Garrett TFE731-3R

Service difficulty reports · 24

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 = 'TFE7313R'
  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 CA110316004Servo · malfunctioned(CAN) ON THE RETURN FLIGHT AFTER COMMENCING DESCENT FROM FL400, WHILE ON AUTOPILOT AT APPROX FL220, THE ACFT BEGAN A TURN TO THE LEFT UN-COMMANDED. DISCONNECTED THE AUTOPILOT TO TAKE CONTROL, BUT THE CONTROL SEEMED JAMMED TO THE LT, WITH MODERATE FORCE WAS ABMar 7, 2011 · Hwksly HS125600B · Autopilot Main ServoSDR CA071011007Attach Fitting · cracked(CAN) AFTER REPAINT OF A/C INSPECTION REVEALED A CRACK ON SIDE OF ATTACH POINT. LDG WAS PULLED TO REPLACE ATTACH POINT BRACKET AND ATTACH POINT BRACKET BOLTS. THESE BOLTS WERE SHOWING WEAR MARKS ON THE SHANK, SUGGESTING THE NUTS WERE THREAD BOUND, INDICATING NSep 14, 2007 · Hwksly HS125600A · Fuselage, Landing Gear Attach FittingsSDR CA060906011Skin · cracked(CAN) DURING REMOVAL FOR ACCESS, A GENERAL VISUAL INSPECTION OF THE RT MAIN GEAR DOOR REVEALED A LARGE CRACK IN THE INNER SKIN PANEL AS WELL AS SEVERAL PULLED RIVETS ADJACENT TO THE GEAR DOOR JACK ATTACH BRACKET. SB 32-192-2845 (TO PREVENT CRACKING OF THE BRASep 6, 2006 · Braero HS125700A · Landing Gear DoorsSDR CA050919006Gearshaft · broken(CAN) AS A/C WAS TAXIING FOR T/O, CREW LOST LT ENGINE OIL PRESSURE. ENGINE WAS SHUTDOWN AND A/C WENT BACK TO GATE. LT ENGINE OIL PUMP WAS FOUND DAMAGED. PUMP WAS REPLACED BUT ENGINE COULD NOT START AS N1 FAN WAS NOT TURNING. ENGINE WAS OPENED UP AND NR 1 BAug 31, 2005 · Braero HS125700A · Turbine Engine Accessory DriveSDR 2004FA0000077Wire Harness · deterioratedWHILE EN ROUTE, NOTED RT ENGINE COMPUTER AMBER WARNING LAMP BECAME ANNUNCIATED. ALSO NOTED, INDICATED LOSS OF POWER RT ENGINE. CONSULTED AND COMPLIED WITH EMERGENCY PROCEDURES WHICH INSTRUCTED TO SWITCH TO MANUAL CONTROL AND MONITOR ALL APPLICABLE ENGINE PARJan 4, 2004 · N120JC · Braero HS125700A · Engine Control System WiringSDR ILPA048FPressure Panel · crackedDURING ROUTINE INSPECTION OF THE RIVETS AT THE FORWARD PRESSURE BULKHEAD, TWO SEPERATE CRACKS WERE NOTED IN THE LT DISHPAN JUST FORWARD OF THE PILOTS RUDDER PEDALS. THE CRACKS WERE BETWEEN FASTENERS. THE PN S25-8FN323-1 WAS REMOVED & REPLACED IN ACCORDANCE WITJan 24, 2003 · N120JC · Braero HS125700A · Fuselage Main, BulkheadSDR CA020607009Gasket · missing(CAN) CREW NOTICED RT ENGINE OIL PRESSURE FLUCTUATING SLIGHTLY.- AFTER A PERIOD OF TIME THE OIL PRESSURE STARTED TO DECAY TO WHERE THE RED LOW OIL PRESSURE LIGHT ILLUMINATED (~25PSI).- A PRECAUTIONARY MANUAL SHUTDOWN WAS PERFORMED ON THE RT ENGINE (S/N P84403May 30, 2002 · Braero HS125700A · Turbine Engine Oil SystemSDR CA020201010Wire · worn(CAN) LT ENGINE STARTER GENERATOR WIRING WORN AT SUPPORT BRACKET.Jan 21, 2002 · Braero HS125700A · Starter-GeneratorSDR CA020201012Fairlead · broken(CAN) LT ENGINE STARTER GENERATOR WIRING WORN AT SUPPORT BRACKET AND PHENOLIC FAIRLEAD BROKEN.Jan 21, 2002 · Braero HS125700A · Starter-GeneratorSDR UO22001F00011Bearing · failedLOWER TOWER SHAFT BEARING FAILED CAUSING DAMAGE TO RELATED SHAFT AND CARRIERS ALSO CAUSING METAL CONTAMINATION TO OIL SYSTEM.Oct 18, 2001 · N405TP · Hawker BAE125700B · Turbine Engine Accessory DriveSDR CA010209017Relay · failed(CAN) AFTER TAXI IN AT YVR THE NR 2 AC INVERTER FAIL LIGHT ILLUMINATED AS WELL AS XS2 BUSS FAIL LIGHT ILLUMINATED. RESET THE NR 2 INVERTER SWITCH FAILED TO RESET THE SYSTEM. MAINTENANCE TROUBLESHOOT THE PROBLEM BACK TO A FAULTY RELAY WITHIN THE CABIN LIGHTING Jan 31, 2001 · Braero HS125700A · Flight Compartment LightingSDR 99ZZZM808Blade · brokenENGINE WAS DISASSEMBLED FOR SCHEDULED MPI. DISCOVERED A FIRST STAGE LOW PRESSURE TURBINE BLADE FAILURE. THE SINGLE BLADE HAD FAILED AT THE MID-POINT OF THE BLADE. ALL OF THE FIRST STAGE AND 2ND STAGE LPT BLADES SUFFERED DAMAGE AND WILL BE REPLACED. 10 OF TNov 18, 1999 · N270KA · Braero HS125700A · Turbine SectionSDR 99ZZZX3009Carbon Seal · failedENGINE LOST OIL PRESSURE IN-FLIGHT. DISASSEMBLY FOUND NR 5 CARBON SEAL BROKEN. CONTAMINATED OIL SYSTEM. PART S/N 960811401752. ENG TSN: 7,666.3 HOURS. ENG CSN: 5,701 HOURS. PART CSN: 547.Jul 30, 1999 · Turbine Engine Compressor SectionSDR 20000712SH038Turbine Wheel · chafedSECOND OCCURRENCE OF 3RD STAGE LP TURBINE RUBBING FORWARD SIDE OF 3RD STAGE LPT SEAL. (X)Jul 26, 1999 · Turbine SectionSDR CA990301002Bearing · seized(CAN) APU SHUT DOWN DUE TO ROTOR GROUP SEIZURE. THE BEARING WAS A CORRECT ONE, AND FAILED MUCH TOO EARLY.Feb 3, 1999 · Braero HS125700A · APU Core EngineSDR 99ZZZX802Engine · malfunctionedENGINE SHUT DOWN AT ALTITUDE BY PILOT. METAL PARTICLES FOUND IN TAIL PIPE DURING ENGINE REMOVAL. ENGINE FAN AND FAN TURBINE TURNED FREELY WITH NO NOISE. ENGINE OIL TANK SERVICED ABOVE SITE GAUGE. AIRFRAME TIME: 6,917.7 HOURS. CYCLES: 6,514. RIGHT ENGINEJan 26, 1999 · N91BZ · Rkwell NA26565 · Engine (Turbine/Turboprop)SDR 99ZZZX824Blade · separatedDURING CRUISE AT FL 350, RT ENG HAD A RAPID RISE IN ITT AND VIBRATION LEVEL. CREW SHUT DOWN ENG. ENG REMOVED TO DETERMINE CAUSE OF FAILURE ANDTO REPAIR. DISASSY REVEALED ON LOW PRESS, 4TH STAGE COMP BLADE, P/N 3072402-1, 'MISSING' FROM COMP ROTOR. BLADE DEJan 26, 1999 · N91BZ · Rkwell NA26565 · Turbine Engine Compressor SectionSDR 99ZZZX60Blade · damagedDURING INSPECTION FOUND NUMEROUS FAN BLADES DAMAGED ON RIGHT ENGINE. FOUND RIVET MISSING AT 6 O'CLOCK POSITION ON ENGINE INLET LIP AND THREE LOOSE RIVETS. SUSPECT INCORRECT INSTALLATION PROCEDURES USED FOR BLIND RIVETS DURING REPAIR. ENGINE INLETS WITH BLINOct 15, 1998 · N38PA · Braero HS125700A · Turbine SectionSDR CA980616016Blade · separated(CAN) AFTER TAKEOFF DURING CLIMB THRU 4000 FEET, A LOUD BANG HEARD, FOLLOWED BY VIBRATION AND NR 1 ENGINE SPOOLING DOWN. ENG SHUT DOWN. NR 1 ENG SUFFERED CATASTROPHIC FAILURE. TEARDOWN SHOWED 10 LPT3 BLADES WERE SEPARATED. ONE BLADE SEPARATED ABOVE PLATFORFeb 18, 1998 · Turbine SectionSDR CA970815014Sleeve Clamp · loose(CAN) UNABLE TO MAINTAIN PRESSURIZATION DURING CLIMB. OPENED FLIGHT DECK VALVE AND RETURNED TO BASE. INVESTIGATION SHOWED A LOOSE CLAMP ON THE SILENCER TO SUPPLY DUCT. CLAMP TIGHTENED AND GROUND CHECKED SERVICEABLE.Aug 4, 1997 · Braero HS125700A · Air Distribution SystemSDR 97ZZZM716Bearing · failedEN ROUTE FROM BOS TO OXC, THE CHIP DETECTOR LIGHT FOR THE RIGHT ENGINE ILLUMINATED. NO OTHER ENGINE ABNORMALITY WAS APPARENT. THE AIRCRAFT LANDED AT OXC WITHOUT INCIDENT. INSPECTION OF THE CHIP DETECTOR REVEALED STEEL CHIPS. A LAB ANALYSIS INDICATED THAT AMay 19, 1997 · N270KA · Braero HS125700A · Turbine Engine Accessory DriveSDR CA970227004Generator · vibrating(CAN) SHORTLY AFTER TAKEOFF, INTERMITTENT VIBRATION WHICH BECAME CONTINUOUS. GENERATOR TRIPPED AND VIBRATIONS DECREASED. ENGINE SHUT DOWN AS PRECAUTIONARY. VIBRATIONS STOPPED IMMEDIATELY. STARTER GENERATOR REPLACED. PART TC: 405.Feb 11, 1997 · Braero HS125700A · Starter-GeneratorSDR CA970206006Fuel Pump · failed(CAN) ENGINE DRIVEN FUEL PUMP HAD NO OUTPUT PRESSURE, UNABLE TO GET START AFTER ENGINE SPOOLED DOWN FROM IDLE. TEAR DOWN REPORT REVEALED DAMAGED BEARING AT VANE STAGE WITH METAL IN UNIT AND ROTOR SMEARED. PART TC: 3,248.Jan 29, 1997 · Braero HS125700A · Engine Fuel PumpSDR JZBR10817Engine · failedWHILE SITTING AT THE END OF RUNWAY, AIRCRAFT WAS CLEAR FOR TAKEOFF. CREW ADVANCED THROTTLES. WHILE SPOOLING UP TO N1 FOR TAKEOFF, THE LEFT ENGINE RELEASED A LOUD EXPLOSION. THROTTLES WERE RETARDED, TRIP WAS CANCELLED. THE AIRCRAFT TAXIED TO A MAINTENANCE FAug 9, 1995 · N746BC · Braero HS125700A · Turbine Section
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