Garrett TFE731-3AR
Service difficulty reports · 30
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 engine_model_key = 'TFE7313AR' 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 engine_model_key = 'TFE7313AR' 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 CA151216021Timer · faulty(CAN) AC EXPERIENCED SUDDEN INCREASE IN DRAG AND CONTROL VIBRATION WHILE IN CRUISE FLT AFTER LEAVING ICING CONDITIONS. UPON RETURN TO BASE THERE WAS ICE BUILD UP NOTED ON THE HORIZ L/E. THE STAB HEAT BLANKETS WERE FOUND TO BE IN SERVICEABLE CONDITION, HOWEVER,SDR DBCA2014092600004Connector · dirtyON DEPARTURE THE NR 1 ENG DEEC TRIPPED TO MANUAL MODE. CREW RETURNED & LANDING WAS UNEVENTFUL. DOWNLOADED THE NR 1 DEEC DATA & CONTACTED TECH SUPPORT. REVIEWED DATA DOWNLOAD & RECOMMENDED COMPLYING WITH P2T2 PROBE RESISTANCE CHECK & CLEANING PROBE CONNECTORSDR FJTA14064811Unknown · unknownDURING CRUISE AT FL360, THE CABIN LOST PRESSURIZATION. THE CABIN STOPPED CLIMB AT APPROX 10,500 FT & WOULD NOT RESPOND UP OR DOWN FOR THE DURATION OF THE DESCENT TO 10,000 FT AT WHICH POINT THE CABIN DESCENDED WITH THE AIRPLANE UNTIL LANDING. THE CREW DECIDESDR 9JLA2014043003864Control Quadrant · faultyCREW REPORTED THE THE LT THRUST REVERSER WAS INTERMITTENT OR SLOW TO DEPLOY. TROUBLESHOOTING WAS ABLE TO DUPLICATE THE DISCREPANCY BY APPLYING A SIDE LOAD TO THE ENG POWER LEVER. IT WAS FOUND THAT THE DEPLOY SWITCH IN THE THROTTLE QUADRANT TO BE DEFECTIVE. SDR CA130131005Gyro · failed(CAN) PRIOR TO DESCENT THE FLIGHT CREW REPORTED THE LOSS OF DIRECTION INFORMATION ON THE NR 1 HSI. FLIGHT CONTINUED TO DESTINATION WITH USE OF NR 2 HSI INFORMATION AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCH TO THE ACFT AND PROCEEDED TO TROUBLESHOOTSDR CA111114007Potentiometer · shorted(CAN) CO-PILOTS INSTRUMENT BACKLIGHTING INOPERATIVE. FOUND CO-PILOTS LIGHT DIMMER UNIT INOPERATIVE DUE TO EDGE LIGHTED PANEL, LIGHTING POTENTIOMETER WIPER RUBBING ON INSTRUMENT LIGHT WIRING CAUSING THE LIGHT DIMMER TO SHORT OUT. UPON FURTHER INSPECTION FOUNDSDR CA110621012Line · leakingFLIGHT CREW REPORTED SMELL OF RUBBER AFTER T/O, WHICH WENT AWAY SLOWLY. ACFT INSPECTED AND NO EVIDENCE OF RUBBER SMELL WAS NOTED. FOUND FREON LINE LEAKING -OIL IN BELLY. REPLACED LARGE FREON LINE IN AFT CABIN, PN 5419410-193. SYS SERVICED AND CHECKED SERVICSDR CA090212004Drive Unit · leaking(CAN) FLAP POWER DRIVE UNIT FOUND LEAKING FROM SOLENOID VALVE, THIS IS THE (4TH) UNIT WE HAVE HAD THE SAME FAULT ON, NO SDR WAS SUBMIITTED ON THE PREVIOUS UNITS. THE FIRST UNIT SN 1385P HAD 1217.9 TT WHEN IT STARTED TO LEAK FROM SOLENOID, REPLACED 2008/04/11, SDR 2007FA0000976Rotor · separatedIAW SERVICE BULLETIN TFE731-72-5175. BLADE SEPARATION ON ONE LPT3 BLADE AS LISTED IN TABLE 1 OF S/B 72-5175.SDR DELR200700001Bolt · shearedAFTER REMOVAL OF SAFTY WIRE TO REMOVE BOLT, THE MOUNT BOLT WAS FOUND SHEARED AT THE NECK OF THE BOLT. THREADED SECTION OF BOLT WAS REMOVED WITH AN EASYOUT IAW CHAPTER 5 THIS ITEM IS LIFE LIMITED AT 20,000.00 HOURS.SDR FAA1031001Skin · delaminatedDEBOND AREA APPROX. 7 IN X 7 IN ON THE RT OB ELEVATOR LOWER COMPOSITE SKIN. ELEVATOR WAS SENT TO MFG FOR EVALUATION AND WAS DEEMED (BEYOND ECONOMICAL REPAIR). A LOANER UNIT WAS INSTALLED WHILE NEW/EXCHANGE UNIT PREPARED. REPLACEMENT ELEVATOR INSTALLED ON THISSDR DXTA200501093Pump · failedON TAKEOFF ROLL THE FUEL 2 LOW PRESS LIGHT CAME ON. ABORTED TAKEOFF AT 60 KNOTS. R & R FAULTY FUEL BOOST PUMP WITH OVERHAULED UNIT IAW HAWKER 800XP MM CHAP 28-20-12. LEAK & OPS CHECK SATISFACTORY. REMOVED LT & RT FUEL FILTERS P/N 897830-1 AND INSTALLED NEW LSDR CA051103009Actuator · inoperative(CAN) AFTER T/O AND UPON GEAR RETRACTION, NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. MULTIPLE GEAR SELECTIONS HAD NO EFFECT. CREW ELECTED TO CIRCLE FOR ABOUT AN HOUR TO BURN OFF FUEL BEFORE RETURNING TO BASE. MAINT WAS ABLE TO CONFIRM SNAG, RECTIFY BY BLEESDR 31177050304Pump · failedDURING DESCENT FROM CRUISE, RIGHT ENGINE FLAMED OUT. ENGINE WAS SUCCESSFULLY RESTARTED. DIVERTED TO KBDL. REPLACED RIGHT ENGINE FUEL PUMP DUE TO LOW PRESSURE. REPLACED RIGHT ENGINE FUEL CONTROL DUE TO METAL CONTAMINATION IN STRAINER BETWEEN FUEL PUMP AND FSDR DJFA2004004Regulator Valve · failedDURING THE CLIMB THE PILOTS NOTICED THE NR 3 ENGINE OIL PRESSURE LIGHT ILUMINATED. OIL PRESSURE WAS DESCENDING THREW 25 PSI. AT THAT POINT THE PILOTS SHUT DOWN THE NR 3 ENGINE AND RETURNED TO THE DEPARTURE AIRPORT.SDR DJFA2004003Regulator Valve · failedDURING THE CLIMB THE PILOTS NOTICED THE NR 3 ENGINE OIL PRESSURE LIGHT ILLUMINATED. OIL PRESSURE WAS DESCENDING THREW 25 PSI. AT THAT POINT THE PILOTS SHUT DOWN THE NR 3 ENGINE AND RETURNED TO THE DEPARTURE AIRPORT.SDR DXTA200300132Compressor · damagedAT FLIGHT LEVER 370, NR 1 ENGINED EXPERIENCE A LOUD BANG WITH ITT SPIKING AT 1016 DEGREES WITH AIRFRAME VIBRATION. N1 AND N2 ROSE, ITT THEN FELL TO 450 DEGREES WITH N1 AND N2 DROPPING. SHUT DOWN ENGINE. TROUBLESHOT NR 1 ENGINE FOUND THE LOW PRESSURE COMPRESSOSDR T0DR200300002Fairlead · brokenRUDDER JAMMED UPON ROTATION. (RUDDER SYS JAM) CHECKLIST. ALL KNOWN SYSTEMS SUSPECTED OF HAVING BRG ON RUDDER SYS. ALL OTHER FLIGHT CONTROL SYS OPERATED NORMALLY AND AC CONTROL WAS NEVER IN DOUBT. EMERG WAS DECLARED, 2 TOWER FLY-BYS WERE EXECUTED TO ALLOW TOSDR 3298SBlade · missing3298S- AIRCRAFT EXPERIENCED VIBRATION IN FLIGHT. NR 2 ENGINE WAS SHUTDOWN IN-FLIGHT. AIRCRAFT ARRIVED SAFETLY. VISUAL INSPECTION OF NR 2 ENGINE REVEALED A 1.0 TO 1.5 INCH PIECE OF 1EA 3RD STAGE TURBINE WHEEL BLADE WAS MISSING. ENGINE WAS SWAPPED WITH A LOASDR R5XR2000003Housing · misoverhauledWHILE PERFORMING MODIFICATION TO 70821, THE EDM PROCEDURE BROKE THROUGH THE WALL OF THE HOUSING DUE TO ERROR IN SETUP OF EDM MACHINE.SDR R5XR2000004Housing · misoverhauledWHILE PERFORMING MODIFICATION TO 70821, THE EDM PROCEDURE BROKE THROUGH THE WALL OF THE HOUSING DUE TO ERROR IN SETUP OF EDM MACHINE.SDR 032031Restrictor Valve · bypassingMAIN ACCOMPLISHED PREFLT INSP AND THEN PILOTS PROCEEDED TO DO THEIR PREFLT INSP. UPON NORMAL EXTENSION OF SPEED BRAKE PANELS, THEY RETRACTED WITH HIGH SPEED AS THOUGH SWITCHES WERE IN THE "GROUND AUTO DEPLOY" POSITION. DISASSEMBLLY OF RESTRICTOR VALVE SHOWEDSDR 032031ARestrictor Valve · bypassingDURING PREFLT INSP, MAINT CREW NOTED THAT SPOILERS FULLY DEPLOYED IN LESS THAN 1 SECOND WITH SPOILER SWITCHES SET TO "IN-FLT" MODE. NORMAL DEPLOY TIME IN THIS MODE IS 6-10 SECONDS WHEREAS "GROUND AUTO-DEPLOY" MODE FOR LANDING IS LESS THAN ONE SECOND. IN PROCSDR CA030218012Terminal Block · overheated(CAN) MFG DESIGN FLAW, INSTRUMENT LIGHTING SYS WAS DISCOVERED WHEN NEW AIR DATA DISPLAY UNIT WAS INSTALLED FOR RVSM UPGRADE. SYMPTOM WAS ADDU LIGHT WOULD GO INTO NIGHT MODE (VERY DIM) WHEN EMER BATT PACK WAS TURNED ON. PACK IS KEPT ON IN FLIGHT TO RUN STANDBYSDR ROCK012303Switch · inoperativePILOT'S TRIM SWITCH BECAME INTERMITTENT AND THEN FAILED TO OPERATE COMPLETELY IN FLIGHT. CO-PILOT AND ALTERNATE TRIM SYSTEMS BOTH REMAINED FUNCTIONAL. TESTED AND REPLACED PILOT'S TRIM SWITCH AT DESTINATION. SYSTEM FUNCTIONED PROPERLY AFTER REPLACMENT OF SWISDR 778Control Cable · brokenNR 1 ENGINE TELEFLEX CABLE BROKE INSIDE ITS HOUSING MAKING IT IMPOSSIBLE FOR THE PILOTS TO HAVE CONTROL OF THE ENGINE AS FAR AS MAKING CHANGES TO THE SPEED AND FOR SHUTTING THE ENGINE DOWN IN THE NORMAL MANNER. THE PILOTS SHUT THE ENGINE DOWN USING THE FIREWALSDR 029041702Line · crackedPILOTS STARTED TAXI OUT TO TAKEOFF. IN PROCESS CONDUCTED THE LANDING SPOILER EXTENSION OPERATIONAL TEST WHICH SURGES AND SLAMS THE HYDRAULIC SYSTEM FAIRLY HARD. WITHIN A FEW SECONDS RECEIVED MASTER WARNING CAUTION LIGHT AND NOTICED LOW HYDRAULIC PRESSURE. SDR APJ2002F00000Oil Cap · not seatedAPPROXIMATELY 1.5 HOURS INTO FLIGHT AT 35,000 FT THE OIL PRESSURE GAUGE FLUCTUATED FOR THE RIGHT SIDE ENGINE AND PROCEEDED TO INDICATE MINIMUM PRESSURE. AS A PRECAUTION, THE PIC SHUTDOWN THE RIGHT SIDE ENGINE WHEN THE OIL PRESSURE REACHED 25 PSI (MINIMUM PRESSDR 20010320CW007Control Unit · malfunctionedON APPROACH, LANDING GEAR WAS LOWERED AND CDS MESSAGE LEFT AND RIGHT INBOARD BRAKE FAILED. CONTINUED WITH NORMAL CHECKLIST. THE AMBER MESSAGE WAS REPLACED BY A WHITE MESSAGE. RETURNED TO BASE AND DOWN LOADED COMPUTER SYSTEMS, OPERATED NORMAL. SENT FINDINGS SDR CA000511046Seat Back · cracked(CAN) PILOTS SEAT BACK REST FOUND CRACKED.
Back to Garrett TFE731-3AR