Garrett TPE331-6-252B

Service difficulty reports · 98

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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 = 'TPE3316252B'
  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 CA190516012Duct · melted(CAN) DURING THE INITIAL CLIMB OUT, THE PILOT FELT ABNORMAL HEAT EVEN THOUGH THE HEATING SYSTEM WAS CORRECTLY SET. A LITTLE WHILE AFTER, SMOKE EXITED FROM THE VENTILATION DUCTS. THE PILOT DECLARED AN EMERGENCY AND RETURNED TO THE DEPARTURE AIRPORT (XXXX) WITMay 15, 2019 · Beech B100 · Heating SystemSDR CA190506003A/C Pack · contaminated(CAN) RIGHT AFTER TAKE OFF PILOT NOTICED SMOKE IN THE CABIN. PILOT DID A CIRCUIT AND LANDED SAFELY. AIRCRAFT IS STILL UNDER INVESTIGATION. AIRCRAFT INSPECTED, ALL HEATING DUCTS INSPECTED FOR OVERHEAT AND FOUND SERVICEABLE, ELECTRICAL WIRING IN INSTRUMENT PANELApr 18, 2019 · Beech B100 · Cabin Cooling SystemSDR CA141015005A/C Pack · failed(CAN) HAD THREE FLOW PACK FAILURES AFFECTING THE PRESSURIZATION SYSTEM.Oct 1, 2014 · Beech B100 · Cabin Cooling SystemSDR CA130911007Gps · failed(CAN) DURING FLIGHT, THE GPS BECAME BLANK WITHOUT ANY INDICATION OR WARNING BLANK PAGE. THE ACFT DID A 90 DEGREE TURN AND RETURN TO DEPARTURE POINT. AFTER SHUTTING OFF THE MASTER THE DISPLAY CAME BACK NORMAL. GARMIN HAS BEEN ADVISED AND A NEW GPS HAS BEEN ISep 4, 2013 · Beech B100 · Global Positioning SystemSDR CA130904005Flap Track · cracked(CAN) UPON INSPECTION PHASE 2, RT OUTWARD FLAP TRACK, INNER TRACK FOUND CRACKED. TRACK HAS BEEN REPLACED.Aug 28, 2013 · Beech B100 · Trailing Edge FlapsSDR CA130626001Ignition Sys · shorted(CAN) DURING CLIMB THE START CONTROL LT BREAKER POP AT THE SAME TIME THE INDICATION OF EGT AND IGNITION WENT OFF. ACFT CAME BACK TO THE BASE AND MAINTENANCE ROUND THAT THE IGNITION UNIT WAS DEAD AND SHORT THIS WAS THE CAUSE OF THE START CONTROL LT BREAKER POPJun 18, 2013 · Beech B100 · Ignition Power SupplySDR CA121107006Fcu · defective(CAN) THE ACFT WAS TAXIING WHEN THE LT ENGINE STOPPED DURING GROUND IDLE MODE. AFTER VERIFICATION THE FCU WAS FOUND DEFECTIVE, IT WAS REPLACED AND EVERYTHING WAS BACK TO NORMAL. SEVERAL PROBLEMS WITH, FCU, 897800-8.Oct 31, 2012 · Beech B100 · Fuel Control/Turbine EnginesSDR CA120614001Skin · cracked(CAN) ON PREFLIGHT INSPECTION PILOT FOUND CRACK ON UPPER SUFACE CENTER OF RT AILERON.Jun 13, 2012 · Beech B100 · AileronsSDR CA120612001Skin · cracked(CAN) ON PREFLIGHT INSPECTION, THE PILOT FOUND A CRACK ON TOP SKIN OF RT AILERON.Jun 8, 2012 · Beech B100 · AileronsSDR CA120418008Engine · fire(CAN) AFTER SHUTDOWN FROM FLIGHT DURING POST FLIGHT OPERATIONS, THE PILOTS NOTICED BLACK SMOKE COMING FROM THE RT TAIL PIPE. THE PILOT HAND-TURNED THE PROP AND THUS TURNED THE ENGINE IN ORDER TO CLEAR THE SMOKE, BUT THE SMOKE GOT THICKER. THEY STOPPED HAND-PRApr 15, 2012 · Beech B100 · Engine (Turbine/Turboprop)SDR CA120314008Duct · melted(CAN) IN CLIMB, THE TEMPERATURE IN THE CABIN WAS REALLY HOT. PILOT PUT TEMP CONTROL OFF AND BLOWER HIGH. THEN SMOKE APPEARED IN COCKPIT. PILOT CAME BACK AND LANDED IN ST-HUBERT. MAINTENANCE CHECKED THE SYSTEM AND FOUND DUCT MELTED UNDER THE FLOOR. ALL RELEVANFeb 21, 2012 · Beech 100BEECH · Air Distribution SystemSDR CA120210002Torque Tube · cracked(CAN) DURING INSPECTION OF ELEVATOR TORQUE TUBE TORQUE FOUND CRACKED.Feb 2, 2012 · Beech B100 · Elevator StructureSDR CA120424008Tube · chafed(CAN) FOUND RUDDER TORQUE TUBE LOOSE AT BELLCRANK (RUDDER CONTROL) ATTACHMENT. THE RIVETS AROUND THE TUBE & FITTING WERE FOUND LOOSE & CHAFED AT A POINT THAT 1 RIVET HEAD WAS MISSING. RIVET HOLES WERE ELONGATED DUE TO CHAFING TOO.Dec 7, 2011 · Beech B100 · Rudder StructureSDR CA111213003Latch · broken(CAN) LATCH FOUND BROKEN IN TWO PIECES WHEN WE REMOVED SPINNER FOR PROPELLER LUBRICATION. LATCH REPLACED.Nov 29, 2011 · Beech B100 · Propeller AssemblySDR CA110712002Firewall · crackedDURING ROUTINE INSP, A CRACK HAS BEEN FOUND ON THE RT INBD WALL OF THE COLLECTOR TANK IN THE FIREWALL FUEL SHUTOFF REGION. REPAIR HAS BEEN DONE IAW THE MM.Jul 1, 2011 · Beech B100 · Nacelle/Pylon, Bulkhead/FirewallSDR CA110513008Line · misinstalledNR 1 VSI AS NOT INDICATING AFTER INITIAL CLIMB. DURING TROUBLESHOOTING AND PITOT STATIC TESTS, IT WAS OBSERVED THAT THE STATIC LINE THAT CONNECTED TO THE TEE ONTO THE BACK OF THE VSI DID A LOOP AND RE-CONNECTED TO THE OTHER SIDE OF THE SAME TEE. ESSENTIALLY May 11, 2011 · Beech B100 · Pitot/Static SystemSDR 2011FA0000136Fuel Nozzle · crackedAFTER TAKING OFF, LEFT ENGINE STARTED LOOSING POWER IN FLIGHT. PILOT DECIDED TO RETURN TO DEPARTURE. ACFT LANDED SAFELY. ACFT WAS THEN PLACED FOR INSPECTION. FOUND THE LT ENGINE SECONDARY FUEL MANIFOLD CRACKED AND LEAKING FUEL. CORRECTED THIS BY CLEANING Feb 14, 2011 · N500KD · Beech B100 · Fuel Injector NozzleSDR CA110211011Powerpack · malfunctionedLANDING GEAR WAS SELECTED UP BUT SOUNDED SLUGGISH. WHEN THE GEAR WAS SELECTED DOWN THE MOTOR RAN TILL 60 AMP BREAKER UNDER FLOOR POPPED. THE GEAR DID NOT DEPLOY. EMERGENCY EXTENSION WAS CARRIED OUT, 3 GREEN, AND LANDED SAFELY. THE ACFT WAS PUT IN THE HANGEFeb 11, 2011 · Beech C90A · Hydraulic System, MainSDR CA110225016Bearing · seized(CAN) APPROACHING THE AIRPORT, PILOTS NOTICED THE "START GEN" ANNUNCIATOR TO ILLUMINATE (LIGHT UP). A FEW MINUTES AFTERWARDS, THEY SAW SPARKS COMING OUT FROM THE ENGINE. FOR PRECAUTION, THEY SHUTDOWN THE ENGINE AND THEY LANDED WITHOUT ANY PROBLEMS. AFTER Feb 4, 2011 · Beech B100 · Starter-GeneratorSDR CA101118003Skin · crackedTHE TOP SKIN OF THE RT AILERON WAS FOUND CRACKED BETWEEN SECOND AND THIRD INBOARD RIBS ON 5 INCHES ALONG AILERON SPAR AND TWO 3 INCHES LONG CRACKS WERE PERPENDICULAR TO THE SPAR.Nov 17, 2010 · Beech B100 · AileronsSDR CA101020002Torque Sensor · brokenTHE TORQUE SENSOR ASSY PN 3101726-3 FAILED. GEAR, PN 3103589-1, WAS FOUND WITH THE INTERNAL SPLINES STRIPPED. SPLINED DRIVE GEARSHAFT, PN 3103405-2, WAS ALSO FOUND STRIPPED. WHEN THESE PARTS FAILED THE INTEGRITY OF THE FCU DRIVE TRAIN WAS LOST AND THE ENGINESep 27, 2010 · Beech B100 · Engine BMEP/Torque IndicatingSDR CA100823001Switch · unserviceableAFTER T/O PILOT REPORT THAT THE GEAR WILL NOT COME IN. HE FLEW THE ACFT GEAR DOWN AND RETURN TO MX BASE. SWITCH V3-1 ROUND UNSERVICEABLE IN THE EMERGENCY HANDLE CIRCUIT. SWITCH REPLACED AND RETURN TO SERVICE.Aug 18, 2010 · Beech B100 · Landing Gear Retraction/Extension SystemSDR CA100127015Bracket · worn(CAN) DURING A ROUTINE INSP OF THE FLAP SYS. DISCOVERED THAT MANY BRGS WERE USED INSIDE THE BRACKETS. EXCESSIVE SIDE PLAY CAUSED WEAR OF FLAP BRACKETS. HAD TO CHANGE THE DAMAGED BRACKETS, ALSO THE BRGS AND THE WASHERS OF TEFLON. A THOROUGH INSP OF OUR FLEETJan 10, 2010 · Beech B100 · Trailing Edge FlapsSDR CA091202018Shutoff Valve · malfunctioned(CAN) BOTH FLOW PACKS INSTALLED ON AIRCRAFT CHECKED ON GROUND RUN, VERY SLOW TO PRODUCE PRESSURIZATION ON EITHER SIDE. TESTED BOTH SIDES IN HANGAR IAW MM, FOUND FIRE WALL SHUTOFF VALVE WOULD NOT OPEN AT SPECIFIED PRESSURE. LEFT SIDE REQUIRED 30 PSI AND OVER Nov 30, 2009 · Beech B100 · Air Distribution SystemSDR CA091113002Valve · malfunctioned(CAN) DURING START UP, THE ENG DID NOT START. THE PILOT NOTICED THAT THERE WAS NO FUEL FLOW RISE UP AND NO ITT. HAVE REPLACED THE FUEL VALVE AND THE ENGINE STARTED NORMALLY.Sep 29, 2009 · Beech 100BEECH · Engine Fuel DistributionSDR 9JL2009F00000Tube · crackedDURING ENGINE START, CREW NOTED A LARGE AMOUNT OF FLUID LEAKAGE FROM NR 1 ENGINE COWLING. ENG WAS IMMEDIATELY SHUTDOWN. MX DISCOVERED THE FUEL ENRICHMENT LINE FROM THE FUEL HEATER TO THE FUEL PUMP WAS LAKING. INSP OF THE TUBE REVEALED A HAIRLINE CRACK AT THAug 31, 2009 · N700BA · Beech B100 · Engine Fuel DistributionSDR CA080724004Indicator · malfunctioned(CAN) WHILE RETURNING TO HOME BASE AT CRUISE FLIGHT, FLIGHT CREW NOTICED THAT THE LT ITT GAUGE WAS ERRATIC. THERE WAS NO NOTICE IN ENGINE PERFORMANCE NOR WERE ANY OF THE REMAINING ENGINE INSTRUMENTS SUPPORTING ENGINE PERFORMANCE ISSUES. UPON RETURN TO BASE, MAJul 21, 2008 · Beech 100BEECH · Engine Temperature Indicating SystemSDR CA080708004Circuit Breaker · failed(CAN) ACFT DEPARTED, OR AFTER SCHEDULED MAINT WAS COMPLETED. IN THE CLIMB OUT IT WAS NOTICED BY THE CREW THAT THE LANDING GEAR FAILED TO RETRACT. THE ACFT LANDED WITHOUT INCIDENT. UPON INSP IT WAS FOUND THAT THE CIRCUIT BREAKER HAD FAILED BUT HAD NOT ACTUALLY Jun 26, 2008 · Beech 100BEECH · Landing Gear Retraction/Extension SystemSDR CA080103005Wire Harness · failed(CAN) AFTER A STOPOVER THE AIRCREW WENT TO START THE NR 2 ENGINE, AT THIS TIME IT WAS NOTED THAT THE ITT GAUGE WAS NOT WORKING. MAINTENANCE PERSONNEL FLEW TO THE AIRCRAFT LOCATION AND THROUGH TROUBLESHOOTING DETERMINED THAT THE ITT HARNESS HAD FAILED. A FERRY Dec 28, 2007 · Beech 100BEECH · Engine Indicating System WiringSDR CA071011001Motor · unserviceable(CAN) IN DESCENT FOR LANDING, THERE WERE ONLY 2 GREEN GEAR DOWN INDICATION LIGHTS INSTEAD OF THREE. AFTER RECYCLING THE GEAR, THE PROBLEM PERSISTED. THE EMERGENCY LANDING GEAR SYSTEM WAS DEPLOYED AND THE 3 GREEN LIGHTS WERE ON AS REQUIRED. AIRCRAFT LANDED WITSep 14, 2007 · Beech B100 · Landing Gear Retraction/Extension SystemSDR CA070827006Connector · melted(CAN) WHILE IN FORMATION FLIGHT, THE LT (BATTERY CHARGE) LIGHT CAME ON AND STAYED ON FOR 15 MINUTES AND THEN EXTINGUISHED. AFTER LANDING AND ENGINES SHUTDOWN, THERE WAS NO MORE POWER COMING FROM THE BATTERIES. AN INSPECTION WAS CARRIED OUT AND THE LT BATTERY Jul 27, 2007 · Beech B100 · Electrical Power System WiringSDR CA070530002Elt · failed(CAN) WHEN TESTING ELT FOR THE REQUIREMENT OF CAR 571 APPENDIX G FOUND G SWITCH WOULD NOT ACTIVATE. (TC NR 20070530002)May 30, 2007 · Beech 100BEECH · Emergency Locator BeaconSDR VOX2007F00000Cowling · damagedUPPER RT COWLING CAME OPEN IN FLIGHT. RECOMMEND INSTALLING 2 SCREWS AT LEADING EDGE OF COWLING TO PREVENT THIS HAPPENING. (K)Apr 4, 2007 · N740PB · Mtsbsi MU2B36 · Nacelle/Pylon, Plate/SkinSDR CA070223002Wire Harness · failed(CAN) FLIGHT CREW DID ATTEMPTED AN ENGINE START NR 2 ENGINE WITH NO SUCCESS. AFTER MAINTENANCE HAD CORRECTED THE PROBLEM ASSOCIATED WITH THE FAILED START, THE CREW PROCEEDED TO CARRY OUT ANOTHER ENGINE START. ONCE THE ENGINE LIT OFF THE CREW NOTED THAT THE ITTFeb 20, 2007 · Beech 100BEECH · Engine Indicating System WiringSDR CA070206002Landing Gear · unknown(CAN) LANDING GEAR (IN TRANSIT) LIGHT STAYED ON AFTER GEAR UP SELECTION AFTER TAKEOFF. GEAR DOWN SELECTED AND GEAR WENT DOWN AND LOCKED NORMALLY (3 GREEN LIGHTS) FOR LANDING BACK TO DEPARTURE AIRPORT. AIRCRAFT JACKED, RETRACTIONS DONE, LANDING GEARS INSPECTEDFeb 5, 2007 · Beech B100 · Landing Gear Position and WarningSDR CA070208002Window · departed(CAN) AFTER TAKEOFF AND CLIMB TO APPROXIMATELY 10,000 FEET, THE LT. (TC NR 20070208002)Jan 28, 2007 · Beech B100 · Flight Compartment WindowsSDR CA061218009Torque Tube · cracked(CAN) DURING COMPLIANCE WITH SB 2145, CHANGED OUT THE DUE TORQUE TUBES AND REPLACE THEM WITH INSPECTED ONES. WHEN THE LT WAS REMOVED A CRACK WAS NOTED GOING FROM THE TAPER PIN HOLE TO THE EDGE OF THE TORQUE TUBE MOUNT BRACKET. IT APPEARS THAT THE PIN WAS OVER-Dec 15, 2006 · Beech B100 · Elevator StructureSDR CA061218011Torque Tube · cracked(CAN) DURING COMPLIANCE WITH SB 2145 (REMOVED THE DUE TUBES TO SEND OUT FOR NDT AND REPLACE WITH INSPECTED SERVICEABLE ONES), A CRACK WAS DISCOVERED RADIATING FROM ONE OF THE TAPER PIN HOLES TO THE EDGE OF THE ATTACH BOSS ON THE LT TUBE. IT APPEARS THAT THE TADec 15, 2006 · Beech B100 · Elevator StructureSDR CA061215002Hinge · damaged(CAN) DURING PHASE NR 2 INSPECTION, IT WAS NOTICED THAT THE LT ELEVATOR WAS LOOSE AT THE OB HINGE. AREA INSPECTED AND FOUND THAT THE 4 BOLTS THAT ATTACH THE HINGE TO THE HORIZONTAL STAB WERE LOOSE. THE HINGE WAS REMOVED AND FOUND THAT THE HOLES WERE ELONGATEDDec 12, 2006 · Beech 100BEECH · Elevator StructureSDR BVX2006F00000Gearbox · failedIMPROPER ASSEMBLY OF THE DETAILED MOTOR GEARBOX CAUSED 2 MLG ACTUATOR IN FLIGHT FAILURES, RESULTING IN THE AIRCRAFT BEING DIVERTED FOR 2 FLIGHTS. THE IMPROPER ASSEMBLY REVOLVED AROUND THE CAM THAT ACTUATES THE LIMIT SWITCHES. THIS CAM IS SUPPOSED TO BE PN 99Aug 14, 2006 · N111YF · Beech B100 · Landing Gear Retraction/Extension SystemSDR CA060504006Torque Tube · wornWHILE CHECKING THE ELEVATOR SYSTEM FOR FREEDOM OF MOVEMENT, EXCESSIVE PLAY WAS NOTICED IN THE LEFT ELEVATOR. THE PLAY WAS ISOLATED TO THE ELEVATOR TORQUE TUBE FITTING. THE TORQUE TUBE WAS REPLACED WITH A NEW ASSEMBLY. THE TORQUE TUBE WAS INSPECTED AND FOUND May 3, 2006 · Beech B100 · Elevator StructureSDR CA060406002Torque Tube · corrodedDURING AN INSPECTION OF THE ELEVATOR TORQUE TUBE, THE PRIMARY ELEVATOR TORQUE TUBE WAS FOUND CORRODED. THE PART WAS REPLACED.Apr 3, 2006 · Beech B100 · Elevator StructureSDR CA060405003Adapter · crackedDURING AN INSPECTION OF THE "OIL FILTER ADAPTER", IT WAS FOUND CRACKED IN TWO PLACES. A SMALL OIL LEAK WAS EVIDENT. THE PART WAS REPLACED.Mar 16, 2006 · Beech B100 · Turbine Engine Oil SystemSDR CA051202003Control Panel · burnedA BURNT ODOR WAS NOTICED FOLLOWED BY SMOKE IN THE COCKPIT, COMING FROM THE TRIM INDICATOR LIGHT PANEL. THE PILOT CLOSED THE RHEOSTAT AND RETURNED TO BASE. AFTER INSPECTION OF THE LIGHT PANEL, HUMIDITY WAS FOUND UNDER THE PANEL, WHICH CAUSED A SHORT CIRCUIT. Nov 25, 2005 · Beech B100 · Flight Compartment LightingSDR CA051130004Fire Detector · failed(CAN) WHEN THE INDICATOR (LT ENGINE FIRE) ILLUMINATED, THE ENGINE WAS SHUTDOWN BY THE PILOT, AND PUT INTO FEATHER. AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNEDTO BASE. AFTER VERIFICATION, NO ENGINE FIRE WAS EVIDENT. THE INDICATORS WERE VERIFIED AND THE AIRNov 22, 2005 · Beech B100 · Fire DetectionSDR CA051109002Stringer · crackedDURING AN INSPECTION OF THE ELEVATOR CABLES, AFT OF THE REAR PRESSURE BULKHEAD, THE ENGINEER DISCOVERED A CRACK IN THE NR 10 STRINGER OF THE AFT PRESSURE BULKHEAD. THIS AIRCRAFT HAS A CVR INSTALLED IAW STC 'SA-02-26' AND THE MOUNTING TRAY FOR THE CVR TIES INTNov 7, 2005 · Beech B100 · Fuselage Main, Longeron/StringerSDR CA051025007Barrel · brokenFLIGHT CREW REPORTED LOSS OF NOSE WHEEL STEERING DURING TAXI. MAINTENANCE FOUND THE NOSE WHEEL BARREL ASSY BROKEN. SLOTS WHICH HOLD IN SPRING RETAINER FOUND BROKEN ALLOWING SPRING TO LOSE TENSION. MX REPLACED THE ASSY AND RELEASED AIRCRAFT FOR RETURN TO SEROct 24, 2005 · Beech B100 · Wheel/Ski/FloatSDR CA051004006Fire Detector · failed(CAN) AFTER TAKE OFF AN (ENGINE FIRE) INDICATION FOR THE RT ENGINE ILLUMINATED. PILOT SHUT DOWN THE ENGINE AND LANDED ON ONE ENGINE. AFTER INSPECTION OF THE SYSTEM, NO FAULT FOUND, SYSTEM NORMAL. AIRCRAFT RETURNED TO SERVICE.Sep 26, 2005 · Beech B100 · Fire DetectionSDR CA050921001Door Frame · cracked(CAN) DURING A DAILY INSPECTION 2 CRACKS WERE DETECTED ON EACH SIDE OF THE UPPER ATTACHMENT FOR THE REAR DOOR. THE PART WAS REPLACED.Sep 16, 2005 · Beech B100 · Fuselage Main, StructureSDR CA050824012Torque Tube · cracked(CAN) WHILE CARRYING OUT A PHASE 2 AND 3 INSPECTION, THE RT ELEVATOR TORQUE TUBE HAD A .5 INCH CRACK. THE CRACK WAS DISCOVERED BETWEEN THE ELEVATOR AND TORQUE TUBE. THE TORQUE TUBE WAS REPLACED.Aug 3, 2005 · Beech B100 · Elevator Control System
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