# Garrett TPE331-1 - Type: Engine model (FAA registry) - Registry code: 29030 - Manufacturer (registry): GARRETT - Model: TPE331-1 - Engine type: Reciprocating - Power: 665 hp - Data sheet: [TCDS E3WE](https://openairdocs.org/tcds/E3WE) (OpenAirDocs) - Holder: Honeywell Aerospace US LLC - Installed in: 5 registered aircraft - Page: https://openairdocs.org/engine/garrett-tpe331-1 Model codes come from the FAA registry's reference file. ## ADs that may apply (OpenAirDocs) Matched to this engine model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. - [AD 2018-17-15](https://openairdocs.org/ad/2018-17-15): Turbine Engine Combustion Section · Honeywell International TPE331-1, TPE331-10, TPE331-10AV and 39 more. Effective Oct 22, 2018 - [AD 2018-13-05](https://openairdocs.org/ad/2018-13-05): Turbine Engine Reduction Gear · Honeywell International TPE331-1, TPE331-10, TPE331-10AV and 18 more. Effective Jul 26, 2018 - [AD 2016-21-07](https://openairdocs.org/ad/2016-21-07): Fuel control drive · Honeywell International TPE331-1, TPE331-10, TPE331-10AV and 26 more. Effective Nov 28, 2016 - [AD 2011-18-51 R1](https://openairdocs.org/ad/2011-18-51-R1): Main shaft bearing · Honeywell International TPE331-1, TPE331-10, TPE331-10A and 82 more. Effective Oct 19, 2011 - [AD 2006-14-03](https://openairdocs.org/ad/2006-14-03): New flight cycle counting method for first, second, and third-stage turbine rotors · Honeywell International TPE331-1, TPE331-10, TPE331-10A and 48 more. Effective Aug 9, 2006 - [AD 2002-21-15](https://openairdocs.org/ad/2002-21-15): Second stage turbine stator inner seal support · Honeywell International TPE331-1, TPE331-2, TPE331-2UA and 9 more. Effective Nov 26, 2002 - [AD 98-04-15](https://openairdocs.org/ad/98-04-15): Turbine Stators · Honeywell International TPE331-1, TPE331-2, TPE331-2UA and 9 more. Effective Apr 27, 1998 - [AD 95-16-08](https://openairdocs.org/ad/95-16-08): Life Limited Turbine Components · Honeywell International TPE331-1, TPE331-10, TPE331-10A and 62 more. Effective Sep 5, 1995 - [AD 94-09-08](https://openairdocs.org/ad/94-09-08): Third Stage Stator Turbine Assemblies · Honeywell International TPE331-1, TPE331-2, TPE331-2UA and 7 more. Effective May 20, 1994 - [AD 93-15-11](https://openairdocs.org/ad/93-15-11): Propeller Pitch Control (PPC) Gasket · Honeywell International TPE331-1, TPE331-10, TPE331-10A and 58 more. Effective Sep 7, 1993 - [AD 92-26-08](https://openairdocs.org/ad/92-26-08): Third Stage Stator Assemblies · Honeywell International TPE331-1, TPE331-2, TPE331-2UA and 7 more. Effective Jul 15, 1993 - [AD 93-05-09](https://openairdocs.org/ad/93-05-09): Third Stage Turbine Stator Assemblies · Honeywell International TPE331-1, TPE331-2, TPE331-2UA and 9 more. Effective Jun 28, 1993 - [AD 89-07-07 R1](https://openairdocs.org/ad/89-07-07-R1): Oil Scavenge Pump Assembly · Honeywell International TPE331-1, TPE331-10, TPE331-10R and 26 more. Effective Oct 30, 1989 - [AD 84-10-06 R1](https://openairdocs.org/ad/84-10-06-R1): Fuel Pump Assemblies · Honeywell International TPE331-1, TPE331-10, TPE331-10B and 45 more. Effective Dec 26, 1984 - [AD 84-01-04](https://openairdocs.org/ad/84-01-04): Third Stage Turbine Wheels · Honeywell International TPE331-1, TPE331-1U, TPE331-1UA and 11 more. Effective Jan 25, 1984 - [AD 73-26-07 R3](https://openairdocs.org/ad/73-26-07-R3): Fuel Pump Shaft Internal Drive Splines · Honeywell International TPE331-1, TPE331-1U, TPE331-1UA and 39 more. Effective Jul 31, 1980 - [AD 78-25-08 R3](https://openairdocs.org/ad/78-25-08-R3): Turbine Rotor · Honeywell International TPE331-1, TPE331-1U, TPE331-1UA and 11 more. Effective Jun 12, 1980 - [AD 78-05-02](https://openairdocs.org/ad/78-05-02): Propeller Pitch Control Cam Follower Pin · Honeywell International TPE331-1, TPE331-1U, TPE331-1UA and 11 more. Effective Apr 5, 1979 - [AD 76-16-01](https://openairdocs.org/ad/76-16-01): Bearing Oil Transfer Tube · Honeywell International TPE331-1, TPE331-1U, TPE331-1UA and 11 more. Effective Aug 6, 1976 - [AD 75-10-05](https://openairdocs.org/ad/75-10-05): Torque Sensor Assembly Mounting Arm · Honeywell International TPE331-1, TPE331-2, TPE331-3U and 3 more. Effective Jul 11, 1975 - [AD 74-10-10](https://openairdocs.org/ad/74-10-10): Fuel Control Assembly Support Bracket · Honeywell International TPE331-1, TPE331-2, TPE331-3U and 2 more. Effective Jul 11, 1975 - [AD 70-19-02](https://openairdocs.org/ad/70-19-02): High Speed Pinion Bearings · Honeywell International TPE331-1, TPE331-1U, TPE331-1UA and 3 more. Effective Feb 20, 1974 - [AD 71-05-07](https://openairdocs.org/ad/71-05-07): High Speed Pinion Assembly · Honeywell International TPE331-1, TPE331-1U, TPE331-1UA and 30 more. Effective Apr 8, 1972 - [AD 70-04-04](https://openairdocs.org/ad/70-04-04): High Speed Pinion Retaining Nut · Honeywell International TPE331-1, TPE331-1U, TPE331-1UA and 3 more Historical (superseded or no longer in force): - [AD 2018-02-14](https://openairdocs.org/ad/2018-02-14) (historical): Turbine Engine Combustion Section · Honeywell International TPE331-1, TPE331-10, TPE331-10AV and 38 more. Effective Feb 28, 2018 - [AD 2015-12-04](https://openairdocs.org/ad/2015-12-04) (historical): Fuel control unit (FCU) · Honeywell International TPE331-1, TPE331-10, TPE331-10AV and 26 more. Effective Jul 22, 2015 - [AD 2011-18-51](https://openairdocs.org/ad/2011-18-51) (historical): Main shaft bearing · Honeywell International TPE331-1, TPE331-10, TPE331-10A and 82 more - [AD 2006-15-08](https://openairdocs.org/ad/2006-15-08) (historical): Woodward fuel control unit (FCU) assemblies · Honeywell International TPE331-1, TPE331-10, TPE331-10AV and 26 more. Effective Aug 24, 2006 - [AD 91-04-02](https://openairdocs.org/ad/91-04-02) (historical): Third stage stator assembly · Honeywell International TPE331-1, TPE331-2, TPE331-2UA and 7 more - [AD 90-21-01](https://openairdocs.org/ad/90-21-01) (historical): Third stage stator assembly · Honeywell International TPE331-1, TPE331-2, TPE331-2UA and 7 more ## Information bulletins (advisory) (1) - [SAIB NE-16-18](https://openairdocs.org/saib/NE-16-18): Power Lever Loss of Power Control. Issued Jul 11, 2016 ## Registered aircraft (5) - [N10192](https://openairdocs.org/aircraft/N10192): [Frontier Agricultural Service Inc](https://openairdocs.org/faa-owner/FRONTIER%20AGRICULTURAL%20SERVICE%20INC), [Calexico, CA](https://openairdocs.org/faa-place/CA/Calexico), built 1989, S/N 401-0731 - [N1836C](https://openairdocs.org/aircraft/N1836C): [Cascade Airways LLC](https://openairdocs.org/faa-owner/CASCADE%20AIRWAYS%20LLC), [Jefferson, OR](https://openairdocs.org/faa-place/OR/Jefferson), built 1978, S/N 36C - [N331U](https://openairdocs.org/aircraft/N331U): [Skyworks Aviation LLC](https://openairdocs.org/faa-owner/SKYWORKS%20AVIATION%20LLC), [Waynesboro, GA](https://openairdocs.org/faa-place/GA/Waynesboro), built 1975, S/N 2136S - [N401RR](https://openairdocs.org/aircraft/N401RR): [Flying Ace LLC](https://openairdocs.org/faa-owner/FLYING%20ACE%20LLC), [Manchester, MI](https://openairdocs.org/faa-place/MI/Manchester), built 2022, S/N LIV-486 - [N999QC](https://openairdocs.org/aircraft/N999QC): [Bennett Ag LLC](https://openairdocs.org/faa-owner/BENNETT%20AG%20LLC), [Pocahontas, AR](https://openairdocs.org/faa-place/AR/Pocahontas), built 1977, S/N 28C ## NTSB investigations (2) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB CEN10LA250](https://openairdocs.org/ntsb/CEN10LA250), May 16, 2010: Ayres S2R (N241WD), Rushville, NE, substantial damage, 1 fatal. Probable cause: The pilot did not maintain clearance from a power line while maneuvering at low altitude. - [NTSB FTW90DPG11](https://openairdocs.org/ntsb/FTW90DPG11), Aug 23, 1990: Air Tractor AT401 (N10192), Altheimer, AR, substantial damage. Probable cause: THE PILOT'S FAILURE TO ALIGN THE AIRPLANE WITH THE RUNWAY DURING LANDING. ## FAA accident and incident reports (3) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Accident 20100516004939A](https://openairdocs.org/incident/20100516004939A), May 16, 2010: Ayres Corp S-2R (N241WD), Rushville, NE, Destroyed, 1 fatal. At approx 1330 MST the aircraft was observed spraying a field. A witness said the aircraft was headed south then yawed to the southeast, rolled upside down and… - [Incident 19990628018629I](https://openairdocs.org/incident/19990628018629I), Jun 28, 1999: Airtrc AT401 (N10192), Griffiyville, AR, Minor damage. (-5)On June 28, 1999, at approximately 1630 p.m. departed Private strip in a/c N10192, a airtractor 401, east to perform areial application, about 100 ft. and… - [Accident 19900823035329A](https://openairdocs.org/incident/19900823035329A), Aug 23, 1990: Airtrc AT401 (N10192), Althiemer, AR, Substantial damage. Wing caught on tall weeds on edge of runway while landing. Aircraft then slid into a ditch. ## Service difficulty reports (211, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR 2017FA0000196](https://openairdocs.org/sdr/2017FA0000196), May 8, 2017: TIRE. FAILED. TIRE BLEW DURING TAKEOFF CAUSING AIRCRAFT TO VEER TO THE RIGHT OF THE RUNWAY. AIRCRAFT HIT A DITCH, AND LEFT WING STRUCK BURM RUPTURING FUEL TANK. AIRCAFT CAUGH - [SDR CA140205001](https://openairdocs.org/sdr/CA140205001), Feb 2, 2014: SENSOR. INACCURATE. (CAN) RT ANNUCIATOR ILLUMINATED AND RT EGT FLUCTUATING. SYSTEM GROUND FAULTED BY MAINTENANCE WITH SRL ON AND OFF. WIRES REPAIRED AT RT SRL COMPUTER FOR SRL ON A - [SDR CA140117009](https://openairdocs.org/sdr/CA140117009), Nov 27, 2013: BEARING. CRACKED. (CAN) ENGINE WAS REPORTED TO BE STIFF TO TURN AT VARIOUS TIMES AFTER ENGINE SHUTDOWN. ENGINE PERFORMANCE/FUNCTION WAS NORMAL. THE STIFFNESS OCCURRED INCONSISTEN - [SDR CA110519002](https://openairdocs.org/sdr/CA110519002), May 18, 2011: TEE FITTING. CRACKED. AFTER AN OPERATIONAL RUN, FUEL WAS FOUND AROUND THE LT ENGINE FUEL BOWL TEE FITTING. THE FITTING WAS REMOVED AND PRESSURE TESTED. A SMALL CRACK WAS FOUND DIRECT - [SDR CA101109014](https://openairdocs.org/sdr/CA101109014), Nov 4, 2010: WIRE. DAMAGED. (CAN) AIRCRAFT TOOK OFF AND 10 MINUTES INTO FLIGHT THE LT RPM WAS VERY ERRATIC AND THEN STOPPED INDICATING. AIRCRAFT RETURNED TO BASE AND MAINTENANCE FOUND A BR - [SDR DUFA20090004](https://openairdocs.org/sdr/DUFA20090004), Oct 2, 2009: FCU. CORRODED. WHILE ON DESCENT DURING APPROACH, PILOT NOTICED AN UNCOMMANDED CHANGE IN PWR ON NR 2 ENG. ATTEMPTED TO ADVANCE PWR LEVER WITH NO INCREASE IN PWR NOTED. CONTINUE - [SDR CA090109004](https://openairdocs.org/sdr/CA090109004), Jan 5, 2009: STATOR. FAILED. (CAN) THIS ENGINE CAME INTO THE SHOP FOR A ROUTINE OVERHAUL. UPON INSPECTING THE NR 3 STATOR IT WAS FOUND TO HAVE THE METAL SPRAY FROM WHEN IT WAS OVERHAULED CO - [SDR CA081117003](https://openairdocs.org/sdr/CA081117003), Nov 13, 2008: IGNITION SWITCH. CRACKED. (CAN) ACFT DEPARTED AIRPORT AND CREW NOTICED SMOKE IN THE CABIN. THE CREW TURNED THE TEMP CONTROLLER OFF - THE BLEEDS WERE TURNED OFF WHICH DUMPED THE CABIN PRE - [SDR CA081020008](https://openairdocs.org/sdr/CA081020008), Oct 9, 2008: WINDSHIELD. CRACKED. (CAN) DURING CRUISE FLIGHT THE LT COCKPIT WINDSHIELD GLASS CRACKED WITH AN EXPLOSIVE BANG. THE CREW IMMEDIATELY DESCENDED AND REDUCED CABIN PRESSURE TO AVOID TH - [SDR CA080819011](https://openairdocs.org/sdr/CA080819011), Aug 10, 2008: TUBE. FRACTURED. (CAN) TUBE HAD BROKEN AT WELDMENT THAT ATTACHES THE TUBE TO THE FLANGE THAT BOLTS IT TO THE ENGINE BLEED. AIR PORT WAS CRACKED 90% OF THE WAY AROUND WELD. THIS - [SDR CA080611010](https://openairdocs.org/sdr/CA080611010), Jun 10, 2008: BEARING RACE. DAMAGED. (CAN) THE INNER SEAL WAS NOTED TO BE PROTRUDING MORE THAN NORMAL. WHEEL ASSY WAS REMOVED AND THE INNER RACE WAS FOUND TO NOT BE SEATED ALL THE WAY. SERVICEABLE - [SDR CA080228011](https://openairdocs.org/sdr/CA080228011), Feb 27, 2008: BELLCRANK. MISSING. DURING MAINTENANCE GEAR RETRACTION A "CLICKING" NOISE WAS HEARD FROM THE NOSE GEAR WHEELWELL. THE ROLLER BEARING ON THE RT NOSE GEAR BELLCRANK WAS BROKEN AND ON - [SDR CA080228012](https://openairdocs.org/sdr/CA080228012), Feb 20, 2008: PIN. DAMAGED. PIVOT PIN FOR RT MAIN GEAR TORQUE KNEE WAS PROTRUDING FROM THE TORQUE KNEE. SPRING PIN REMOVED AND INSPECTED. NO DAMAGE FOUND. NEW SPRING PIN INSTALLED. NO FURT - [SDR CA071106010](https://openairdocs.org/sdr/CA071106010), Oct 30, 2007: FUEL NOZZLE. CRACKED. (CAN) FUEL NOTICED IN ENGINE COWL DURING INSPECTION. NOZZLE IN NR 3 POSITION FOUND CRACKED WHERE PRIMARY/SECONDARY LINES HOOK UP TO NOZZLE. CRACK WAS 95 PERCENT - [SDR CA070615005](https://openairdocs.org/sdr/CA070615005), Jun 13, 2007: AUDIO CONTROL. STICKING. (CAN) BUTTONS HAVE TO BE PRESSED NUMEROUS TIMES BEFORE THEY ENGAGE, REPLACED UNIT. (TC NR 20070615005) - [SDR PNSA060806](https://openairdocs.org/sdr/PNSA060806), Aug 15, 2006: FUEL SYS. BYPASSING. ON TAKEOFF FROM ANC RT ENGINE FUEL BYPASS OPEN LIGHT CAME ON EARLY AT 610C EGT. AIRCRAFT ABORTED AND RETURNED TO BLOCK. MX DEFFERED FUEL BYPASS SYSTEM ON RT ENG - [SDR PNSA060602](https://openairdocs.org/sdr/PNSA060602), Jun 20, 2006: ENGINE. MALFUNCTIONED. DURING TAKEOFF FROM ANC LT ENGINE RPM ROLLED BACK TO 98.5 PERCENT. CREW VERIFIED SPEED LEVER WAS FULL FORWARD. TAKEOFF WAS ABORTED AND AIRRCRAFT RETURNED TO BLO - [SDR BMAC060007](https://openairdocs.org/sdr/BMAC060007), Mar 14, 2006: POWER SUPPLY. DISCHARGED. EMERGENCY LIGHT SYSTEM DOES NOT TEST PROPERLY. (2 LIGHTS OUT) REMOVED AND REPLACED FORWARD POWER SUPPLY UNIT AND 4 BATTERY PACKS P/N AD3128. - [SDR 2006F00010](https://openairdocs.org/sdr/2006F00010), Jan 21, 2006: TORQUE SHAFT. BROKEN. LT MAIN GEAR UPPER TORK LINK SHAFT (P/N 27-51540-003) BROKE ON LANDING, AIRCRAFT WAS UNABLE TO TAXI, LT MAIN WHEEL DIRECTION UNCONTROLLABLE. TORK LINK SHAFT BRO - [SDR AU510001827](https://openairdocs.org/sdr/AU510001827), May 9, 2005: ACM. FAILED. RT AIRCYCLE MACHINE (ACM) FAILED. SMOKE AND FUMES IN AIRCRAFT. - [SDR CA040614003](https://openairdocs.org/sdr/CA040614003), Jun 10, 2004: BETA SWITCH. INTERMITTENT. (CAN) LT BETA LIGHT ILLUMINATED IN FLIGHT. AIRCRAFT RETURNED TO BASE, SWITCH REPLACED AND AIRCRAFT RETURNED TO SERVICE. - [SDR AUS20040235](https://openairdocs.org/sdr/AUS20040235), Mar 24, 2004: SEAL. FAULTY. (AUS) REFUEL/DEFUEL VALVES NOT CLOSING CORRECTLY ALLOWING AIR TO BE DRAWN INTO ENGINE FUEL SYSTEM. INVESTIGATION FOUND THE SEALINGWASHERS INSIDE THE VALVE ASSEM - [SDR CA030729007](https://openairdocs.org/sdr/CA030729007), Jul 23, 2003: STARTER GEN. FAILED. (CAN) STARTER GENERATOR HAD INTERNAL FAILURE CAUSING AN ELECTRICAL SHORT CIRCUIT TO GROUND, CAUSING THE BUSS TIE TO LT BUSS CURRENT LIMITER TO BLOW, THUS CAUSIN - [SDR O3X01119261](https://openairdocs.org/sdr/O3X01119261), Nov 17, 2001: LINE. LOOSE. EN ROUTE FROM BRL-STL, WHEN THE LEFT ENGINE STARTED TO HAVE TORQUE AND TEMPERATURE FLUCTUATIONS NORMAL PROCEDURES WERE FOLLOWED. ENGINE TORQUE AND TEMP REMAINED - [SDR CA001030010](https://openairdocs.org/sdr/CA001030010), Oct 24, 2000: LINE. LEAKING. (CAN) UPON STARTING THE LT ENGINE, THE ENGINEER NOTICED SMOKE COMING FROM INSIDE THE COWLING. HE SIGNALED THE PILOT TO ABORT THE START. WHEN THE COWLS WERE OPEN - [SDR FJT00108753](https://openairdocs.org/sdr/FJT00108753), Oct 17, 2000: HARNESS. CHAFED. REFERENCE SRD FJT00108751: WHILE ENROUTE FROM STL TO UIN AT AN ALTITUDE OF 4,000 FT THE R/H ENG EGT & TORQUE INST BEGAN TO FLUCTUATE/ A/C YAWED & CONT'D TO DO S - [SDR 20000427SH023](https://openairdocs.org/sdr/20000427SH023), Mar 2, 2000: CYLINDER. CRACKED. RADIUS ROD, PN 1862/H, S/N LK-8500827, WAS RETURNED FOR REPAIR DUE TO LEAKAGE AT ROD END. BENCH CHECK CONFIRMED REPORTED LEAKAGE, AND NDT INSPECTION OF CYLINDER - [SDR VTZA990248](https://openairdocs.org/sdr/VTZA990248), Jul 21, 1999: FUEL CONTROL. OUT OF ADJUST. FLT 7602 - IAD-BGM - AIRCRAFT ABORTED TAKEOFF DUE TO RIGHT ENGINE ONLY MADE 94 PERCENT TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE I - [SDR VTZA990245](https://openairdocs.org/sdr/VTZA990245), Jul 18, 1999: FUEL CONTROL. OUT OF ADJUST. FLT 7486 - IAD-BUF - DURING TAKEOFF, CREW ABORTED TAKEOFF DUE TO NR 1 ENGINE RPM ROLLED BACK TO 99.5 PERCENT. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS - [SDR VTZA990243](https://openairdocs.org/sdr/VTZA990243), Jul 16, 1999: FUEL CONTROL. OUT OF ADJUST. FLT 7439 - IAD-GSO - CREW ABORTED TAKEOFF DUE TO NR 2 ENGINE RPM DROPPED TO 99.5 PERCENT ON TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MA - [SDR 99ZZZM775](https://openairdocs.org/sdr/99ZZZM775), Jul 9, 1999: ENGINE. MALFUNCTIONED. FLT 7546 - IAD-EWR - DURING TAKEOFF, MADE AN UNSCHEDULED LANDING DUE TO LEFT ENGINE NOT MAKING TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINT - [SDR VTZA990194](https://openairdocs.org/sdr/VTZA990194), Jun 24, 1999: ENGINE. SHUTDOWN. FLT 7319 - SYR TO IAD - DURING CLIMB, A/C MADE AN UNSCHEDULED LANDING DUE TO LT ENGINE SHUTDOWN IN FLT. A/C RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENAN - [SDR VTZA990093](https://openairdocs.org/sdr/VTZA990093), Jun 21, 1999: ENGINE. MALFUNCTIONED. FLT 7203 - IAD-ROA - ABORTED TAKEOFF DUE TO LEFT ENGINE TORQUE ROLLED BACK ON TAKEOFF ROLL. AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE - [SDR VTZA990146](https://openairdocs.org/sdr/VTZA990146), Jun 9, 1999: ENGINE. MALFUNCTIONED. IAD/ROC - FLT 7292 - DURING TAKEOFF, AIRCRAFT ABORTED TAKEOFF DUE TO LT ENGINE NOT MAKING TORQUE. MAINTENANCE ADJUSTED LT ENGINE MAX FUEL FLOW, GROUND RUN GOOD. - [SDR VTZA990147](https://openairdocs.org/sdr/VTZA990147), Jun 9, 1999: ENGINE. MALFUNCTIONED. IAD/CLE - FLT 7451 - DURING TAKEOFF, AIRCRAFT ABORTED TAKEOFF DUE TO LT ENGINE NOT MAKING TORQUE. MAINTENANCE PERFORMED MAINTENANCE RUNS WITH NO DEFECTS NOTED. - [SDR VTZA990211](https://openairdocs.org/sdr/VTZA990211), Jun 9, 1999: CONTROLLER. FAILED. IAD/PHI - FLT 7652 - DURING TAXI AT 0700, AIRCRAFT LT ENGINE FLAMED OUT DURING MORNING TTL TEST. AIRCRAFT WAS EVACUATED ON THE RUNWAY. MAINTENANCE REMOVED AND R - [SDR 99ZZZX2621](https://openairdocs.org/sdr/99ZZZX2621), Jun 7, 1999: ENGINE. MALFUNCTIONED. ABE/IAD - FLT 7155 - DURING TAKEOFF, AIRCRAFT ABORTED TAKEOFF DUE TO RT ENGINE NOT MAKING REQUIRED TORQUE. AIRCRAFT FERRIED TO IAD. MAINTENANCE REPLACED RT DELT - [SDR VTZA990127](https://openairdocs.org/sdr/VTZA990127), May 28, 1999: FUEL CONTROL. OUT OF ADJUST. FLT 7193 - IAD-ROA - DURING TAKEOFF, AIRCRAFT ABORTED TAKEOFF DUE TO LEFT ENGINE DID NOT MAKE TORQUE WITHIN 10 SECONDS. AIRCRAFT RETURNED TO THE GATE WITH NO FU - [SDR VTZA990128](https://openairdocs.org/sdr/VTZA990128), May 28, 1999: P3 LINE. CRACKED. FLT 7631 - IAD-RDU - DURING TAKEOFF, AIRCRAFT ABORTED TAKEOFF DUE TO RIGHT ENGINE WOULD NOT MAKE MORE THAN 60 PERCENT TORQUE. AIRCRAFT RETURNED TO GATE WITH NO - [SDR VTZA990102](https://openairdocs.org/sdr/VTZA990102), May 25, 1999: FILTER. DIRTY. FLT 7305 - AVP-IAD - AIRCRAFT ABORTED TAKEOFF DUE TO NR 2 FUEL FILTER WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTEN - [SDR VTZA990095](https://openairdocs.org/sdr/VTZA990095), May 23, 1999: FUEL CONTROL. OUT OF ADJUST. FLT 7195 - IAD-ROA - AIRCRAFT ABORTED TAKEOFF DUE TO LEFT ENGINE WOULD ONLY PRODUCE 99.2 PERCENT RPM. AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MA - [SDR VTZA990126](https://openairdocs.org/sdr/VTZA990126), May 23, 1999: ENGINE. POWER LOSS. FLT 7207 - IAD-PHF - DURING CLIMB, AIRCRAT MADE AN UNSCHEDULED LANDING DUE TO RIGHT ENGINE TORQUE DROP TO APPROX 84 PERCENT. AIRCRAFT RETURNED TO THE GATE WITH - [SDR VTZA990139](https://openairdocs.org/sdr/VTZA990139), May 23, 1999: ENGINE. MALFUNCTIONED. FLT 7207 - IAD-PHF - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RIGHT ENGINE TORQUE DROP TO APPROX 84 PERCENT. AIRCRAFT RETURNED TO THE GATE WITH - [SDR VTZA990092](https://openairdocs.org/sdr/VTZA990092), May 20, 1999: ENGINE. MALFUNCTIONED. FLT 7272 - PRIOR TO TAKEOFF, DURING TORQUE AND TEMPERATURE LIMIT TEST, FLIGHT CREW NOTED DROP IN FUEL FLOW AND RPM ON LT ENGINE. TEST REPEATED 3 TIMES WITH SAME - [SDR 99ZZZM424](https://openairdocs.org/sdr/99ZZZM424), May 17, 1999: ENGINE. FAILED. FLT 8832 - LAN-MDW - RIGHT ENGINE FAILED IN FLIGHT WITH OIL CONTAMINATION LIGHT. AIRCRAFT LANDED IN SBN WITHOUT INCIDENT. RIGHT ENGINE REMOVED AND SENT TO OVERH - [SDR VTZA990077](https://openairdocs.org/sdr/VTZA990077), May 12, 1999: ENGINE. FAILED. FLT 7643 - ROC-IAD - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LOSS OF OIL PRESSURE. AIRCRAFT DIVERTED TO MDT AND WENT TO THE GATE WITH NO FURT - [SDR VTZA990056](https://openairdocs.org/sdr/VTZA990056), May 2, 1999: FUEL CONTROL. OUT OF ADJUST. FLT 7282 - IAD-ROA - DURING LANDING MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS RIGHT ENGINE FLAMED OUT ON LANDING. AIRCRAFT WENT TO GATE WITH NO F - [SDR VTZA990037](https://openairdocs.org/sdr/VTZA990037), Apr 21, 1999: FUEL CONTROL. FAILED. FLT 7318 - CHO-IAD - DURING APPROACH, AIRCRAFT EXPERIENCED IN FLIGHT SHUTDOWN OF LEFT ENGINE. MAINTENANCE INSPECTED AND REMOVED AND REPLACED LEFT FUEL CONTROL F - [SDR VTZA990421](https://openairdocs.org/sdr/VTZA990421), Apr 21, 1999: ENGINE. FAILED. FLT 7599 - BGM-IAD- DURING APPROACH, LEFT ENGINE FAILED IN FLIGHT 0 PERCENT TORQUE 50 PERCENT, SRL, FUEL, OIL PRESS CAPTIONS. ENGINE FAILED WITH ANTI-ICE AND IG - [SDR VTZA9907733](https://openairdocs.org/sdr/VTZA9907733), Apr 21, 1999: ENGINE. FAILED. BGM\IAD - FLT 7599 - DURING APPROACH, LEFT ENGINE FAILED IN-FLIGHT, ZERO PERCENT TO 50 PERCENT RPM, SRL, FUEL OIL PRESSURE CAPTIONS. ENGINE FAILED WITH ANTI-ICE All 211: https://openairdocs.org/engine/garrett-tpe331-1/reports.md ## STCs that may be installed (OpenAirDocs) (3) Approved for this engine model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has. - [STC SE00265AT](https://openairdocs.org/stc/SE00265AT): Install Ayres Fuel Manifold Purge Assembly Kit, P/N 21757-1 in accordance with "Installation Instructions - Ayres P/N 21757-1 Fuel Manifold Purge Assy-Kit" Dwg. No. 21757-1(1), Revision none, dated April 20, 1993, or later FAA approved revision. Thrush Aircraft Inc - [STC SE383CH](https://openairdocs.org/stc/SE383CH): Modification of engines. National Flight Services, Inc - [STC SE8029SW](https://openairdocs.org/stc/SE8029SW): Modify propeller pitch control, P/N 869130, by installing pitch control cam, Garrett P/N869386-1. Agri Jet Power, Inc --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.