INSTALLED IN THE PROPER LOCATION. THE RETAINING RING WAS INSTALLED ON THE WROSDR 98UAL9005916 Oil Pres Tube · crackedNR 1 ENGINE OIL QUANTITY INDICATOR BEGAN TO SHOW GRADUAL LOSS OF OIL EN ROUTE. ELECTED TO LAND AT SYR. *S/D* THE LOSS OF OIL WAS DUE TO A CRACK IN THE NR 6 BEARING OUTER INTERNAL OIL PRESSURE LINE AT THE BRAZE JOINT NEAR THE FIXED FERRULE. THE LINE WAS REPLASDR VTZA98355Chip Detector · activatedFLT 6426 - IAD-DTW - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RIGHT ENGINE OIL CONTAMINATION WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND FOUND FLAKES OF METAL ON CHIP DETECTOR ANDSDR CA981209003Bearing · worn(CAN) DURING CRUISE, 42 MINUTES AFTER TAKEOFF, THE NR 1 ENGINE OIL QUANTITY WAS READ AT 1.75 GALLONS. THE OIL LEVEL HAD BEEN SERVICED TO 4.0 GALLONS PRIOR TO DEPARTURE. DURING THE NEXT 5 MINUTES, THE OIL QUANTITY DECREASED TO 1.25 GALLONS. THE NR 1 ENGINE WSDR 98ZZZX4787Fan · leakingCOWLING FAN STARTED TO LEAK OIL IN OPERATION. INSPECTION UPON DISSASSSEMBLY REVEALED A CRACKED CARBON SEAL. SUBMITTER SUGGESTED CAUSE OF DEFECT AS IMPROPER INSTALLATION. ASSEMBLY PROCEDURES HAVE BEEN REVIEWED TO ENSURE PROPER INSTALLATION.SDR VTZA98324Chip Light · illuminatedFLT 6324 - EWR-IAD - DURING CRUISE, AIRCRAFT MADE UNSCHEDULED LANDING DUE TO RT ENGINE OIL CONTAMINATION WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. AIRCRAFT FERRIED TO LAND. MAINTENANCE INSPECTED AND REMOVED, CLEANED AND SDR VTZA98309Chip Detector · malfunctionedFLT 6510 - IAD-LGA - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RIGHT OIL CONTAMINATION WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED CLEANED AND REINSTALLED CHIP DETECTOR, OPSSDR VTZA98304Chip Light · illuminatedFLT 6175 - IAD-JFK - DURING CRUISE, EXPERIENCED A RIGH ENGINE CONTAMINATION LIGHT. AIRCRAFT DECLARED AN EMERGENCY AND MADE AN UNEVENTFUL LANDING AT JFK. MAINTENANCE CONTROL DISPATCHED MAINTENANCE TO THE AIRCRAFT WHERE THE MAINTENANCE PERSONNEL INSPECTED THE SDR CA980928007Plug · damaged(CAN) NR 3 ENGINE OIL QUANTITY WENT TO ZERO IN-FLIGHT. OIL PRESSURE DROPPED TO 38 PSI, LOW OIL PRESSURE LIGHT ILLUMINATED AND THE ENGINE WAS SHUT DOWN. THE ENGINE MAINTAINED A POSITIVE OIL PRESSURE ABOVE 20 PSI FOR THE DURATION OF THE FLIGHT. POST-FLIGHT TRSDR 98ZZZX3695Housing · crackedHOUSING ASSY ACCESSORY DRIVE P/N 3101836 HAS A CRACK IN THE MOUNTING PAD BOSS. FOUR BOLTS ATTACH THE RT ENGINE MOUNT TO THE BOSS. THE LOWER OUTBOARD BOLT INSERT CRACKED OUT.SDR CA980922002Chip Detector · illuminated(CAN) DURING FIREFIGHTING OPERATIONS, THE CHIP LIGHT ILLUMINATED. AFTER INSPECTION, THE AIRCRAFT WAS RETURNED TO SERVICE. ONE HOUR INTO OPERATIONS, THE CHIP LIGHT AGAIN ILLUMINATED AND THE AIRCRAFT WAS REMOVED FROM SERVICE. A FURTHER REPORT WILL BE SUBMITTESDR AU981532Bearing · brinelled(AUS) NR 1 ENGINE ACCESSORY GEARBOX NR 19 BEARING BRINELLED. METAL CONTAMINATION OF ENGINE OIL SYSTEM. INVESTIGATION ALSO FOUND THE GAS PRODUCER SHROUD WORN FOR APPROXIMATELY 180 DEGREES OF THE CIRCUMFERENCE BY THE GAS PRODUCER WHEEL. PART TC: 566.SDR HEEA0015952Pump Assy · mismanufacturedRECEIVING INSPECTION REVEALED: DEEP CASTING FLAWS BEYOND SERVICEABLE LIMITS IN OIL PUMP ASSY SCAVENGE PORT.SDR PLGA98031ADetector · contaminatedBOS - FLT 4275 - AFTER TAKEOFF, THE LEFT ENGINE CHIP DETECTOR WARNING ILLUMINATED. AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED DETECTOR AND GROUND RAN ENGINE PER GE CMM. ALL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR CA980916013Bearing · failed(CAN) NR 1 ENGINE EXPERIENCED POWER LOSS IN-FLIGHT. TORQUE DROPPED FROM 66 PERCENT TO 33 PERCENT. FUEL FLOW DROPPED FROM 380 TO 280 PPH AND OIL PRESSURE DROPPED TO ZERO. NR 1 ENGINE WAS SHUT DOWN. INITIAL INVESTIGATION ON CAUSE OF POWER LOSS SHOWED A FAILUSDR CA980909024Gearbox · seized(CAN) DURING FLIGHT, THE NR 2 ENGINE OIL PRESSURE DROPPED. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT DIVERTED. POST-FLIGHT INSPECTION FOUND THE GEARBOX SEIZED. THE ENGINE WAS REPLACED.SDR 98ZZZX3715Bearing · roughBEARING ROUGH. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR MALA976170Chip Light · illuminatedRIGHT CHIP DETECT LIGHT CAME ON IN FLIGHT, COMPLIED WITH QRH AND RETURNED TO STW. MAINTENANCE REMOVED RIGHT ENGINE CHIP DETECTOR AND FOUND ONE SMALL SLIVER, CHIP WAS ALLOWABLE. INSPECTED SUMP, NO DEBRIS FOUND. RAN AIRCRAFT, CHECKS GOOD. ALL WORK DONE IAW G
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