Garrett TFE731-5BR
Service difficulty reports · 328
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 = 'TFE7315BR' 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 = 'TFE7315BR' 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 9PVA2012F00176Pump · defectiveAFTER LEVEL OFF AT FL380 AND APPROX 18 MINUTES INTO THE FLIGHT THE "ENG 1 FUEL" CAUTION LIGHT ON THE OVERHEAD PANEL ILLUMINATED, INDICATING "EITHER FUEL FILTER BLOCKED OR FUEL OVERHEAT" IAW THE AIRPLANE FLIGHT MANUAL THE NR 1 ENGINE THRUST LEVER WAS REDUCED TOSDR DXTA2012082005098Master Cylinder · failedPILOT'S SIDE RT BRAKE PEDAL DEPRESSES ALL THE WAY TO THE STOP. ONLY MINIMAL PRESSURE SHOWING ON THE GUAGE. NO BRAKING AVAILABLE FROM RT PEDAL. FOUND PILOTS RT MASTER CYLINDER LEAKING. R & R PILOTS RT MASTER CYLINDER, BLED MASTER CYLINDER AND RT BRAKE SYS IASDR DXTA2012081005084Brake · weakRIGHT BRAKE IS SPONGY, COMPARED TO THE LEFT. BLED RIGHT BRAKES INBD AND OTBD IAW AMM 32-40-00. OPS CHECKED GOOD.SDR DXTA2012080205073Connector · backed outAFTER SELECTING GEAR DOWN, ONLY THE 2 MAIN GEAR LIGHTS WERE GREEN. NOSE GEAR HAD NO GREEN OR RED LIGHTS. NOSE GEAR PIN WAS UP (INDICATING GEAR DOWN). LIGHTS TESTED NORMAL. AFTER ABOUT 10 SECONDS. NOSE GEAR INDICATED GREEN WITH NO RED. ALL OTHER INDICATIONSDR 9JLA2012073103534Sensor · defectiveTHE CREW REPORTED THAT DURING THE POST FLIGHT CHECKS, THE STALL CHANNEL 1 AND 2 WILL NOT IDENT. TROUBLESHOOTING IDENTIFIED THE F3 FUSE AS BEING OPEN BECAUSE OF HIGH RESISTANCE IN THE RT AIRFLOW SENSOR PN 1703-12, SN 1569. THE AIRFLOW SENSOR AND THE FUSE WERE RSDR 2012FA0000440Valve · noisyDURING TAKEOFF AND CRUISE, THE FUEL BOX VALVE MAKES AN UNUSUAL BUZZING NOISE WHICH CAN BE FELT IN THE CABIN. SERVICE AD FSA 900/28-00/01 ADDRESSES THIS ISSUE.SDR 2012FA0000441Valve · vibrationPRIOR TO THE INSTALLATION, VALVE UNIT WAS BENCH TESTED AND AN UNUSUAL NOISE/VIBRATION WAS NOTICED. SERVICE AD FSA 900/28-00/01 ADDRESSES THIS ISSUE.SDR 2012FA0000472Valve · noisyDURING TAKEOFF AND CRUISE, THE FUEL BOX VALVE MAKES AN UNUSUAL BUZZING NOISE WHICH CAN BE FELT IN THE CABIN. FSA 900/28-00/01 ADDRESSES THIS ISSUE. BEING THAT MFG IS UP TO A SERIES 1006 FROM THE 1002. IT WOULD APPEAR THAT THE MFG IS STILL WORKING ON AN INHESDR DXTA2012073105070Skin · corrodedTOP OF RT WING HAS CORRODED FASTENERS. REMOVED ALL FASTENERS AFFECTED BY CORROSION AND BLENDED ALL AREAS OF VISIBLE CORROSION ON THE RT UPPER WING SKIN SURFACE. PERFORMED NDT INSPECTIONS FOR CORROSION REMAINING AND REMAINING MATERIAL THICKNESS AT ALL BLENDEDSDR Y9PA2012062800001Rudder Control · obstructedDURING PREFLIGHT, NOTICED THE RUDDER WAS DEFLECTED FULL RIGHT AND WAS BINDING. DURING INVESTIGATION FOUND INCORRECT HARDWARE IN COCKPIT FLOORBOARD ABOVE RUDDER GUSTLOCK BELL CRANK. DHS1426-1-2D IS THE CORRECT HARDWARE FOR THE FLOORBOARD, FOUND AN3-9 BOLTS INSDR CA120614003Downlock Switch · contaminated(CAN) ON FINAL APPROACH, CREW SELECTED GEAR DOWN, THEY HAD NO INDICATION LIGHTS ON GEAR ANNUNCIATOR PANEL. ALL RT DIM ANNUNCIATOR LIGHTS WERE INOPERATIVE ON COPILOT SIDE. ACFT DID A GO AROUND, FOLLOWED CHECKLIST & LANDED WITHOUT INCIDENT. ON THE INITIAL INSSDR 9JLA2012052303524Fuel Control · defectiveLT ENGINE WOULD NOT GO TO IDLE THRUST WITH THROTTLE LEVER IN THE IDLE POSITION. TROUBLESHOOTING IDENTIFIED THE ENGINE FUEL CONTROL WAS DEFECTIVE. INSTALLED A REPAIRED UNIT. FUNCTIONAL CHECKED SATISFACTORY.SDR CA120417011Seal · loose(CAN) DOOR SEAL BLEW OUT ON ROUTE,THROUGH FL 310. PRESSURIZATION WAS NOT AFFECTED, BUT THE NOISE CAUSED PROBLEMS WITH ATC COMMUNICATION. THE NOISE WAS CONSIDERABLE UNTIL PRESSURIZATION DIFFERENTIAL WENT DOWN. MAINTENANCED ADDRESED PROBLEM BY, REPAIRING DOOSDR DXTA2011121204820Fcu · failedON INITIAL CLIMB, AT APPROX 600-1000 FT AGL, NR 1 ENGINE COMPUTER LIGHT ILLUMINATED ASSOCIATED WITH A NOTICABLE YAW OF THE ACFT. ABNORMAL CHECKLIST ITEMS COMPLETED AND ENGINE COMPUTER SET TO OVERSPEED PROT. NO ENGINE EXCEEDANCES NOTED AND ENGINE OPS CONTINUEDSDR DXTA2011112804797Pump · malfunctionedDEPARTING AND CLIMBING PAST 12,000 FT, THE RT ENGINE OIL PRESSURE WENT ABOVE 46 PSI AND CONTINUED INCREASING. REDUCING ENGINE POWER DID NOT REDUCE PRESSURE INDICATIONS. STOPPED CLIMB AT 27,000 FT AND PRESSURE WENT TO 70 PSI. PRESSURE REMAINED 60-70 PSI. ENGISDR CA111028008Terminal · corroded(CAN) FLIGHT COMMAND BARS FLUCTUATING IN ALT MODE AS WELL AS OTHER VERTICAL MODES. TROUBLESHOOTING CONFIRMED FLIGHT COMMAND BARS WERE FLUCTUATING UP TO +/- 10 DEGREES. FOUND FLAP COMPENSATION WIRING AT AVIONICS PANEL JA IN THE RT WING MX COMPARTMENT (ACCESS PSDR DJFA2011039Oil Cap · misinstalledDURING CLIMB, CREW NOTED THE MASTER WARNING LIGHT ILLUMINATED IN CONJUNCTION WITH THE LT ENGINE LOW OIL PRESSURE LIGHT. ADDITIONALLY, THE CREW NOTED THE LT ENGINE OIL PRESSURE INDICATOR DISPLAYED ZERO OIL PRESSURE. THE LT ENGINE WAS SHUTDOWN AND THE ACFT RETSDR CWQA06302011Switch · false indication(CWQA) APU FIRE WARNING AIRBOURNE, APU AUTO SHUTDOWN, APU FIRE BOTTLE BLOWN IAW CHECKLIST, FIRE WARNING WENT AWAY. INSPECTION PERFORMED, DETERMINED NO FIRE, DETERMINED WAS FALSE FIRE WARNING. TESTING AND REPLACING FIRE DETECT SWITCH PN 17343-62-600, SN NSN, SDR CA110614011Turbine Blades · damaged(CAN) ON CLIMB-OUT THROUGH 25,000 FT A LARGE BANG WAS HEARD AND MODERATE VIBRATION FELT THROUGH THE REAR OF THE ACFT FOLLOWED BY AN EXHAUST ODOR. AIRCRAFT LEVELLED OUT AT 26,000 FT. ALL INDICATIONS WERE WITHIN LIMITS, BUT THERE WAS A LOWER ITT, N1, N2 AND SDR 2011FA0000332Compressor · separatedRETURNED FOR A REPORTED IN FLIGHT SHUTDOWN. REPAIR AND O/H DISASSEMBLED THE ENGINE IAW THE CURRENT MM FOR ENGINEERING INVESTIGATION. DISASSEMBLY FINDINGS REVEALED SEPARATION OF THE SECOND STAGE COMPRESSOR ROTOR ROTATING SHROUD. THE SHROUD WAS SUBMITTED TO PSDR DXTA2011030804498Warning Light · multiple failDURING DECENT HAD ELECTRICAL AND ICE PROTECT LOOK UP LIGHTS COME ON. SAW THE GEN 1 AND ALT 1 FAIL LIGHTS ON. NOTICED THE LT OIL PRESSURE WAS FALLING. CHECKED GUAGE AND SAW 10 PSI. DIGIT WAS STILL GREEN BUT OUR CHECK LIST CALLS FOR HP COCK TO BE CLOSED IF IT SDR DXTA2011030844971Fcu · malfunctionedDURING DECENT, ELECTRICAL AND ICE PROTECT LOOK UP LIGHTS COME ON. GEN 1 AND ALT 1 FAIL LIGHTS ON. NOTICED LT OIL PRESSURE FALLING. CHECKED GUAGE, 10 PSI. DIGIT STILL GREEN BUT CHECK LIST CALLS FOR HP COCK TO BE CLOSED IF IT FALLS BELOW 25. RAN SHUTDOWN CHSDR E81RJT229443Bracket · crackedFLIGHT CREW REPORTED AN UNLOCKED LANDING GEAR/DOOR INDICATION FOLLOWING GEAR RETRACTION AFTER DEPARTURE. LANDING GEAR WAS CYCLED AND INDICATIONS WERE NORMAL FOLLOWING RETRACTION. NO UNUSUAL NOISE/BUFFETING, NOTED DURING CRUISE FLIGHT. UPON ARRIVAL NOTED THESDR DXTA2011011804420Engine · vibrationWHILE IN LEVEL FLIGHT AT FL 380, BOTH CREW MEMBERS FELT A VIBRATION AND IMMEDIATELY THE RT ENGINE SHUTDOWN. INSTRUMENTATION INDICATED NO ROTATION ON EITHER N1 OR N2. ENGINE WAS SECURED AND LANDING WAS MADE.SDR DXTA2010121904366Transducer · intermittent"ENGINE 1 COMPUTER" ANNUNCIATOR CAME ON DURING CRUISE AT FL360. NOTICED REDUCED N1AND N2 SPEEDS (APPRX. 7 PERCENT LESS THAN ENG 2.) PERFORMED CHECKLIST AND PLACED ENG COMPUTER SWITCH TO "OVSPD PROT". REPLACED NR1 ENGINE, N1 MONOPOLE TRANSDUCER MOTIONAL PICKUSDR DXTA2010121304363Downlock Switch · dirtyRIGHT MLG RED UNSAFE LIGHT ON AFTER INITIALLY RETRACTING THE GEAR. INSPECTED, CLEANED AND LUBED RT NORMAL & STANDBY DOWNLOCK SWITCHES, JACKED ACFT AND CYCLED GEAR NUMEROUS TIMES WITH NO DISCREPANCYS NOTED, OPS CHECKED GOOD IAW MM 32-60-00-501.SDR CA101202006Controller · failed(CAN) AIRCRAFT HAD SUDDEN DEPRESSURIZATION AT 36000 FT JUST AS DESCENT FOR LANDING WAS INITIALIZED. RAPID DECOMPRESSION, NOV 2010. 1: REASON FOR OUTFLOW VALVE REMOVAL/REPLACEMENT: CAMP NR 210146 + 210161, DUE FOR 1200 HR INSPECTION REQUIRMENTS, P/N ON/OFF: LSDR DXTA2010112904332Master Cylinder · lowPILOTS SIDE BRAKES ARE MUSHY AND THEN BECOME GRABBY AS THEY APPROACH THE FLOOR. UNABLE TO CHECK CO-PILOTS SIDE DUE TO PAX ONBOARD. INSPECTED BRAKE ACCUMULATOR, PRESSURE GOOD. RESEVOIR FLUID LEVEL GOOD, NOTED IN HISTORY LEFT BRAKES & MAXERET WERE BLED. CHECKSDR DJFA2010031Coalescer Bag · dirtyHOT BLEED AIR LEAK NOTICED IN REAR BAY COMPARTMENT - SOURCE IS UNKNOWN - ODOR IN CABIN AND REAR BAY COMPARTMENT WITH EITHER APU BLEED AIR OR ENGINE BLEED/AIR VALVE OPEN WAS ALSO NOTED. MAINTENANCE CHANGED THE COALESOR SOCK BUT COULD NOT FIND EVIDENCE OF A BLESDR DJFA2010030Unknown · odorAFTER TAKEOFF CREW REPORTED BURNED FUEL ODOR IN THE COCKPIT. THE ODOR SLOWLY DISSPATED TO A STRONG HOT ODOR. ACFT CONTINUED TO ITS DESTINATION AND LANDED SAFELY. MAINTENANCE RAN BOTH ENGINES AND THE APU BUT WERE UNABLE TO DUPLICATE THE DISCREPANCY.SDR DXTA2010090904227Unknown · multiple indOST FMS 1, FMS 2, COMM 1, NAV 1, FLIGHT DIRECTOR, AUTO PILOT, GPWS, WX RADAR, RADAR ALTIMETER AND HAD A FLASHING AOA WHEN WE ENCOUNTERED MODERATE TURBULENCE AT FL 400 AND .75 MACH. POWERED THE AIRPLANE DOWN ON LANDING AND NOW EVERYTHING WORKS AFTER POWERING THSDR DXTA2010090904228Transducer · fluctuatesNR 2 ENG SHUTDOWN IN FLT DUE TO FLUCTUATION OF N1, N2, & FUEL FLOW. FLUCTUATIONS INCREASED AS POWER DECREASED. PRIOR TO SHUTDOWN, ENG FLUCTATED 75-95 % N1. A SMALL FLUCTUATION OBSERVED AFTER DEPARTURE. ENG NORMAL TO FL 400. INSPECTED INLET & EXHAUST FOUND NO DSDR 2010F00224Pump · failed(TM2R) CREW REPORTED THE "ENG NR1 FUEL" ANNUNCIATOR ILLUMINATED DURING FLIGHT.SDR DJFA2010008Pump · inoperativeON APPROACH FOR LANDING, THE LT ENGINE LOW OIL PRESSURE LIGHT ILLUMINTATED. CREW NOTED THE OIL PRESSURE DROPPED TO 20PSI. THE ENGINE WAS SHUTDOWN AND DECLARED AN EMERGENCY FOR PRIORITY HANDLING. ACFT LANDED SAFELY. MX DISCOVERED THE OIL PUMP FAILED. THE OSDR DXTA2010031804040Fuel Control · faultyON CLIMBOUT, RT ENG POWER ROLLED BACK TWICE. 1ST OCCURENCE DURING CLIMB 3000 TO 5000 WITH POWER SET FOR A SHORT DURATION CLIMB (APRROX 90 PERCNET N1). RT ENG ROLLED BACK TO APPROX 60 % N1 WITH NO WARNING LIGHT OR MASTER CAUTION LIGHT. POWER FROM RT ENG RETURSDR 2010F00058Cabin Pressure · malfunctionedACFT WOULD NOT PRESSURIZE AFTER LIFTOFF. MAIN VALVES BOTH ON, DUMP VALVE CLOSED, CB'S ALL IN, AND AUTO PRESS SWITCH IN AUTO. CLIMBED TO 10000 BEFORE TURNING BACK.SDR DXTA2010030404013Brake · malfunctionedON LANDING, RT BRAKE PEDAL TRAVEL ON LT SIDE WAS EXCESSIVE IN ORDER TO BRAKE. ACTIVATING RT BRAKE PEDAL SEVERAL TIMES RESULTED IN NORMAL BRAKING TO TAXI IN. WHEN ACFT IS COLD SOAKED, RT BRAKE PEDAL IS MUSHY. SERVICED PILOTS RT MASTER CYL IAW MM 32-40-00. TASDR DXTA2010030304011Receptacle · looseIN FLIGHT WE LOST ALL COMMUNICATIONS, APPEARED TO BE STUCK MIC ON CAPTAINS SIDE. WHEN WE SWITCHED RADIOS IT FOLLOWED TO NEXT RADIO. WE FINALLY WERE ABLE TO COMMUNICATE ON EMERGENCY. TIGHTENED LOOSE HAND MIC JACKS IN YOKE. REPOSTIONED COPILOTS BOOM MIC JACK TOSDR DXTA2010030104009Computer · failedELECTRIC PITCH TRIM WENT FULL NOSE DOWN WHEN LEVEL AT 38000. ELECTRIC PITCH TRIM CIRCUIT BREAKER WAS PULLED. ELECTRIC PITCH MOTOR CONTINUED TO RUN WITH CIRCUIT BREAKER PULLED. WERE ABLE TO OVER-POWER THE MOTOR AND MAINTAIN CONTROL OF THE ACFT. DESCENDING TSDR DXTA2010022604006Smoke Detector · false activation"BAG FIRE" LIGHT CAME ON AT FL380 3 DIFFERENT TIMES, IN A PERIOD OF 5 MINUTES, FOR 2-3 SECONDS EACH TIME. SCAN OF ALL 3 COMPARTMENTS PLUS UNDER SINK AREA AND FOUND NO EVIDENCE OF SMOKE, FIRE, OR EXCESSIVE HEAT. "BAG FIRE LIGHT DID NOT COME ON FOR THE REST OF TSDR DXTA2010021803993Brake · weakBRAKE PEDAL TRAVEL EXCESSIVE ON BOTH SIDES TO SLOW/STOP ACFT. PEDALS SPONGY AND CAN EASILY BE PUSHED TO THE STOP. SERVICED BRAKE SYS IAW AMM 32-40-00. SERVICED MASTER CYLINDERS, BLED BRAKE CONTROL VALVE, BLED LT OTBD, LT INBD, RT OTBD, AND RT INBD BRAKES, BOTSDR CWQA2010F00030Controller · faultyAUTO PRESSURIZATION CONTROLLER FAILURE DROVE CABIN BELOW SEA-LEVEL AFTER TAKE OFF.SDR 2010FA0000000Bearing · failedDURING FLIGHT INBOUND, THERE WAS AN IN FLIGHT SHUTDOWN OF THE NR 2 ENGINE. THE ENGINE UNDERWENT A MPI/CZI INSP 80.8 HOURS PRIOR TO THE FAILURE. TEARDOWN INSP REVEALED A FAILURE OF THE UPPER TOWER SHAFT BEARING. THIS WAS AN ORIGINAL BEARING THAT UNDERWENT CZI SDR DXTA2009120103874Wire · looseAFTER ROTATION, PASSING 300' AGL, NR 1 ITT INDICATOR WENT INTO RED, SHOWED APPROX 1100 DEG C. REDUCED PWR BELOW 74 PERCENT N1. ITT CAME OUT OF RED BUT THEN INCREASED BACK ABOVE RED LINE. PWR FURTHER REDUCED TO JUST ABOVE IDLE. ITT THEN CAME BACK WITHIN LIMISDR OZT2009F00000Bulb · inoperativeDURING APPROACH, CREW LOWERED GEAR. UPON GEAR EXTENSION, NO GREEN LIGHT NOTED FOR NOSE GEAR. CREW PERFORMED A MISS APPROACH AND FOLLOWED ACFT CHECKLIST. UPON RE EXTENSION NO LIGHT INDICATION WAS NOTED FOR NOSE GEAR, ALTHOUGH NOSE GEAR PIN INDICATED GEAR WAS SDR DJSR20091001Engine · failedSUSPECTED - N2 TRANSDUCER SENSOR FAILURE, DIGITAL ENG CONTROL WENT TO MANUAL OPERATION. FUEL CONTROL FAILED TO LIMIT TEMP TO 941 DEGREES. ENGINE UNCOMMANDED 106.5 N1 OVERSPEED/1000 DEGREE OVERTEMP WHILE IN CRUISE AT 32,000 FT, COMPUTER LIGHT ILLUMINATED (RT SDR CA090825002Engine · smokeIMMEDIATELY AFTER TAKEOFF, WITH OILY SMELLING SMOKE APPEARED IN COCKPIT AND CABIN. OIL LEVELS CHECKED IN ENGINES, APU, AND ACM FOUND TO BE CORRECT. VISUAL INSP CARRIED OUT BY BORESCOPE BEHIND FAN AREA FOR OIL TRACES NO FAULT FOUND. APU BLEED DUCT INSPECTED FOSDR CA090819002Servo Valve · leaking(CAN) CAPTAIN`S NR 2 BRAKES FAILED ON LANDING, CO-PILOTS WORKED TO BRING ACFT TO A STOP. FOUND BRAKE RESERVOIR LEVEL LOW/EMPTY, LEAKING EXCITATION SERVO VALVE ON EMERGENCY PWR BRAKE VALVE. (1) HYDRAULIC LINE FOUND TUBE ASSY. PN MY20745-259 LEAKING/CRAKED. RSDR DJFA2009024Engine · making metalDURING CRUISE, CREW REPORTED HEARING FOUR (4) LOUD "BANGS" FROM THE NR 2 ENGINE FOLLOWED BY LOSS OF POWER FROM THAT ENGINE AND SMOKE IN THE CABIN. ENGINE REGAINED POWER BUT IT WAS ACCOMPANIED BY A VIBRATION IN THE YOKE AND RUDDER PEDALS. ACFT LANDED SAFELY. SDR DJFA2009023O-Ring · damagedON CLIMB OUT, NR 1 ENGINE BEGAN TO LOSE OIL PRESSURE. CREW ELECTED TO SHUT DOWN THE ENGINE AND LAND. MX FOUND THE OIL SERVICING CAP NOT INSTALLED. THE CAP WAS FOUND NEAR THE ACCESSORY GEARBOX AND THE CAP'S O-RING APPEARED TO BE EXPANDED. MX REPLACED THE O-
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