Garrett TPE331-10R

Service difficulty reports · 88

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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 = 'TPE33110R'
  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 39LA2014082696Rib · corrodedTOP INNER RIB OF LT HORIZONTAL STABILIZER AT INBD ATTACH FITTING FOUND CORRODED BEYOND LIMITS. REPLACED INNER RIB AS REQUIRED.Aug 26, 2014 · N621AR · Casa C212DF · Horizontal Stabilizer, Spar/RibSDR 39LA2014082084Window Frame · corrodedDURING WINDSHIELD REMOVAL AT HEAVY CHECK CORROSION FOUND ON THE COPILOT’S WINDSHIELD FRAME LOWER SECTION. REPAIRED IAW EO 12032-2036 SUPPORTED BY FAA FORM 8110-3.Aug 20, 2014 · N621AR · Casa C212DF · Flight Compartment WindowsSDR 39LA2014082085Window Frame · corrodedDURING WINDSHIELD REMOVAL AT HEAVY CHECK CORROSION FOUND ON THE COPILOT'S WINDSHIELD FRAME LOWER SECTION. REPAIRED IAW EO 12032-2036 SUPPORTED BY FAA FORM 8110-3.Aug 20, 2014 · N621AR · Casa C212DF · Flight Compartment WindowsSDR 39LA2014082086Window Frame · corrodedDURING WINDSHIELD REMOVAL AT HEAVY CHECK CORROSION FOUND ON THE COPILOT'S WINDSHIELD FRAME INBD VERTICAL SECTION. REPAIRED IAW EO 12032-2036 SUPPORTED BY FAA FORM 8110-3.Aug 20, 2014 · N621AR · Casa C212DF · Flight Compartment WindowsSDR 39LA2014082087Window Frame · corrodedDURING WINDSHIELD REMOVAL AT HEAVY CHECK CORROSION FOUND ON THE COPILOT'S WINDSHIELD FRAME INBD VERTICAL SECTION. REPAIRED IAW EO 12032-2036 SUPPORTED BY FAA FORM 8110-3.Aug 20, 2014 · N621AR · Casa C212DF · Flight Compartment WindowsSDR CA140617002Shaft · sheared(CAN) AS PILOT ATTEMPTED TO TAXI AWAY FROM DOCK HE REALIZED HE COULDN`T GET OFF THE STOP LOCKS, MEANING HE HAD LITTLE OR NO REVERSE. AIRCRAFT REPAIR SERVICE REMOVED THE PLANE FROM THE WATER & INSPECTED THE PILOTS DEFECT. IT WAS THEN WE HAD REALIZED AFTER TRYJun 16, 2014 · Dhav DHC3 · Fuel Control/Turbine EnginesSDR 3RAA20140520001Gear · failedDURING A JUMP RUN, WHILE IN CRUISE, THE LT ENGINE CHIP LIGHT FLICKERED MOMENTARILY & THEN THE ENGINE SHUT DOWN. RETURNED TO THE DEPARTURE & LANDED WITHOUT FURTHER INCIDENT. SUSPECT CATASTROPHIC FAILURE OF THE LT ENGINE. R & R ENGINE. ACFT RETURNED TO SERVMay 19, 2014 · N467CS · Casa C212200 · Turbine Engine Reduction GearSDR 39LA2014030561Engine · fluctuatesEN ROUTE DURING CRUISE FLIGHT BETWEEN OAMS & OAIX AT 13,500 FEET, THE FLIGHT CREW NOTICED THE TORQUE FLUCTUATED ON THE NR 1 ENG FROM 89% TO 110% NON-COMMANDED. AS A PRECAUTION, THE NR 1 ENG WAS SHUT DOWN. FLIGHT CREW DECLARED AN EMERGENCY & LANDED WITHOUT INMar 5, 2014 · N603AR · Casa C212CC · Engine (Turbine/Turboprop)SDR 3RAA2014FA0000064Support · crackedDURING A ROUTINE INSPECTION, MAINTENANCE DISCOVERED THE PILOT'S RUDDER PEDAL ADJUSTMENT SHAFT SUPPORT CRACKED. AIRCRAFT WAS TAKEN OUT OF SERVICE AND REPLACEMENT PART IS ON ORDER.Feb 10, 2014 · N495CS · Casa C212CC · Rudder Control SystemSDR 8EKA20140206001Coupling · crackedDURING 400HR SCHEDULED INSPECTION MECHANIC FOUND NR 2 ENG FIRE SHIELD AUGMENTER FLANGE COUPLING ATTACHED TO FIREWALL CRACKED APPROXIMATELY 80% AROUND CIRCUMFERENCE. REMOVED & RE-INSTALLED ENG & PROPELLER TO FACILITATE REMOVAL & REPLACEMENT OF COUPLING WITH NEJan 23, 2014 · N348CA · Casa C212CC · Engine FiresealsSDR 39LA2013122642Skin · corrodedDURING CPCP INSPECTION, FOUND CORROSION ON LT WING TE AT CTR OF INBD FLAP, BETWEEN WING STATION 1266 & 2620.Dec 26, 2013 · N4399T · Casa C212DF · Wing, Plate/SkinSDR 8EKA20140124002Stringer · crackedCRACKS ON & IN THE VICINITY OF THE AFT UPPER DOOR WERE FOUND. ON 22-NOV-13 5 CRACKS WERE REPAIRED IAW THE SRM. THE ACFT WAS FLOWN UNTIL 27-NOV-13 WHEN THE DOM BECAME AWARE OF THE CRACKS, UPON READING THE E-MAIL & THEN PULLED THE ACFT OUT OF SERVICE. THIS E-Nov 5, 2013 · N348CA · Casa C212CC · Cargo/Baggage DoorsSDR 3RAA2013212001Wire · chafedTHE LEFT ENGINE FIRE WARNING LIGHT FLICKERED DURING THE TAKEOFF ROLL. THE CO-PILOT CALLED THE LIGHT AND THE PIC ABORTED THE TAKEOFF. NO SECONDARY INDICATIONS WERE OBSERVED. PIC CONFIRMED THAT THE ENGINE WAS NOT ON FIRE AND PERFORMED A NORMAL SHUTDOWN. MAINMay 9, 2013 · N467CS · Casa C212 · Fire Protection System WiringSDR 39LA2013032200004Engine · vibrationUPON POWER REDUCTION TO FLIGHT IDLE, IN FLIGHT, AT 1600FT AGL, THE NR 1 ENGINE EXHIBITED MASSIVE VIBRATION AND TORQUE/RPM FLUCUATION. NR 1 ENGINE WAS SHUTDOWN IAW EMERGENCY PROCEDURES UPON LANDING.Mar 19, 2013 · N969BW · Casa C212CC · Engine (Turbine/Turboprop)SDR EHAA20130211002Engine · power lossFIFTEEN MINUTES INTO THE FLIGHT, THE NR 1 ENGINE EXPERIENCED A MOMENTARY POWER LOSS OF ABOUT TEN PERCENT TORQUE. ALL THE GAUGES INDICATED THE SAME AND THE ACFT YAWED IN THAT DIRECTION. THIS LASTED ONLY A SECOND OR TWO, BUT A FEW MINUTES LATER THE SAME THING Feb 11, 2013 · N502FS · Casa C212CD · Engine (Turbine/Turboprop)SDR 39LA2013020600024Connector · failedNR 2 ENGINE, SRL BOTH, TORQUE IN CLIMB DROPPED TO 60 PERCENT, EGT DROPPED TO 545 AND FUEL FLOW DROPPED TO 300 PPH. SRL TO ONLY, ALL NORMAL.Feb 5, 2013 · N969BW · Casa C212CC · Engine Indicating System WiringSDR 39LA2013011800003Indication Sys · malfunctionedON CLIMB OUT, RT ENGINE EGT BEGAN TO FLUCTUATE BETWEEN 200- 400 DEGREES. CLIMB POWER WAS SET PRIOR TO FLUCTUATION, EGT READING WAS ERRONEOUS. POWER REDUCED TO PRECLUDE AN INADVERTENT EGT OVER TEMP. SHORTLY AFTER, EGT FLUCTUATIONS BECAME LARGER CAUSING THE EJan 17, 2013 · N969BW · Casa C212200 · Engine Indicating SystemSDR 39LA2013011500013Sensor · dirtyON CLIMB OUT, ABOUT 8 MILES FROM DPRATURE, RT ENGINE STARTED TO SURGE BETWEEN 95 -60 PERCENT TORQUE, AND 650- 250 EGT. RETURNED TO DEPARTURE. AS ACFT LEVELED OFF AND STARTED TO DESCEND THE ENGINE RAN NORMALLY. NO OTHER ABNORMALITIES WERE NOTED AND LANDINGJan 15, 2013 · N605AR · Casa C212200 · Engine (Turbine/Turboprop)SDR KGBR2012070600001Spar · corrodedLT WING, UPPER FWD SPAR AFT HORIZONTAL LEG, EXFOLIATED AT APPROX WS 3496, ALSO PROBABLE EXFOLIATION AT WS 2130 TO 2450 AND POSSIBLE EXFOLIATION AT WS 2900 TO 3000.Jul 6, 2012 · N602AR · Casa C212200 · Wing SparSDR STZA2011F00151Wire Harness · corrodedPRIMARY LT FUEL BOOST PUMP LOST POWER. ACFT SAFELY RETURNED TO ORIGINATING AIRPORT. FOUND THAT THE PUMP WIRE HARNESS (THE INTEGRAL WIRES FROM THE PUMP TO THE CONNECTOR) WAS CORRODED.Jun 23, 2011 · N502FS · Casa C212200 · Fuel Boost PumpSDR CA110419011Bracket · corroded(CAN) DURING ANNUAL ACFT INSPECTION, THE DETACHABLE BOTTOM PART OF THE OLD STYLE BRACKET WAS REMOVED FOR INTERNAL INSPECTION. HEAVY CORROSION WAS EVIDENT AND THE PART WAS REJECTED. A NEW STYLE BRACKET, PN C3FS169-11 WAS INSTALLED AND THE ACFT WAS RETURNED TOApr 18, 2011 · Dhav DHC3 · Rudder StructureSDR CA110420009Engine · failed(CAN) WHILE RETURNING TO THE AIRPORT, THE ACFT RT ENGINE FAILED AND THE PROPELLER WAS THEN FEATHERED. TO THE BEST OF MY KNOWLEDGE, APPROXIMATELY 18 MINUTES LATER, THE SECOND ENGINE FAILED AND THAT PROPELLER WAS ALSO FEATHERED. AN EMERGENCY LANDING WAS THEN CApr 1, 2011 · Casa C212CC · Engine (Turbine/Turboprop)SDR BIGA20110114001Trunnion · misinstalledDURING INSPECTION IT WAS FOUND THAT THE UPPER SUPPORT TRUNNION HOLDING THE TOP OF THE NOSE GEAR STRUT WAS HITTING THE MOUNT ON THE FUSELAGE. IT LOOKED AS THOUGH THE TRUNNION WAS INSTALLED UPSIDE DOWN DUE TO THE COLLAR HITTING THE EDGE OF THE FUSEALGE MOUNT, AJan 14, 2011 · N112BH · Casa C212200 · Fuselage, Landing Gear Attach FittingsSDR 2010FA0000776Attach Bracket · crackedDURING A ROUTINE CORROSION INSP, A MX FOUND A CRACK IN THE CTR WING LOWER ATTACH FITTING FRON THE FWD BOLT HOLE TO THE END OF THE FITTING, MX REMOVED THE OUTER WING FROM THE CTR WING AND PERFORMED NDT INSP ON ALL ATTACH FITTINGS. DURING THE NDT THE OUTER WING Aug 3, 2010 · N495CS · Casa C212CC · Wing, Attach FittingsSDR A8OA090717001Unknown · unknownAPPROX 15 MIN AFTER DEPARTURE, NR 2 GEN LIGHT CAME ON. SUCCESSFUL RESET. 5-10 MIN LATER SUDDEN YAW TO RIGHT. CREW SUSPECTED ENG FAILURE. CONFIRMED, SECURED ENGINE & RETURNED TO DEPARTURE. SUSPECTED HIGH EGT TEMPS NO RESTART ATTEMPT. LANDED SAFELY WITH NO INJul 17, 2009 · N423C · Casa C212CC · Engine (Turbine/Turboprop)SDR CA090521001Cable · damaged(CAN) ACFT DEPARTED DEEP SNOW AND PIC NOTICED ABNORMAL INPUTS IN THE RUDDER PEDALS UPON CLIMB OUT. GROUND PERSONNEL CONFIRMED TAIL SKI HANGING DOWN FARTHER THAN NORMAL. UPON LANDING, THE TAILSKI IMPACTED THE RWY AND NOSED OVER WITH THE DESTRUCTION OF TAIL SKI May 9, 2009 · Dhav DHC3 · Wheel/Ski/FloatSDR P4Y2008F00004Turbine Blades · failedHAVE RECEIVED AN ENGINE THAT HAS SUFFERED AN INFLIGHT FAILURE AND SHUTDOWN. UPON INITIAL INVESTIGATION WE HAVE IDENTIFIED THAT A 1ST STAGE TURBINE WHEEL BLADE APPEARS TO HAVE FAILED IN THE ROOT AREA. THIS BLADE HAS CAUSED SUBSTANTIAL DAMAGE TO THE REMAINDER Sep 8, 2008 · N962BW · Casa C212200 · Turbine SectionSDR BIG2008F00000Pitch Control · malfunctionedON THE LT ENG WITH THE SPEED LEVERS EET AT 100 PERCENT AND YOU TRY TO BRING THE POWER LEVER BACK TO CRUISE, AT ABOUT 70 PERCENT TO 80 PERCENT TORQUE THE RPM DROPS TO 93 PERCENT. TORQUE TEMP AND FUEL FLOW WILL INCREASE TO A HIGHER SETTING ON ITS OWN MAKING CONJul 14, 2008 · N107BH · Casa C212CC · Propeller Controlling SystemSDR CA080404005Shutoff Valve · unserviceableENGINE WOULD NOT SHUT DOWN USING NORMAL SHUT DOWN PROCEDURES. EMERGENCY SHUTOFF PROCEDURES USED. TROUBLESHOOTING FOUND FUEL SHUTOFF VALVE U/S (SOLENOID STICKING). REPLACED FUEL SHUTOFF VALVE. ENGINE RUN-UP AND SHUT DOWN NORMAL. AIRCRAFT RETURNED TO SERVICMar 31, 2008 · Dhav DHC3 · Fuel Selector/Shut-Off ValveSDR 2008FA0000125Gear · brokenENGINE RECEIVED WITH BROKEN FEATHER VALVE, NOSE CONE NUTS LOOSE, ROTATION OF ENGINE ROTATING COMPONENTS FOUND CLUNKY AND SEIZED. MAGNETIC PLUG CONTAMINATED WITH FINE METAL PARTICLES. NOSE CONE AND DIAPHRAGM REMOVED TO INVESTIGATE CAUSE OF FAILURE. WHEN DIAPFeb 12, 2008 · N961BW · Casa C212CC · Turbine Engine Reduction GearSDR DSC4331DL6292Retainer Seal · crackedNO GEARCASE NEGATIVE PRESSURE INDICATED DURING ENGINE TEST STAND FUNCTIONAL TESTING. TROUBLESHOOTING FOUND CRACKS IN SEAL RETAINER. SUBJECT RETAINER IS MADE WITH ALUMINUM. OLDER PN 693905-10 IS MADE WITH STEEL. SB 72-0224 AUTHORIZED INSTALLATION OF ALUMINUMJan 10, 2008 · Turbine Engine Reduction GearSDR CA070724002Cable · frayed(CAN) DURING A 100/150 HOURS INSPECTION, THE ELEVATOR, LOWER TRIM CABLE (P/N: C3CF348-7) WAS FOUND FRAYED IN (2) LOCATIONS. THE FIRST LOCATION WAS IN THE PEDESTAL AREA WHERE THE TRIM CABLE ATTACHES TO THE ELEVATOR TRIM DRUM ASSEMBLY (P/N: C3CF222-3). IT APPEARJul 11, 2007 · Dhav DHC3 · Elevator Tab Control SystemSDR 200700114Stiffener · crackedWHILE PERFORMING CASA COM LETTER 212-224 AND CASA SB 212-57-57-30, A CRACK WAS NOTED FROM THE 4TH RIVET TO THE 5TH RIVET FROM THE BOTTOM, ON THE VERTICAL STIFFINER LOCATED ON THE LT WING AT STA 4700, AFT SPAR WEB. THREE STIFFINERS NEXT TO THE ORIGINAL ARE CRAJan 30, 2007 · N515RL · Casa C212 · Wing Miscellaneous StructureSDR CA060728007Engine · vibrates(CAN) DURING DESCENT FOR FLOAT LANDING ON WATER, PILOT NOTICED VIBRATION IN ENGINE . ENGINE SHUTDOWN, PROP FEATHERED. AIRCRAFT LANDED WITHOUT INCIDENT. ENGINE REMOVED SENT TO REPAIR FACILITY. (TC NR 20060728007)Jul 27, 2006 · Dhav DHC3 · Engine (Turbine/Turboprop)SDR CA060214003Control Cable · broken(CAN) DURING ROUTINE MAINTAENANCE INSPECTION, SEVERAL WIRES FOUND BROKEN ON RT AILERON CONTROL CABLE AS IT PASSES AROUND CABLE PULLEY AT FRAME 4. PULLEY FOUND SEIZED TO BOLT. CABLE, PULLEY AND BOLTS REPLACED. (TC NR 20060214003)Feb 7, 2006 · Casa C212CC · Aileron Control SystemSDR 20050615Lock Plate · separatedINSP MX RUN-UP, VIBRATION NR 2 PROP ASSY, VIBRATED A FEW SEC THEN DIMINISHED. DISCOVERED 2 SAFETY WIRED BOLTS HEADS ON GROUND THAT SNAPPED OFF PROP ASSY. SPINNER HAD PUNCTURE DAMAGE, MINOR DAMAGE TO 2 PROP BLADES. SPINNER REMOVED, 2 LOCK WIRED BOLTS HAD SHEJun 15, 2005 · Casa C212CC · Propeller AssemblySDR 20040209Selector Valve · failedDURING LANDING ROLL-OUT AC VEERED LT. PC WAS STILL ON FLT CNTRLS (CONTROL YOKE, POWER LEVERS, AND RUDDERS) WITH FULL RT RUDDER INPUT AND PWR LEVERS IN FULL REVERSE. PC WAS APPLYING BRAKES. GO-AROUND WAS NOT AN OPTION AS THERE WAS NOT ENOUGH RUNWAY, NOR TIME May 26, 2004 · Casa C212CC · Steering UnitSDR 20010411CW005Engine · making metalON DOWNWIND LEG AT 2000 FT PILOT NOTICED NR 2 ENGINE TORQUE GAGE READ 0. COPILOT VISUAL OF NR 2 PROP REPORTED AS FEATHERED EMERGENCY HANDLE ACTIVATED AND UNEVENTFUL LANDING MADE. SUBSQUENT ENGINE START FAILED. NEXT START ATTEMPT FOLLOWING DAY FOR TROUBLEMar 6, 2001 · N422CA · Casa C212CC · Engine (Turbine/Turboprop)
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