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.

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 BApr 30, 1999 · Bell 206B3SDR HEED064545Seal · leakingMAG SEAL LEAKS. ORDERED REPLACEMENT.Apr 27, 1999 · N236X · Bell 230SDR HEED064543Seal · leakingMAG SEAL LEAKS. ORDERED REPLACEMENT.Apr 27, 1999 · N236X · Bell 230SDR 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 MOTTLEApr 27, 1999SDR 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 PADApr 19, 1999 · Piper PA31TSDR AU990454Bearing · failed(AUS) LEFT ENGINE NR 1 ACCESSORY GEAR BEARING LOCATED IN THE ACCESSORY GEARBOX FAILED.Apr 18, 1999 · Frchld SA227DCSDR 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 OMar 18, 1999 · Boeing 72725SDR 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 RAMar 15, 1999 · N402XJ · Saab 340BSDR 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.Mar 8, 1999 · N500E · Gulstm GIVSDR 99ZZZX1417Housing · damagedTHREADS FOR FITTING OF AFT OIL SCAVENGE PUMP LINE, IN ACCESSORY/GEAR HOUSING, STRIP OUT CAUSING OIL LEAK.Mar 1, 1999 · N687HB · Mtsbsi MU2B36SDR CA990308010Gearbox · making metal(CAN) DURING REMOVAL OF THE ALTERNATOR, FERROUS METAL WAS FOUND IN THE ALTERNATOR AREA. THE GEARBOX WAS REPLACED.Feb 19, 1999 · Braero HS7482BSDR 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, Feb 16, 1999 · N275AS · Emb EMB120RTSDR 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.Feb 11, 1999 · Fokker F27MK600SDR 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.Feb 9, 1999SDR 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)Feb 6, 1999 · N557HK · Jetair JETSTM4101SDR 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'CLOCFeb 5, 1999 · N543DA · Boeing 727232SDR R7MA0000579Magnetic Seal · leakingSTARTER SEAL LEAKING ON NR 2 ENGINE. (X)Jan 30, 1999 · N109RX · Agusta A109K2SDR 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 Jan 27, 1999 · Cndair CL6002B19SDR 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.Jan 21, 1999 · N802JW · Lear 35ASDR 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.Jan 12, 1999SDR 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 RUNJan 11, 1999 · N571CA · Boeing 75723APFSDR 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. Jan 9, 1999 · N344BE · Saab SF340ASDR 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 PRESSURJan 5, 1999 · N480UE · Bag JETSTM3201SDR 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. MAINTEJan 4, 1999 · N301UE · Jetair JETSTM4101SDR 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 Dec 28, 1998SDR 99ZZZM38Seal · leakingOIL LEAK FROM RIGHT ENGINE ACCESSORY SECTION. INVESTIGATION AND INSPECTION FOUND FUEL CONTROL UNIT GARLOCK SEAL LEAKING. REPLACED WITH NEW GARLOCK SEAL. (M)Dec 26, 1998 · N860CA · Beech 1900DSDR 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 Dec 24, 1998 · N887MA · Boeing 727225SDR 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 BOXDec 23, 1998 · N887MA · Boeing 727225SDR 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 UDec 22, 1998 · Dhav DHC8*SDR 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 REWDec 22, 1998 · N8945A · Beech C35BEECHSDR 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 SERDec 20, 1998SDR 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 POSITIODec 9, 1998 · N983US · Doug DC932SDR 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 WRODec 8, 1998 · Beech 99SDR 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 REPLADec 3, 1998 · N7443U · Boeing 727222SDR 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 ANDNov 27, 1998 · N332UE · Jetair JETSTM4101SDR 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 WNov 27, 1998 · Boeing 72722SDR 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.Nov 24, 1998SDR 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 Oct 30, 1998 · N306UE · Jetair JETSTM4101SDR 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, OPSOct 17, 1998 · N333UE · Jetair JETSTM4101SDR 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 Oct 3, 1998 · N333UE · Jetair JETSTM4101SDR 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 TRSep 22, 1998 · Boeing 727227SDR 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.Sep 15, 1998 · N423CA · Casa C212CCSDR 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 SUBMITTESep 12, 1998 · Bell 205A1SDR 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.Sep 11, 1998 · Bolkms BK117B2SDR HEEA0015952Pump Assy · mismanufacturedRECEIVING INSPECTION REVEALED: DEEP CASTING FLAWS BEYOND SERVICEABLE LIMITS IN OIL PUMP ASSY SCAVENGE PORT.Sep 4, 1998SDR 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)Aug 31, 1998 · N355BE · Saab 340BSDR 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 FAILUAug 31, 1998 · Dhav DHC8311SDR 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.Aug 25, 1998 · Boeing 75723ASDR 98ZZZX3715Bearing · roughBEARING ROUGH. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.Aug 15, 1998 · N118LF · Bolkms BK117A4SDR 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 GJul 28, 1998 · N142XJ · Saab SF340A
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