# Service difficulty reports: Garrett TPE-331-10UG A list on [Garrett TPE-331-10UG](https://openairdocs.org/engine/garrett-tpe-331-10ug.md). Newest first. General aviation reporting is voluntary. Page 1 of 2 · 100 reports - [SDR CA100826012](https://openairdocs.org/sdr/CA100826012.md): Engine · making metal · Aug 25, 2010 · Bag JETSTM3112 · Engine (Turbine/Turboprop) > (CAN) ON APPROACH THE NR 2 ENGINE LOST POWER, FLAMED OUT AND STARTED TO NEGATIVE TORQUE SIGNAL (NTS). THE PILOTS WENT THROUGH THE PROCEDURE TO SHUT DOWN AND FEATHER THE NR 2 ENGINE AND LANDED THE PLANE SAFELY. UPON INVESTIGATION, IT WAS DISCOVERED THAT THERE - [SDR CA100827002](https://openairdocs.org/sdr/CA100827002.md): Seal · failed · Jul 25, 2010 · Bag JETSTM3112 · Hydraulic Pump (Electric/Engine), Main > (CAN) DURING SERVICE CHECK TECH FOUND ENGINE OIL TO BE OVER SERVICED. ENGINE OIL ALSO HAD A REDDISH COLOR. UPON FURTHER INSPECTION HYDRAULIC OIL FOUND TO BE UNDER SERVICED. AIRCRAFT WAS GROUNDED UNTIL SOAP SAMPLE WAS RETURNED CONFIRMING HYDRAULIC OIL HAD BE - [SDR CA080724003](https://openairdocs.org/sdr/CA080724003.md): Bearing · spalled · Jul 17, 2008 · Swrngn SA227AC · Turbine Engine Compressor Section > (CAN) SN OF THE PART IS MS030633106124 WAS UNABLE TO PUT THIS INTO SN FIELD. A/C WAS DOWN FOR A ROUTINE OIL SAMPLE. AT THIS TIME THE OIL SAMPLE WAS NOTED TO HAVE A UNUSUAL AMOUNT OF METAL IN THE OIL SAMPLE. THE ENGINE SHOP WAS INFORMED TO HAVE A LOOK AT THE M - [SDR CA080709005](https://openairdocs.org/sdr/CA080709005.md): Retaining Ring · missing · Jul 6, 2008 · Bag JETSTM3212 · Rudder Control System > (CAN) RUDDER PEDAL BECAME DISENGAGED FROM PEDAL SPIGOT, RS87 RETAINING RING CAME OUT OF RETAINING SLOT. RETAINING RING SEEMED TO HAVE INSUFFICIENT TENSION TO STAY IN SLOT. NEW RING INSTALLED AND NO FURTHER PROBLEMS. FLEETWIDE INSPECTION CARRIED OUT AND NO SIMI - [SDR CA080609009](https://openairdocs.org/sdr/CA080609009.md): Attach Fitting · cracked · Jun 4, 2008 · Bag JETSTM3212 · Trailing Edge Flaps > (CAN) WHILE CARRYING OUT A 7 DAY SERVICE CHECK, TECH FOUND 3 FLAP TO SLAT ATTACHEMENT CLEATS, P/N`S 137201B88, 137202B62 AND 137203B57 WERE FOUND TO BE CRACKED. THE FLAP SECTION WAS REMOVED AND A SERVICEABLE UNIT INSTALLED. FUNCTION CHECKS CARRIED OUT WITH NO - [SDR CA080606005](https://openairdocs.org/sdr/CA080606005.md): Bearing · lack of lube · May 16, 2008 · Frchld SA227DC · Wheel/Ski/Float > (CAN) ON TAXI FOR DEPARTURE THE PILOT NOTICED A VIBRATION FROM THE NOSE GEAR. HE RETURNED AND MAINT FOUND LT NOSE WHEEL INNER BEARING SEAL WAS STICKING OUT FROM ITS SEAT. WHEEL BEARING WAS ALSO FOUND TO BE ROUGH TO THE (FEEL) AND WERE DRY. NOSE WHEEL ASSY REP - [SDR 2008FA0000250](https://openairdocs.org/sdr/2008FA0000250.md): Engine · overheated · Mar 5, 2008 · N139LC · Swrngn SA227AC · Engine (Turbine/Turboprop) > IN CRUISE TO 8000 FT, INDICATION OF RED LIGHT OF OIL PRESSURE WITH 870 DEGREE TEMPERATURE. LIGHT TURNS OFF. AFTER 15 SECONDS, THE LIGHT TURNS ON AGAIN WITH 870 DEGREE TEMPERATURE, BUT THE PRESSURE DOWN NEAR ZERO. THE CREW MADE THE SHUTDOWN ENGINE PROCEDURE - [SDR CA080306002](https://openairdocs.org/sdr/CA080306002.md): Valve · failed · Mar 4, 2008 · Bag JETSTM3212 · Hydraulic System, Main > (CAN) THE RT NON RETURN VALVE ASSEMBLY DOWNSTREAM OF THE RT HYDRAULIC PUMP FAILED. NON RETURN VALVE ASSEMBLY IS A UNIT THAT IS SWAGED TOGETHER. THE SWAGE LET GO, ALLOWING HYDRAULIC FLUID TO VENT OVERBOARD. THIS VALVE IS INSTALLED TO PREVENT PRESSURE FROM EITHE - [SDR CA071217006](https://openairdocs.org/sdr/CA071217006.md): Bolt · backed out · Dec 14, 2007 · Bag JETSTM3212 · Fuel Control/Turbine Engines > (CAN) ON CLIMB OUT, THE PILOT REPORTS NR 1 ENG RPM DROPPED TO 97 PERCENT AND HE WAS NOT ABLE TO RESTORE THE ENG TO 100 PERCENT RPM. PROCEEDED TO MAKE AN UNSCHEDULED LANDING AT DEPARTURE AIRFIELD. UPON INVESTIGATION IT WAS FOUND THAT THE BOLT ATTACHING THE SPE - [SDR CA071219010](https://openairdocs.org/sdr/CA071219010.md): Tube · chafed · Dec 14, 2007 · Bag JETSTM3212 · Turbine Engine Oil System > (CAN) DURING A SCHEDULED FLIGHT BETWEEN, A WARNING INDICATION OF OIL PRESSURE LOSS ON THE NR 1 ENGINE APPEARED ON THE ANNUNCIATOR PANEL. THE CREW VERIFIED THE WARNING BY OBSERVING THE OIL PRESSURE GAUGE. THE ENGINE WAS SHUTDOWN AND AN EMERGENCY WAS DECLARED. T - [SDR CA071026008](https://openairdocs.org/sdr/CA071026008.md): Line · leaking · Oct 23, 2007 · Bag JETSTM3212 · Hydraulic System, Main > (CAN) DURING A ROUTINE 200 HOUR AIRFRAME INSP, HYD FLUID WAS FOUND TO BE LEAKING FROM ABOVE THE BAGGAGE POD ON THE BELLY OF THE AC. THE AIRCRAFT`S IMPENDING DEPARTURE WAS CANCELLED, AND THE POD REMOVED TO INVESTIGATE. IT WAS FOUND THAT THERE WAS A CLAMP MISS - [SDR CA070927003](https://openairdocs.org/sdr/CA070927003.md): Bolt · sheared · Sep 25, 2007 · Bag JETSTM3101 · Nose/Tail Landing Gear > (CAN) DURING INSPECTION IAW AD 024-05-87 BAE SB 53-A-JA870510R1 PART B, IT WAS NOTED THAT THE TWO UPPER BOLTS WERE SHEARED. THE AIRCRAFT WAS REMOVED FROM SERVICE AT THIS TIME. THE LOWER 2 BOLTS HAVE NOT YET BEEN REMOVED FOR INSPECTION. DUE TO THIS FINDING AN - [SDR CA070615003](https://openairdocs.org/sdr/CA070615003.md): Switch · failed · Jun 13, 2007 · Bag · Landing Gear Retraction/Extension System > (CAN) DURING APPROACH, THE CREW EXPERIENCED A LANDING GEAR FAILURE AND OBSERVED THE CIRCUIT BREAKER HAD POPPED. THEY PROCEEDED WITH AN EMERGENCY LANDING GEAR EXTENSION AND LANDED WITHOUT INCIDENT. THE FAULT WAS TRACED TO THE LT UPLOCK MICROSWITCH. WHEN THE MIC - [SDR CA070615004](https://openairdocs.org/sdr/CA070615004.md): Bolt · failed · Jun 13, 2007 · Bag JETSTM3101 · Nose/Tail Landing Gear > (CAN) SCHEDULE INSPECTION AD UK 024-05-87 / SB53A-JA870510R1, WE NOTICE THE 2 UPPER BOLT OF THE NLG JACK MOUNTING BRACKET WERE SHEARED AND THE 2 LOWER ONES WERE LOOSE. ACCOMPLISHED PART A OF THE SB C/OUT(ALL 4 BOLTS AND NUTS REPLACED), PARTS INSPECTED AND AIR - [SDR BMAC07002](https://openairdocs.org/sdr/BMAC07002.md): Bulb · wrong part · Apr 23, 2007 · N530PA · Bag JETSTM3101 · Landing Gear Position and Warning > DURING APPROACH PHASE AT BED UNABLE TO GET GREEN LIGHT ON RT MAIN AND NOSE. SWAPPED BULBS AND FINALLY GOT GREEN LIGHT ON RT MAIN. STILL NO RED OR GREEN LIGHT ON NOSE. PROCEEDED WITH CHECK LIST AND LANDED UNEVENTFULLY. INSTALLED GEAR LOCK PINS. MAINT FOUND INCO - [SDR BMAC07003](https://openairdocs.org/sdr/BMAC07003.md): Line · leaking · Apr 23, 2007 · N539PA · Bag JETSTM3101 · Hydraulic System, Main > UPON LANDING, BRAKES AND STEERING FOUND TO BE VERY SLUGGISH AND BOTH HYD PUMPS INDICATED NEAR ZERO, APPROX. 100 PSI. TAXI TO GATE WITH NO FURTHER INCIDENT. MAINT FOUND HYD SUPPLY PIPE IN RT IB WING CHAFED. REPLACED PIPE AND ARE REPLACING BOTH HYD PUMPS DUE TO - [SDR CA070409007](https://openairdocs.org/sdr/CA070409007.md): Gear · unknown · Feb 28, 2007 · Engine Fuel Pump > (CAN) GEARS DRIVING THE FUEL PUMP FAILED CAUSING THE ENGINE TO SHUTDOWN IN FLIGHT. (TC NR 20070409007) - [SDR CA070215002](https://openairdocs.org/sdr/CA070215002.md): Housing · broken · Feb 13, 2007 · Bag JETSTM3212 · Turbine Engine Accessory Drive > (CAN) ACCESSORY DRIVE HOUSING BOTTOM CASE DRAIN THREADED MOUNTING BOSS DISCOVERED BROKEN. ENGINE REMOVED AND LOANER ENGINE INSTALLED. (TC NR 20070215002) - [SDR CA070212005](https://openairdocs.org/sdr/CA070212005.md): Engine · unserviceable · Feb 7, 2007 · Bag JETSTM3212 · Engine (Turbine/Turboprop) > (CAN) DURING PRE FLIGHT INSPECTION FLIGHT CREW HEARD ABNORMAL NOISE COMING FROM ENGINE WHILE THEY TURNED THE PROPELLER. MAINTENANCE WAS NOTIFIED AND ENGINE WAS INSPECTED, SUSPECT REAR BEARING FAILURE, OIL SYSTEM INSPECTED AND FOUND TO HAVE NO METAL CONTAMINATI - [SDR CA070131007](https://openairdocs.org/sdr/CA070131007.md): Windshield · delaminated · Jan 28, 2007 · Bag JETSTM3212 · Flight Compartment Windows > (CAN) DURING MAINTENANCE INSPECTION, WINDOW WAS FOUND TO BE DELAMINATING AT THE CENTER OF THE BOTTOM EDGE. WINDOW WAS REPLACED. (TC NR 20070131007) - [SDR BMAC06012](https://openairdocs.org/sdr/BMAC06012.md): Battery Pack · discharged · Dec 29, 2006 · N529PA · Bag JETSTM3101 · Emergency Lighting > PILOT REPORTED FORWARD EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED AFT BATTERY PACK, SYSTEM OPERATION CHECKED GOOD IAW AMM 33-50-00. - [SDR CA070115011](https://openairdocs.org/sdr/CA070115011.md): Planetary Gear · damaged · Nov 26, 2006 · Turbine Engine Accessory Drive > (CAN) UPON DOING A OIL SAMPLE, METAL WAS NOTED IN THE OIL FILTER. THE ENGINE P-63235C WAS REMOVED. ENGINE WAS FORWARDED TO THE ENGINE SHOP FOR INSPECTION OF THE METAL AND FOUND THAT 1 PLANETARY GEAR WITH THE INNER RACE PEELING METAL AND 3 PLANETARY GEARS WITH - [SDR CA061024003](https://openairdocs.org/sdr/CA061024003.md): Unknown · odor · Oct 24, 2006 · Bag JETSTM3212 · Air Distribution System > (CAN) DURING CRUISE FLIGHT CREW COULD DETECT FUMES OF AN ELECTRICAL NATURE. AIRCRAFT RETURNED TO DEPARTURE POINT WITHOUT INCIDENT. A MAINTENANCE INVESTIGATION IS UNDER WAY TO DETERMINE THE CAUSE OF THE FUMES/ODOUR. A REPORT WILL FOLLOW WHEN CAUSE IS IDENTIFIED - [SDR CA061020004](https://openairdocs.org/sdr/CA061020004.md): Line · cracked · Oct 14, 2006 · Bag JETSTM3212 · Fuel Pressure Sensor > (CAN) P3 LINE FLANGE FOUND WITH SMALL CRACK DURING ROUTINE ENGINE CHANGE. LINE REPLACED WITH NEW UNIT. (TC# 20061020004) - [SDR CA061108005](https://openairdocs.org/sdr/CA061108005.md): Bracket · cracked · Sep 12, 2006 · Bag JETSTM3212 · Trailing Edge Flaps > (CAN) FLAP SLAT BRACKETS CRACKED AT RADIUS. (TC NR 20061108005) - [SDR CA061109005](https://openairdocs.org/sdr/CA061109005.md): Bracket · cracked · Sep 4, 2006 · Bag JETSTM3212 · Trailing Edge Flaps > (CAN) IB FLAP P/N 13760B463, SLAT BRACKETS P/N 137204B51 AND 137205B67 FOUND CRACKED AT BEND RADIUS. REMOVED AND REPLACED WITH NEW. (TC NR 20061109005) - [SDR CA060719005](https://openairdocs.org/sdr/CA060719005.md): Wheel · damaged · Jul 19, 2006 · Bag JETSTM3212 · Wheel/Ski/Float > (CAN) DURING TOWING OF AIRCRAFT THE PIC AND GROUND HANDLERS NOTICED A WOBBLE ON THE RH MLG. MAINTENANCE WAS CONTACTED AND IT WAS DISCOVERED THAT A 10" PIECE OF THE EDGE OF THE INNER WHEEL RIM WAS MISSING. THE TIRE STILL REMAINED INFLATED. THE WHEEL AND TIRE WA - [SDR CA060616006](https://openairdocs.org/sdr/CA060616006.md): Connector · damaged · Jun 15, 2006 · Bag JETSTM3101 · Turbine Engine System Wiring > (CAN) AFTER DEPARTURE CLIMBING THROUGH 7500FT THE RIGHT ENGINE TORQUE STARTED TO FLUCTUATE.CREW PULLED THE QRH AND FOLLOWED THE DRILLS AND WERE GETTING 10-20% FLUCTUATION CAUSING THE A/C TO YAW RADICALLY LEFT AND RIGHT AT ALL POWER SETTINGS WITH TTL ON OR OFF - [SDR CA060525003](https://openairdocs.org/sdr/CA060525003.md): Engine · malfunctioned · May 25, 2006 · Bag JETSTM3212 · Engine (Turbine/Turboprop) > IN CRUISE, RT ENGINE TORQUE INCREASED TO 104.5%, WHEN TTL TURNED OFF WENT TO 120%. FUEL FLOW ON RT ENG DROPPED TO 200LBS. - [SDR CA060529004](https://openairdocs.org/sdr/CA060529004.md): Flange · split · Apr 28, 2006 · Bag JETSTM3212 · Propeller Governor > FOUND OIL DRIPPING UNDER RIGHT ENGINE AFTER SHUT DOWN, ENGINE CLEANED AND CASE NEGATIVE PRESSURE CHECKED, FOUND SERVICEABLE. ENGINE GROUND RUN/MAX POWER CARRIED OUT. OIL FOUND TO BE LEAKING FROM THE PROP GOVERNOR. PROP GOVERNOR REPLACED WITH SERVICEABLE UNI - [SDR CA060209005](https://openairdocs.org/sdr/CA060209005.md): Starter Gen · failed · Feb 7, 2006 · Bag JETSTM3212 · Starter-Generator > (CAN) RT GENERATOR FAILER INDICATION ON APPROACH. CREW LANDED A/C WITH NO MORE PROBLEMS. STARTER/GENERATOR REPLACED. STARTER/GEN 67.9 HOURS REMAINING BEFORE OVERHAUL DUE. BRUSH INSPECTED TO BE 20 PERCENT REMAINING. (TC NR 20060209005) - [SDR CA060116001](https://openairdocs.org/sdr/CA060116001.md): Valve · cracked · Jan 12, 2006 · Bag JETSTM3212 · Hydraulic System, Main > ON APPROACH, UPON FLAP SELECTION, NO SYSTEM HYD PRESSURE. EMERG GEAR SELECTION USED TO EXTEND L/G, AND TO OBTAIN 10 DEGREES FLAP. A/C LANDED W/O INCIDENT, DUE TO LOSS OF SYS HYD PRESSURE, N/W STEERING INOP AND MAIN BRAKING WAS LIMITED. TOWED TO HANGAR. MX - [SDR CA060104004](https://openairdocs.org/sdr/CA060104004.md): Windscreen · cracked · Jan 2, 2006 · Bag JETSTM3212 · Flight Compartment Windows > AT CRUISE ALT 20,000 FT, NOTICED CRACK AND SUBSEQUENT FLAME WITHIN LAYERS OF LT WINDSHIELD. FLAME SELF EXTINGUISHED WITH DE-SELECTION OF WINDSHIELD HEAT. DURING DESCENT ADDITIONAL CRACKING. DIVERTED TO CYMM. MX DISPATCHED, REPLACED WINDSHIELD. UPON MX REV - [SDR CA051214001](https://openairdocs.org/sdr/CA051214001.md): Generator · failed · Dec 13, 2005 · Bag JETSTM3212 · AC Regulator > (CAN) IAW AMM 24-30-00 501 DC GENERATION-ADJUSTMENT/TEST. GENERATOR VOLTAGE MUST BE WITHIN 0.3 VOLTS OF EACH OTHER. WHEN REPLACING COMPONENTS IN THE GENERATOR SYSTEM, A CHECK OF THE GCU'S VOLTAGE IS RECOMMENDED AS NUMEROUS HOURS OF TROUBLESHOOTING AND PARTS - [SDR CA051011005](https://openairdocs.org/sdr/CA051011005.md): Generator · separated · Sep 21, 2005 · Bag JETSTM3212 · DC Generator-Alternator > (CAN) GENERATOR WENT OFF LINE IN CLIMB OUT. AIRCRAFT RETURNED TO BASE. GENERATOR REPLACED WITH OVERHAULED UNIT. SYSTEM TESTED SATISFACTORY. - [SDR CA050919008](https://openairdocs.org/sdr/CA050919008.md): Engine · unknown · Sep 14, 2005 · Bag JETSTM3212 · Engine (Turbine/Turboprop) > (CAN) ENGINE REMOVED AND SENT REPAIR STATION. RESULTS TO FOLLOW. - [SDR CA051003009](https://openairdocs.org/sdr/CA051003009.md): Brushes · frayed · Sep 11, 2005 · Bag JETSTM3212 · Starter-Generator > (CAN) FOUND WIRES NOT FASTENED TO STARTER GENERATOR BRUSHES, DUE TO RIVET BEING LOOSE,WHICH THEN CAUSED ARCING OF WIRE AND RIVET TO CAUSE THE TEMPOR OUT OF THE RIVET. - [SDR CA050818003](https://openairdocs.org/sdr/CA050818003.md): Bulkhead · cracked · Aug 9, 2005 · Bag JETSTM3212 · Fuselage Main, Bulkhead > (CAN) CRACK ON FRONT PRESSURE BULKHEAD LT VERTICAL WEB, AT LT NOSE GEAR TRUNNION ATTACHMENT BRACKET TOP CENTER BOLT HOLE. - [SDR BMAC050010](https://openairdocs.org/sdr/BMAC050010.md): Connector · dirty · Aug 6, 2005 · N530PA · Jetair JETSTM4101 · Engine BMEP/Torque Indicating > ERATIC TORQUE +/- 4 PERCENT RT ENGINE INDICATION. MAINTENANCE CLEANED PLUG AT DELTA P/P TRANSDUCER IAW J31 MM 76-10-21, PERFORMED ENGINE RUN, OPS CHECKED GOOD AT THIS TIME. - [SDR CA050506011](https://openairdocs.org/sdr/CA050506011.md): Case · cracked · Apr 1, 2005 · Bag JETSTM3212 · Turbine Engine Compressor Section > (CAN) RT ENGINE FAILED TO MEET TAKEOFF TORQUE SETTING. EX ONLY GOT 90 PERCENT TORQUE ON A +7C, 1900 ASL (TRUE) DAY. SHOULD BE 104.5. ON INSPECTION, IT WAS FOUND THAT THE GAS GENERATOR CASE WAS CRACKED AT THE AIRFRAME SERVICE FLANGE. ENGINE REMOVED AND LOANER - [SDR CA050414008](https://openairdocs.org/sdr/CA050414008.md): Line · leaking · Mar 8, 2005 · Bag JETSTM4112 · Engine Fuel Distribution > (CAN) IT WAS NOTICED AFTER A FUEL NOZZLE CHANGE THAT THERE WAS FUEL LEAKING. FUEL LEAK WAS CAUSED BY CHAFING BY THE ADEL CLAMP THAT WAS ATTACHED TO THE TUBE ASSY. TUBE ASSY REPLACED. NO FURTHER PROBLEMS. - [SDR CA050308012](https://openairdocs.org/sdr/CA050308012.md): Bracket · cracked · Feb 24, 2005 · Bag JETSTM3212 · Leading Edge Devices > (CAN) FLAP SLAT BRACKET FOUND CRACKED DURING MAINTENANCE, CHECK THE CRACKS IN THOSE 3 BRACKETS ARE 1 INCH LONG LOCATED IN THE FORWARD RADIUS OF THE BENDS. - [SDR CA050131006](https://openairdocs.org/sdr/CA050131006.md): Engine · failed · Jan 19, 2005 · Bag JETSTM3212 · Engine (Turbine/Turboprop) > (CAN) ENGINE FAILED IN FLIGHT, AIRCRAFT HAD JUST EXITED ICING CONDITIONS, CONTINUOUS IGNITION WAS TURNED OFF A FEW MINUTES PRIOR TO ENGINE FAILURE. AIRCRAFT RETURNED TO BASE AND ENGINE WAS INSPECTED FOR ANY CAUSE OF THE FAILURE, NOTHING WAS FOUND. GROUND/POWE - [SDR CA050217003](https://openairdocs.org/sdr/CA050217003.md): Stud · failed · Jan 17, 2005 · Bag JETSTM3212 · Accessory Gearboxes > (CAN) GEARBOX COMPRESSOR BEARING RETAINING STUDS FAILED CAUSING THE NR 1 IDLER TO MISALIGN WITH THE FCU DRIVE TRAIN AND THE ROTATING GROUP TO MOVE FORWARD. - [SDR CA050131004](https://openairdocs.org/sdr/CA050131004.md): Starter Gen · failed · Jan 15, 2005 · Bag JETSTM3212 · Starter-Generator > (CAN) GENERATOR WENT OFF LINE, SMOKE AND OIL VISUAL ON COWLING. - [SDR CA050131007](https://openairdocs.org/sdr/CA050131007.md): Engine · failed · Jan 11, 2005 · Bag JETSTM3212 · Engine Oil System (Airframe Furnished) > (CAN) SOAP SAMPLE INDICATED MAJOR ALUMINIUM IN THE OIL SYSTEM, 2ND SOAP SAMPLE TAKEN AND FOUND MAGNESIUM AND CARBON STEEL PARTICLES IN THE SAMPLE. ENGINE REMOVED AND SENT FOR EVALUATION, AMO 50-04. - [SDR BMAC05001](https://openairdocs.org/sdr/BMAC05001.md): Windscreen · cracked · Jan 10, 2005 · N538PA · Bag JETSTM3101 · Flight Compartment Windows > PILOT REPORTED: DURING CLIMB OUT, (W/S) CAPTION APPEARED FOR THE RT WINDSCREEN. UPON FURTHER INSPECTION NOTICED CRACKS IN THE UPPER PORTION OF THE WINDSCREEN. CREW DECIDED TO RETURN TO DEPARTURE. REPLACED RT WINDSCREEN DUE TO CRACKING OF OUTER PANE. (K) - [SDR BMAC040019](https://openairdocs.org/sdr/BMAC040019.md): Handle · out of adjust · Jan 6, 2005 · N536PA · Bag JETSTM3101 · Passenger/Crew Doors > PILOT REPORTED: DOOR CAP LIGHT CAME ON DURING FLIGHT. PERFORMED DOOR HANDLE ADJUSTMENTS IAW AMM. OPS CHECKED GOOD AT THIS TIME. - [SDR BMAC040018](https://openairdocs.org/sdr/BMAC040018.md): Selector Switch · inoperative · Jan 3, 2005 · N535PA · Bag JETSTM3101 · Landing Gear Selector > PILOT REPORTED: ON TAKE-OFF, GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. RETURNED TO DEPARTURE. REMOVED AND REPLACED LANDING GEAR SELECTOR SWITCH IAW AMM. OPERATIONALLY CHECKED OK AT THIS TIME. (K) - [SDR BMAC040017](https://openairdocs.org/sdr/BMAC040017.md): Selector Valve · inoperative · Dec 29, 2004 · N531PA · Bag JETSTM3101 · Trailing Edge Flap Control System > UNCOMMANDED FLAP DEPLOYMENT IN FLIGHT VERIFIED VISUALLY TO APPROXIMATELY 20 DEGREES. FLAPS CONTINUED TO DEPLOY TOWARD 35. UPON LANDING FLAPS RETURNED TO ZERO VERIFIED VISUALLY UNCOMMANDED. NO HORN WAS HEARD WITH FLAPS DEPLOYED AND POWER LEVER BELOW 20 PERCE Next page: https://openairdocs.org/engine/garrett-tpe-331-10ug/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'TPE33110UG' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/engine/garrett-tpe-331-10ug/reports --- 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.