Garrett TFE731-5R
Service difficulty reports · 108
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 = 'TFE7315R' 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 = 'TFE7315R' 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 2022FA0000279None · noneDURING CLIMB PASSING FL 355 THE "CABIN ALTITUDE" LIGHT CAME ON WITH DIFFERENTIAL PRESSURE INDICATOR SHOWING ZERO. CABIN DID NOT LOSE PRESSURIZATION; HOWEVER THE CREW FOLLOWED THE CHECKLIST DECLARED EMERGENCY, DESCENDED TO LOWER ALTITUDE AND RETURNED TO THE DEPSDR 2021F00032Oil System · fluctuatesAFTER DEPARTURE FROM KJVL DURING CLIMB OUT THE CREW NOTICED THE RH ENGINE OIL PRESSURE FLUCTUATING. THE CREW FOLLOWED CHECKLIST PROCEDURES AND SHUT THE ENGINE DOWN AS A PRECAUTION.SDR 2019FA0000330Relay · malfunctionedDURING POST MAINTENANCE FUNCTIONAL CHECK, FOUND LH OIL PRESSURE INDICATOR LIGHT TO NOT ILLUMINATE DURING CHECK (PUSH TO TEST CHECK GOOD). MECHANICS FOLLOWING MAINTENANCE TECHNICAL DATA CHECKED BULBS, AND SD CARD PER INSTRUCTIONS. AFTER FURTHER TROUBLESHOOTING,SDR G73R201808225587Cabin Pressure · malfunctionedDURING CRUISE AT FL360, WITH CABIN CONTROLLER SET TO FL380 AND NORMAL PRESSURIZATION. AT TOP OF DESCENT REDUCED POWER SLIGHTLY AND AT THE SAME TIME THE CABIN RATE KNOB TURNED TO MIN AND CABIN CONTROLLER MOVED SLIGHTLY TOWARD FIELD ELEVATION. WITHIN SECONDS SDR ZP7A2016F00039Fuel Control · defectiveAT FL400, ENGINE NR 2 BEGAN LOOSING POWER, N1 REDUCED TO BELOW 60 PERCENT, DESCENDED TO 14,000 FT N1 REDUCED TO BELOW 40 PERCENT. AT BELOW 8000 FT MSL ENGINE POWER BECAME FULLY RESPONSIVE.SDR JLTA20150824001Engine · malfunctionedON FRIDAY, AUGUST 21ST AT APPROX 1900Z, ACFT DEPARTED EMPTY & ENTERED CRUISE, EVERYTHING WAS NORMAL. ON THE INITIAL DESCENT CREW HEARD A STRANGE NOISE & OBSERVED AN ENG COMPUTER LIGHT FOR THE NR 2 ENG. ALL OF THE INSTRUMENTS FOR THE NR 2 ENG THEN FLUCTUATED SDR 9JLA201506247566Controller · defectiveCREW REPORTED THAT DURING FLIGHT THE RT ENG DEEC LIGHT CAME ON AT 86% N1. THE CREW INDICATED THAT THE ENG DIVERTED TO MANUAL MODE. TROUBLE SHOT THE DISCREPANCY & FOUND THAT THE ENG SYNC CONTROLLER WAS DEFECTIVE. THE UNIT WAS R & R WITH AN EXCHANGE UNIT PN 2SDR CA150113022Tube · leaking(CAN) POST ARRIVAL, FLIGHT CREW CONDUCTED POST FLIGHT INSPECTION OF ACFT AND NOTED SIGNIFICANT OIL LEAKAGE ON LT ENGINE COWLINGS, NO INFLIGHT INDICATIONS WERE EVIDENT TO FLIGHT CREW DURING APPROXIMATE 4.5 HR FLIGHT. OIL LEVEL COULD NOT BE SEEN THROUGH OIL TANKSDR 2014FA0000506Indication Sys · failedFAILURE OF RT MLG INDICATION WHEN GEAR SELECTED DOWN FOR LANDING.SDR CA140407014Wire Harness · chafed(CAN) FLIGHT CREW REPORTED LANDING GEAR SELECTOR WOULD NOT MOVE AFTER TAKEOFF. CHECKLIST CARRIED OUT AND FLIGHT CREW DECIDED TO RETURN TO AIRPORT AFTER CIRCLING SUFFICIENT TIME TO LOWER FUEL WEIGHT TO OBTAIN PROPER LANDING WEIGHT. ACFT LANDED WITHOUT INCIDENTSDR VIBR20131202001Stud · unsecureENGINE STARTER GENERATOR "B" STUD NOT SECURE IN STARTER GENERATOR TERMINAL BLOCK.SDR 9JLA2012073106330Computer · defectiveCREW REPORTED THE LT ENGINE DEEC LIGHT COMES ON STEADY IN FLIGHT. THE ENGINE COMPUTER WAS REMOVED. A NEW COMPUTER WAS INSTALLED. FUNCTIONAL CHECKS WERE SATISFACTORY.SDR DXTA2012042004955Cap · looseWHILE ENROUTE AT 39000 FT, NOTICED RT ENGINE OIL PRESSURE TURN YELLOW & BOUNCE FROM 55 TO 57 PSI FOR APPROX 5 SECONDS. DROPPED TO 53-55 PSI FOR APPROX 5 TO 10 SECONDS. PRESSURE DROPPED TO 48 PSI. SHUTDOWN RT ENGINE. SINGLE ENGINE LANDING WAS MADE. OIL WASDR 2012F00067Transducer · inoperativeON THE LAST LEG OF THE TRIP, ON START UP, THE RT ENGINE COMPUTER INOPERATIVE LIGHT ILLUMINATED. FOUND BAD N2 TRANSDUCER. REPLACED THE TRANSDUCER, OPS CHECKED GOOD.SDR L7OA2012F00066Fuel Sys · leakingON CLIMB OUT, NOTICED FUEL COMING FROM THE LT WING VENT AREA. ACFT RETURNED TO DEPARTURE WITHOUT INCIDENT.SDR DXTA2011100304738Fuel Control · malfunctionedAT CRUISE ALTITUDE, NR 2 ENGINE COMPUTER MM ANNUNCIATOR ILLUMINATED. ENGINE POWER CHANGED ON ITS OWN AT THAT MOMENT. CHECKLIST ITEMS COMPLIED WITH AND NR 2 ENG COMPUTER SWITCH SELECTED IN OVERSPEED PROT MODE. NORMAL LANDING MADE. PERFORMED ENGINE DEEC DOWNSDR 9JLA20110801001Pump · defectiveTHE CREW REPORTED DURING CLIMBOUT THAT THE ENG 2 FUEL ANNUNCIATOR ILLUMINATED. THE FUEL FILTER HAD BEEN REPLACED 2 DAYS PRIOR WITH SATISFACTORY OPERATIONAL CHECKS. TROUBLSHOOTING FOUND THAT THE ENGINE DRIVEN FUEL PUMP WAS DEFECTIVE. P/N 3070850-57 S/N 396995SDR V0JA041176HOil System · low pressureDURING TAXI TO RUNWAY THE CREW WAS ALERTED TO LOW OIL PRESSURE IN THE NR 1 ENGINE BY THE MWS ANNUNCIATORS. THE LOW OIL PRESSURE WAS VERIFIED BY THE NR 1 ENGINE OIL PRESSURE GAUGE AND THE ENGINE WAS SHUTDOWN FOR PRECAUTIONARY MEASURES. TECH WAS CALLED IN TO TSDR CA110209019Pipe · crackedDURING REMOVAL OF THE ENGINE FOR INSP, IT WAS NOTED THAT THE PORTION OF PIPE EXTENDING PAST THE WELD LINE ON THE INNER SURFACE OF THE AFT COUPLING OF THIS TUBE HAD BEEN CRACKED AWAY. THERE WAS NO INDICATION OF CRACKING ON THE OUTER SURFACE OF THE PIPE, ONLY OSDR CA110209021Outflow Valve · crackedDURING INSP OF THE REAR PRESSURE BULKHEAD, THE FLAPPER VALVES ON THE MAIN CABIN NON RETURN VALVE WERE FOUND TO BE STUCK IN THE OPEN POSITION. FURTHER INSP REVEALED THAT THE CTR SHAFT HAD TOOLING MARKS ON IT AND THE SHAFT WAS CRACKED. THE SPRINGS THAT FORCE THESDR CA110209022Diaphragm · corrodedAFTER REMOVAL OF THE VENTRAL FUEL TANK FOR ROUTINE INSP, CORROSION WAS FOUND 1" BELOW FUEL FILLER AT 7 O`CLOCK POSITION. DURING CORROSION REMOVAL, IT WAS FOUND THAT IT HAD PROPAGATED ENTIRELY THROUGH THE AFFECTED AREA OF DIAPHRAGM 9.SDR CA110209024Wire · burnedDURING INSP, IN THE AFT EQUIPMENT BAY, THE ENTIRE LENGTH OF THE ABOVE MENTIONED WIRE WAS FOUND BADLY BURNED. 50 PERCENT OF THE WIRE INSULATION HAD BEEN MELTED OFF AND THE SURROUNDING WIRING HAD VISIBLE SCORCH MARKS THIS WIRE WAS USED AS THE GROUND FOR A NR OF SDR CA110209026B-Nut · crackedDURING INSP, A CRACK IN THE B-NUT ATTACHED TO THE SEQUENCE VALVE IN THE LT LANDING GEAR WELL AS NOTED. THE CRACK WAS RUNNINQ PERPENDICULAR TO THE THREADS OF THE NUT. THERE WERE NO PREVIOUS REPORTS OF HYD FLUID LEAKAGE.SDR CA110209028Nut · crackedDURING REMOVAL OF THE VENTRAL FUEL TANK, THE ABOVE MENTIONED NUT WAS FOUND TO BE SEIZED IN PLACE. 2 CRACKS WERE NOTED ON THE OUTER SURFACE OF THE NUT: 1 PERPENDICULAR TO THE DIRECTION OF THE THREADS. AFTER DISASSEMBLY, SEVERE CORROSION OF THE THREADED PORTIONSDR CA110209031Frame · cracked(CAN) DURING 24 YEAR INSP, A CRACK IN THE TOP CTR MEMBER OF THE LOWER PRESSING WAS FOUND.SDR CA110209027B-Nut · cracked(CAN) DURING INSPECTION A CRACK IN THE B-NUT ATTACHED TO THE SEQUENCE VALVE IN THE LT LANDING GEAR WELL AS NOTED. THE CRACK WAS RUNNING PERPENDICULAR TO THE THREADS OF THE NUT. THERE WERE NO PREVIOUS REPORTS OF HYDRAULIC FLUID LEAKAGE.SDR CA101116017Power Supply · overheated(CAN) STROBE POWER SUPPLY CAPACITOR OVERHEATED AND MELTED INSULATION RESIN CAUSING ODOR AND EYE IRRITATION TO PASSENGERS. OPEN CIRCUIT TO ONE OF THE THREE STROBE OUTPUT CIRCUITS CAUSED AFFECTED CAPACITOR TO OVERHEAT BECAUSE OF INABILITY TO DISCHARGE. THE CONSDR 2010F00225Annunciator · activatedCREW REPORTED THE "ENG 1 FUEL" ANNUNCIATOR ILLUMINATED DURNING FLIGHT.SDR 2010F00226Annunciator · activatedCREW REPORTED THE "ENG 2 FUEL" ANNUNCIATOR ILLUMINATED DURING FLIGHT.SDR CA100106005Steering Sys · failed(CAN) NOSE WHEEL STEERING UNSERVICEABLE AFTER LANDING NOSE WHEEL STEERING SYS INSPECTED AND LUBRICATED AND FUNCTION TESTED IAW MM 32-50-00. SYS OPS CHECK OK. FAULT DID NOT DUPLICATE.SDR CA100104004Terminal · burned(CAN) PILOTS REPORTED SMOKE IN THE COCKPIT. FIRST REPORTS THAT SMOKE CAME FROM THE INSTRUMENT PANEL. UPON INSP, FOUND LT WINDSHEILD C/B PN 6TC14-10. TERMNIAL A1 WAS BURNED AND DAMAGE TO THE WIRE.SDR CA090909002Seal · leakingNLG ACTUATOR SEAL FAILED OVER NIGHT WHILE ACFT WAS SITTING IN HANGAR. A LARGE AMOUNT OF HYD FLUID LEAKED, REQUIRING REPLACEMENT OF NOSE GEAR TIRES.SDR CA090506009Bearing · binding(CAN) FOUND 2 BEARINGS IN ENGINE ACCY GEARBOX INTERMITTENTLY BINDING, STARTER GENERATOR DRIVESHAFT OFF BEARING (PN 3072885-1) AND OIL PUMP DRIVESHAFT FWD BEARING (PN 3072885-1) . REPLACED STARTER GEN DRIVESHAFT FWD BEARING (PN 3072883-1) AS A PERCAUTIONARY MESDR 2009FA0000257Engine · damagedPILOT REPORTED THAT THE RT ENGINE LOST OIL PRESSURE AND RPMS. NO N1 INDICATION. ENGINE WAS SHUT DOWN AND ACFT RETURNED TO DEPARTURE.SDR CA090225011Diode · shorted(CAN) PILOT REPORTED SMOKE COMING FROM UNDER COPILOTS SEAT, WITH BATTERY SWITCHED OFF AND MASTER REFUEL PANEL POWERED ON. MASTER REFUEL VALVE WAS OPEN, MAIN FUEL VALVES WERE OPEN. OCCURENCE OCCURED WHILE ACFT WAS PARKED ON GROUND. MX ACTION REMOVED SHORTED DSDR CA081104001Hose · leaking(CAN) PILOTS REPORTED LOSS OF HYD PRESSURE AFTER LANDING WHILE TAXING BACK TO AMO. ON INSP, FOUND IN THE RT GEAR WELL A FLEX HYD LINE INSTALLED WITH A SLIGHT TWIST ON IT. THE LOCKWIRE ON THE B-NUT WAS LOOSE, AND THE TWIST ON THE HYD LINE AIDED IN ALLOWING THESDR CA081021006Jackscrew · frozen(CAN) CREW REPORT THE ELEVATOR TRIM WAS DIFFICULT TO MOVE IN FLIGHT. UPON INSPECTION BY MX IT WAS FOUND THE ACTUATOR WAS CORRODED INTERNALLY AND THE GREASE WAS CONTAMINATED AND HARDENED. HAWKER BEECHCRAFT ALREADY HAS SB 27-3840 R1 TO CHECK FOR THIS SAME ISSUE SDR DGC2008F00002Line · crackedAT CRUISE FLIGHT, AFTER 1 HR 27 MIN INTO FLIGHT, THE LT OIL PRESSURE INDICATOR FLUCTUATED FROM APPROXIMATELY 42-45 PSI DOWN TO 30-35 PSI TWICE PER SECOND CONTINUOUSLY. OIL TEMP REMAINED NORMAL, ALL OTHER ENGINE INDICATIONS NORMAL, (N1, ITT, N2). APPROXIMATELY SDR 2008FA0000382Regulator · damagedRECEIVED O/H OIL TEMP REGULATOR FROM MFG UNDER THEIR WO 815978-001, DATED 04/22/2008. WHILE PERFORMING INCOMING PARTS INSPECTION ON 04/24/2008, FOUND FUEL INLET PORT SMASHED. THERE WAS NO DAMAGE TO THE SHIPPING CONTAINER. PROBABLE CAUSE OF DAMAGE WAS MOST LSDR DXTA200802843Unknown · odorELECTRICAL BURNING ODOR FROM BEHIND OR UNDER COPILOTS SEAT. POWERED UP AC SYS USING THE APU AND BOTH ENGS, SELECTED FULL HOT ON TEMP SELECTOR, RADIO MASTER ON, ENG ALTERNATOR'S ON WINDSCREEN HEAT ON AND COCKPIT AND CABIN LIGHTS ON OPERATED ALL SYS FOR 1 HR WITSDR DXTA200802839Unknown · odorBURNING ELECTRICAL AND RUBBER ODOR FROM BEHIND CO-PILOTS SEAT. ON ENTERING CABIN THE ONLY ODOR NOTED WAS THAT OF NEW INTERIOR. ACCESSED THE DA PANEL AND OPENED SUB PANELS DA/A (CB PANEL BEHIND CO-PILOT) DA/B (RELAY PANEL BEHIND CO-PILOT), DA/J (A/C ELECTRICAL SDR DXTA200802834Outflow Valve · inoperativeAFTER T/O LT MAIN AIR VALVE LIGHT CAME ON AND CHECKLIST CALLS TO RECYCLE CLOSED/OPEN. LIGHT CAME BACK ON. REPLACED LT MAIN AIR VALVE WITH O/H UNIT. OPS AND LEAK CHECKED GOOD IAW MM 21-16-25.SDR DELA200700009Fuel Filter · unknownENG 2 FUEL LIGHT. ABORTED TAKEOFF DUE TO ENGINE 2 FUEL LIGHT ON. REPLACED FILTER WITH NEW, PERFORMED GROUND ENGINE RUN, NO LEAKS NOTED, (ENG 2 FUEL) ENUNCIATOR DID NOT ILLUMINATE.SDR CA071126007Computer · inoperative(CAN) ENGINES FRESH, NEW INSTALLATION OF DEECS ON AC. DEEC PROBLEMS OCCURRED. THE PROBLEM ENCOUNTERED WITH DIGITAL ENGINE COMPUTERS (DEEC). (TC NR 20071126007)SDR CA071016021Float Valve · stuck(CAN) DURING REFUELLING USING SINGLE-POINT SYS & FILLING BOTH MAIN (WINGS) & VENTRAL TANK. AS VENTRAL TANK REACHED 1.5 TO 3 QUARTERS CAPACITY FUEL WOULD FLOW THROUGH VENT SYS INTO LT SURGE TANK & SHUTDOWN BY CLOSING MAIN VALVE. COMPLETION OF REFUELLING COULD OSDR CA070827003Seal · deteriorated(CAN) UPON CLIMB OUT WITH CABIN DIFFERENTIAL PRESSURE APPROACHING APPROXIMATELY 6 PSI, A DISTINCT AUDIABLE DISCERNING NOISE WAS HEARD FROM THE CENTER AREA OF THE CABIN. DURING DESCENT WHERE CABIN DIFFERENTIAL PRESSURIZATION FELL BELOW 6 PSI, NOISE WOULD SUBSIDSDR DJFA2006337Hsi · burnedDURING PREFLIGHT, RT HSI WAS FLICKERING ON AND OFF THEN SMOKE STARTED BELLOWING OUT FROM UNDER THE WHOLE INSTRUMENT PANEL. COCKPIT FILLED WITH SMOKE IN SECONDS. FOUND THE RT EHSI TO BE THE CAUSE OF THE SMOKE. INSTALLED A KNOWN GOOD UNIT AND FUNCTIONALLY CHESDR AOQ2006F00003Switch · intermittent(REF NR: ON 800FH101706JC) AFTER TAKEOFF, COULD NOT RAISE LANDING GEAR. INSPECTED LANDING GEAR. FOUND LEFT WEIGHT ON WHEELS SWITCH TO BE INTERMITTENT. REPLACED LEFT MAIN GEAR WEIGHT ON WHEEL MICROSWITCH. ACCOMPLISHED SEVERAL GEAR SWINGS WITH SATISFACTORY SDR COZ2006F00000Display · unreliableAT FLIGHT LEVEL 34 K, FLIGHT CREW ENCOUNTERED STATIC BUILD UP IN THE COMM SYSTEM. IT WENT AWAY SHORTLY FOLLOWED BY AUTOPILOT DISCONNECTING AND PRIMARY DISPLAYS BECAME UNRELIABLE. THE AIRCRAFT LANDED SAFELY. ON THE GROUND, FLIGHT CREW POWERED DOWN THE AIRCRSDR RU32006F00002Landing Gear · malfunctionedGEAR HANDLE WOULD NOT MOVE TO UP POSITION. AC LANDED WITH GEAR LEFT IN DOWN POSITION. OVERWEIGHT LANDING INSPECTION REQUIRED. VISIBLE PRECIP. ICING PREVAILED ON GROUND AT T/O AND AT LEVEL OFF ALT OF 5000MSL. CLEANED SELECTOR LEVER AND MICROSWITCH IN NOSE
Back to Garrett TFE731-5R