U/A Canada PT6A-60A

Service difficulty reports · 596

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 = 'PT6A60A'
  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 CA050607006Windshield · failed(CAN) DURING CRUISE AT FL260 THE INNER PANE OF THE RT WINDSHIELD SHATTERED WITH A LOUD BANG, STARTLING THE CREW AND PASSENGERS. THERE IS NO APPARENT REASON FOR THE FAILURE. THE LT WINDSHIELD INNER PANE SHATTERED AND WAS REPLACED IN SEPTEMBER OF 2004 AT 1879.7 Jun 2, 2005 · Beech B300B350C · Flight Compartment WindowsSDR 2005FA0000823Bearing · seizedPILOT REPORTED RT ENGINE SURGING, SMOKE FROM EXHAUST SIMULTANEOUSLY WITH RT GENERATOR GOING OFF LINE IN CRUISE FLIGHT. FOUND RT STARTER/ GENERATOR ANTI-DRIVE (BRUSH END) BEARING SEIZED, INPUT SHAFT INTACT. REPLACED STARTER/GENERATOR AND EXAMINED OIL FILTER May 26, 2005 · N350TT · Beech B300 · Starter-GeneratorSDR ACE051805Windshield · crackedPILOT REPORTED LT WINDSHIELD CRACKED OUTER PLY VERIFIED CRACKED - REPLACED WINDSHIELD (WITHIN MFG. WARRANTY PERIOD).May 18, 2005 · N111AX · Beech 1900C · Flight Compartment WindowsSDR 2005FA0000736Connector · damagedLT WINDSHIELD HEAT FOUND BURNED/OVERHEATED WIRING CONNECTOR AT CENTER ELEMENT POSITIVE WIRE ATTACH TOP OB CORNER OF WINDSHIELD. NO DAMAGE TO WIRING NOTED. SYSTEM WAS PREVIOUSLY INSPECTED IAW SB. ALL ITEMS CHECKED SATISFACTORY. (NO COMPONENT FAILED, ONLY THMay 13, 2005 · N956PC · Pilats PC1245 · Windshield/Door Rain/Ice RemovalSDR 2005FA0001056Antenna · inoperativeFOUND LOWER UAT ANTENNA UNSERVICEABLE DURING UAT UPGRADE. (K)Apr 29, 2005 · N1232Y · Cessna 208B · Central DisplaySDR 2005FA0000654Control Cable · looseDURING SCHEDULED INSPECTION, FOUND CABLE QUADRANT FOR AUTOPILOT RUDDER SERVO LOOSE ON RUDDER TORQUE SHAFT ASSY. REPLACED LOOSE RIVETS W/NEXT SIZE LARGER RIVETS INSTALLED WET W/EA 9309 STRUCTURAL ADHESIVE IAW TECH SUPPORT RECOMMENDATIONS. RECOMMEND THIS AREAApr 23, 2005 · N768WT · Beech B300 · Rudder Control SystemSDR 2005FA0000653Screw · wrong partDURING SCHEDULED INSPECTION FOUND SCREWS ATTACHING AFT LOWER EDGES OF FORWARD WING ROOT FAIRINGS TO UNDERSIDE WING ROOT FAIRINGS TO BE OF EXCESSIVE LENGTH. SCREW TIPS HAD GOUGED LT AND RT LOWER FUSELAGE SKINS AT THE APPROXIMATE FS 166.300 LOCATION TO 0.020 INApr 22, 2005 · N768WT · Beech B300 · FastenersSDR TIM2005F00005Fire Detector · contaminatedFIRE DETECTOR GAVE A FALSE FIRE WARNING IN FLIGHT. MOISTURE WAS PROBABLE CAUSE. AFTER TAXI, THE FIRE WARNING LIGHT EXTINGUISHES. NO OTHER PROBLEMS WITH THE SYSTEM. (K)Apr 19, 2005 · N14MV · Beech 99 · Fire DetectionSDR CA050419001Hydromech Unit · inoperative(CAN) DURING CRUISE THE ENGINE EXPERIENCED AN UNCOMMANDED POWER REDUCTION. THE CREW SHUT THE ENGINE DOWN IN FLIGHT. THE HYDROMECHANICAL FUEL CONTROL UNIT WAS SUBSEQUENTLY REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.Apr 4, 2005 · Beech 300BEECH · Fuel Controlling SystemSDR 2005FA0000572Downlock Switch · intermittentDURING NORMAL GEAR EXTENSION, NO NOSE GEAR DOWN LOCK LIGHT INDICATION. CYCLED GEAR SEVERAL TIMES WITH NO CHANGE. MANUALLY EXTENDED GEAR AND OBTAINED GREEN INDICATION. MAINTENANCE FOUND SWITCH INTERMITTENT. (K)Mar 31, 2005 · N911CX · Beech C90 · Landing Gear Position and WarningSDR CA050407009Bearing · failed(CAN) GENERATOR FAIL LIGHT CAME ON IN FLIGHT. MAINTENANCE FOUND THAT THE FRONT BALL BEARING HAD FAILED.Mar 31, 2005 · Beech B300B350C · Starter-GeneratorSDR 2005FA0000982Windshield · failedPILOTS WERE INCRUISE WITH WINDSHIELD HEAT ON AND WINDSHIELD (INNER) SHATTERED. TALKED TO TECH AND WAS STATED IT WAS USUALLY THE INNER THAT SHATTERS. ALTITUDE 22,000 FT CLEAR, -35 DEGREES C. NO TURBLANCE, NO ICING. (EA17200508780) (K)Mar 22, 2005 · N905GP · Beech 200BEECH · Flight Compartment WindowsSDR RU32005F00000Packing · cutINBOUND TO DESTINATION, NOTICED A THIN STREAM OF CLEAR LIQUID COMING FROM THE TOP VENTS OF THE LT ENGINE. THE CREW DECIDED TO RETURN TO HOME STATION TO HAVE FLUID AND POSSIBLE LEAK REPAIRED. REPLACED DEFECTIVE FUEL FILTER O-RING ON LT ENGINE. (K)Mar 18, 2005 · N70 · Beech 300BEECH · Engine Fuel DistributionSDR CA050315010Arm · mismanufactured(CAN) DURING AN INSPECTION OF THE RUDDER SYSTEM ON A 4TH PHASE 800 HOUR INSPECTION THE BLIND RIVETS WHICH ATTACH THE CONTROL ARM QUADRANT P/N 101-524038-1, TO THE RUDDER TORQUE SHAFT P/N 101-524012-11, WERE FOUND TO BE LOOSE. THE COMPLETE ASSEMBLY WAS REMOVED Mar 11, 2005 · Beech B300B350C · Rudder Control SystemSDR CA050315001Bearing · disintegrated(CAN) DURING 800 HR INSP OF AC, TAIL SEC WAS BEING INSPECTED IAW CHECK SHEETS. LIGHT RUB AND WEAR WAS NOTICED ON RUDDER HINGE POINTS STRUCTURE. IT WAS ALSO, THAT RUDDER APPEARED TO BE SITTING LOWER THAN NML ON ITS HINGE POINTS. INSP OF RUDDER AND ITS STRUCTUMar 11, 2005 · Beech B300B350C · Rudder StructureSDR 2005FA0000343Solenoid Valve · failedINSTALLED A NEW C&D AIRCRAFT HEATER AS A REPLACEMENT TO THE OLD HEATER UNIT. THE NEW HEATER WOULD RUN APPROX 5 MINUTES AND THEN PRODUCE NO HEAT. TROUBLESHOOTING SHOWED THAT FUEL WAS REACHING TO THE NOZZLE SOLENOID VALVE, BUT NOT PAST. VOLTAGE WAS PRESENT, Mar 3, 2005 · N220FS · Piper PA31T · Heating SystemSDR 2005FA0000257Windshield · brokenPILOT REPORTS THAT AT CRUISE ALTITUDE 24,000 FT, EVERYTHING NORMAL THE PILOTS WINDSHIELD OUTER GLASS SHATTERED. TO PREVENT RECURRENCE, REPLACED WITH KIT-STRESS FREE WINDOW INSTALLATION IAW INSTRUCTIONS PROVIDED. (K)Feb 17, 2005 · N345WK · Beech B200 · Flight Compartment WindowsSDR CA050222007Engine · damaged(CAN) AS A RESULT OF PROP STRIKE ENG SUFFERED SOME TIP RUBS IN COMPRESSOR, PT & SCORING DAMAGE IN A PROPSHAFT BOLT HOLE. FULL O/H LEVEL INSP OF RGB COMPONENTS FOUND ONLY NORMAL OPS DAMAGE WITH NO ADDITIONAL DAMAGES. ENG FOUND TO HAVE 14 OF 47 1ST STAGE PT BLADFeb 15, 2005 · Engine (Turbine/Turboprop)SDR 2005FA0000196Clevis Pin · brokenPILOT REPORTED SOUND (LIKE A TIRE BLOWING OUT) UPON LANDING. THERE WAS SEVERE VIBRATION ON ROLLOUT. THERE WAS NO VIBRATION ON TAXI BACK TO HANGAR. UPON EXITING AIRCRAFT, PILOT NOTICED RT MAIN GEAR MISALIGNED. FURTHER INSP BY MAINTENANCE, FOUND RETAINING CLFeb 10, 2005 · N6571S · Beech E90 · Main Landing Gear Attach SectionSDR CA050210005Bleed Valve · inoperative(CAN) WHILE CLIMBING OUT AFTER TAKEOFF THE FLIGHT CREW NOTICED A THROTTLE SPLIT TO MAINTAIN THE SAME ENGINE TORQUE. AT ALL TIMES THE ENGINES WOULD MAKE RATED POWER, BUT THE LT ENGINE REQUIRED MORE FORWARD THROTTLE MOVEMENT TO MAKE BOOK TORQUE. MAINTENANCE PERFFeb 7, 2005 · Beech B300B350C · Compressor Bleed ValveSDR CA050208001Engine · failed(CAN) ENG SUFFERED ONLY MINOR DAMAGE FROM PROP STRIKE WHICH WERE TIP RUBS IN COMPRESSOR, PWR TURBINE COMPONENTS. TIP RUBS FOUND ON PT BLADE PATHS ARE CONSIDERED TO BE MINOR AND NOT UNCOMMON TO FIND AT ANY DISASSEMBLY EVEN AFTER ONLY 77 HOURS OPERATION SINCE THJan 31, 2005 · Engine (Turbine/Turboprop)SDR 2005FA0000213Skin · mismanufacturedUPON REMOVAL OF AC TOP SKIN, FOUND 4 RIVETS ON STRINGER NR 4R JUST FWD OF THE EMERGENCY EXIT HATCH TO HAVE NO EDGE DISTANCE. ABOVE THIS AREA AT FS165.25 AND STRINGER NR 2R THERE WAS FOUND ONE FASTENER HOLE WITH SHORT EDGE DISTANCE. FWD OF THIS AREA AT FS 148Jan 21, 2005 · N905GP · Beech 200BEECH · Fuselage Main, Plate/SkinSDR CA050120011Wire Harness · burnedACFT POWERED UP FOR DAILY INSPECT IN HANGER. CABIN INDIRECT LIGHTING TURNED ON, SOON AFTER, SMOKE NOTED COMING FROM AFT HEADLINER ASSY, OUT OF CABIN DOOR. HEADLINER REMOVED & CONNECTER W2J4 WAS BURNED, & WIRING DAMAGED. IT SHOULD BE NOTED THAT WIRING IN CLOJan 18, 2005 · Beech B300B350C · Light System WiringSDR 2004FA0000941Stringer · crackedSTRINGER NR 9 ON THE RT SIDE WAS FOUND CRACKED DURING NON-RELATED MAINTENANCE.Dec 21, 2004 · N200EW · Beech B200 · Fuselage Main, Longeron/StringerSDR RU3A0421Cooling Fan · burnedWHILE SETTING UP FOR FLIGHT INSPECTION MANEUVER, GOT A RED MASTER CAUTION LIGHT WITH AN AP TRIM DISC LIGHT. TEMPORARILY LOST TCAS, PILOTS FLIGHT DIRECTOR, AND THE PILOTS NCU. AT THE SAME TIME HEARD ELECTRICAL SHORTING SOUND. STRONG ELECTRICAL FUMES WERE DETDec 8, 2004 · N76 · Beech 300BEECH · Inertial Guidance SystemSDR 2005FA0000708Pressure Switch · brokenHEATER SHOWED SIGNS OF ABNORMAL COMBUSTION IE. SOOT TRAIL FROM FUEL DRAIN VENT. UPON INVESTIGATION. FOUND COMBUSTION AIR BLOWER FAN WHEEL ASSY HAD COME APART AND FODED HEATER. FAN MOTOR WOULD STILL RUN. AIR PRESSURE SWITCH HAD FAILED IN CLOSED POSITION IAWDec 8, 2004 · N250CT · Piper PA31T1 · Heating SystemSDR 2005FA0000709Blower · brokenHEATER SHOWED SIGNS OF ABNORMAL COMBUSTION IE. SOOT TRAIL FROM FUEL DRAIN VENT. UPON INVESTIGATION, FOUND COMBUSTION AIR BLOWER FAN WHEEL ASSY HAD COME APART AND FOD`D HEATER. FAN MOTOR WOULD STILL RUN AIR PRESSURE SWITCH HAD FAILED IN CLOSED POSITION. IAW Dec 8, 2004 · N250CT · Piper PA31T1 · Heating SystemSDR 2005FA0000012Governor · malfunctionedDURING NORMAL GROUND RUN-UP. THE AIRCRAFT PROPELLER AUTO-FEATHER SYSTEM WAS OPERATIONALLY CHECKED. BOTH LT AND TR PROPELLER SWITCHES WERE SELECTED AND BOTH PROPELLERS FEATHERED CORRECTLY. WHEN THE SWITCHES WERE RELEASED THE LT PROPELLER DID NOT COME OUT OF Dec 6, 2004 · N981LL · Beech B300 · Propeller Controlling SystemSDR POSA1204041Indicator · false indicationON FLIGHT, THE FLIGHT CREW TOOK OFF, RETRACTED LANDING GEAR AND NOTICED GEAR HANDLE STAYED RED INDICATING. LANDING GEAR WAS NOT FULLY UP AND STOWED. FLIGHT CREW LOWERED LANDING GEAR AND LANDED WITHOUT INCIDENT. ONLY FLIGHT CREW WAS ON BOARD. THERE WAS NO SDec 4, 2004 · N100KA · Beech 100BEECH · Landing Gear Position and WarningSDR FVY2004F00000Control Cable · failedPILOT REPORTS THAT ELEVATOR CONTROL WAS UNAVAILABLE IN FLIGHT AND UNABLE TO ACHIEVE NOSE DOWN POSITION WITHOUT TRIM. MAINTENANCE INSPECTED ELEVATOR CABLES. REMOVED AND REPLACED ELEVATOR DOWN CABLE FROM TORQUE TUBE TO AFT. BAGGAGE COMPONENT TENSION AND RIGGENov 29, 2004 · N142PA · Gulstm G73 · Elevator Control SystemSDR 2005FA0000242Windshield · brokenINNER PLY OF WINDSHIELD SHATTERED AT 29,000, -38 DEGREES C., RT HAND POSITION. THEN 8-10 SECONDS LATER LT WINDSHIELD SHATTERED. RECOMMEND SUBSEQUENT SCHEDULED WINDSHIELD RETORQUES BEING CAREFULLY PERFORMED TO ENSURE ORIGINAL CONTOUR OF WS INSTALLATION IAW KINov 15, 2004 · N20NK · Beech 300BEECH · Flight Compartment WindowsSDR 2005FA0000698Key · missingTHE RT WING RETRACTABLE LANDING LIGHT WAS FAILED, REMOVED, SENT OUT FOR O/H. RETURNED FROM O/H, INSTALLED 8/6/04 AND OPS CHECKED OK. UNIT FAILED 11/1/04 AND WAS REMOVED. UNITS MOTOR WORM GEAR WAS ACCESSED, REMOVED AND THE MECHANIC DETECTED NO WOODRUFF KEY WNov 1, 2004 · N10RM · Cessna 425 · Exterior LightingSDR 2005FA0000699Worm Gear · missingTHE RT WING RETRACTABLE LANDING LIGHT WAS FOAIED, REMOVED, SENT OUT FOR O/H. RETURNE FROM O/H, INSTALLED 8/6/04 AND OPS CHECKED OK. UNIT FAILED 11/1/04 AND WAS REMOVED. UNITS MOTOR WORM GEAR WAS ACCESSED, REMOVED AND THE MECHANIC DETECTED NO WOODRUFF KEY WNov 1, 2004 · N10RM · Cessna 425 · Exterior LightingSDR ACE103004Actuator · erraticPILOT REPORTED, AFTER 3 GEAR EXTENSION CYCLES AND THE QRH MANUAL EXTENSION PROCEDURE, NOSE GEAR GREEN LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE COULD NOT DUPLICATE (SUSPECT INTERMITTENT SWITCHES) AND REPLACED NOSE GEAR ACTUATOR.Oct 30, 2004 · N114AX · Beech 1900C · Landing Gear ActuatorSDR CA040916011Channel · cracked(CAN) THE CREW REPORTED THAT THE CABIN DOOR APPEARED TO BE LEAKING AROUND ITS LOWER AFT CORNER. MAINTENANCE DISCOVERED A 1-INCH CRACK IN THE CABIN DOOR SKIN AT THE LOWER AFT CORNER. THE CRACK RUNS THROUGH THE AFT-MOST HINGE ATTACHMENT RIVET. WHEN THE DOOR WSep 14, 2004 · Beech B300B350C · Fuselage, Door HingeSDR ACE08282004Stringer Clip · missingDURING SCHEDULED STRUCTURAL INSPECTION OF THE AREA, FOUND STRINGER CLIP PN. 114-430066-5 NEVER INSTALLED AND THE BULKHEAD AT FS 363.25 HAD CRACKS IN THE FLANGE ABOVE AND BELOW THE MISSING CLIP LOCATION.Aug 28, 2004 · N113AX · Beech 1900C · Fuselage Main, Attach FittingsSDR ACE082304Limit Switch · out of adjustPILOT REPORTED LANDING GEAR HANDLE WARNING LIGHTS REMAINED ON AFTER GEAR WAS RETRACTED. CREW RETURNED TO AIRPORT FOR AN UNEVENTFUL LANDING. MAINTENANCE ADJUSTED THE NOSE LANDING GEAR UP LIMIT SWITCH FOR PROPER OPERATION.Aug 23, 2004 · N113AX · Beech 1900C · Landing Gear Position and WarningSDR CA040809006Hinge · cracked(CAN) INSPECTION OF THE CABIN DOOR HINGE REVEALED CRACKING OF THE DOOR HALF AFT TWO SECTIONS. FUSELAGE HINGE HALF UNDAMAGED. DOOR HINGE HALF AND PIN TO BE REPLACED NEW.Aug 9, 2004 · Beech B300B350C · Passenger/Crew DoorsSDR CA040805017Cross Tie · cracked(CAN) UPON REMOVING THE LT EMERGENCY EXIT FOR UNRELATED ROUTINE MAINTENANCE, PERSONNEL DISCOVERED A CRACK IN THE LT FUSELAGE CROSSTIE AT STATION 201.775. THE CRACK LOCATION IS NEAR THE LOWER AFT CORNER OF THE LT EMERGENCY EXIT HATCH. CRACK IS APPROX .375 INCAug 5, 2004 · Beech B300B350C · Fuselage Miscellaneous StructureSDR CA040806003Windshield · broken(CAN) AT CRUISE ALTITUDE THE LT WINDSHIELD SHATTERED. FLIGHT CREW DESCENT TO 16000 FEET ALTITUDE AND LANDED AT SAFELY. WINDSHIELD ASSY WILL BE REPLACED.Aug 5, 2004 · Beech B300B350C · Flight Compartment WindowsSDR CA040723001Bearing · failed(CAN) WITH AIRCRAFT IN CRUISE FLIGHT A (LT GEN TIE OPEN) ANNUNCIATOR LIGHT CAME ON. GENERATOR TIE RESET AS IAW CHECK LIST. SHORTLY THEREAFTER THE (LT GEN TIE OPEN) CAME ON FOLLOWED BY THE (LT GEN FAIL) LIGHT ANNUNCIATOR. AIRCRAFT SECURED IAW CHECK LIST AND Jul 22, 2004 · Beech B300B350C · Starter-GeneratorSDR EHA2004F00004Selector Valve · inoperativeLT MAIN GEAR FAILED TO RETRACT. FOUND NITROGEN EXTENSION VALVE OPEN. CLOSED NITROGEN EXTENSION VALVE. SERVICED SYSTEM PROCEDURE FOR (AFTER EMER EXTENSION). SYSTEM OPS CHECK NORMAL. REF MM8101Jul 14, 2004 · N514RD · Beech 200BEECH · Landing Gear Retraction/Extension SystemSDR 2004FA0000524Torque Tube · looseDURING AN INSPECTION, THE LT ELEVATOR CORNTOL TORQUE TUBE THAT ATTACHES TO IB END RIB OF THE LT ELEVATOR WAS FOUND TO HAVE PLAY BETWEEN THE ACTUATING HORN AND THE TORQUE TUBE ITSELF. THE COLLAR WITH THE FLANGE AND THE 4 MOUNTING BOLTS ATTACHING THE TORQUE TUBJul 1, 2004 · N7232R · Beech B200C · Elevator Control SystemSDR RU32004F00000Engine · bird ingestionWHILE CONDUCTING CLEARANCE BELOW PATH RUN, A PAIR OF PIGEONS DIVED AND STRUCK LEFT ENGINE AREA. HEARD A THUMP AND ALL CREW MEMBERS STARTED NOTICING A BURNING SMELL. NO ABNORMAL ENGINE INDICATIONS WERE OBSERVED. CREW REQUESTED IMMEDIATE LANDING AND WAS GIVENJun 25, 2004 · N66 · Beech 300BEECH · Engine (Turbine/Turboprop)SDR LX52004F00001Pressure Switch · leakingDURING A SCHEDULED FLIGHT, THE PILOT NOTICED THE LOW HYDRAULIC FLUID LIGHT HAD COME ON. UPON APPROACH, THE GEAR WAS SELECTED DOWN AND THE POWER PACK RAN FOR 14 SECONDS THEN TRIPPED THE BREAKER. THE GEAR WAS THEN MANUALLY PUMPED DOWN AND PLANE LANDED WITHOUT Jun 21, 2004 · N961LL · Beech 300BEECH · Hydraulic System, MainSDR CA040609009Connector · corroded(CAN) LT WING AUX FUEL TANK INDICATION ALWAYS INDICATING (0). WHEN TESTING SYSTEM LT QUANTITY CAUTION LIGHT WON'T COME ON. DURING TROUBLESHOOTING, FOUND A LOT WATER TRAPPED UNDER THE ACCESS PANEL AND THE WIRING WAS CORRODED. WATER REMOVED AND CONNECTOR WILLJun 9, 2004 · Beech B300B350C · Electrical ConnectorsSDR BAQR361CWheel · damagedWHEEL HAD 64.9 HOURS, 106 LANDINGS SINCE OVERHAULED.Jun 2, 2004 · N777GS · Beech A100 · Wheel/Ski/FloatSDR 2004FA0000523Torque Tube · looseDURING PHASE INSPECTION, THE RT ELEVATOR CONTROL TORQUE TUBE THAT ATTACHES TO THE IB END RIB OF THE RT ELEVATOR WAS FOUND TO HAVE PLAY BETWEEN THE COLLAR WITH THE FLANGE THAT BOLTS TO THE END RIB AND THE TORQUE TUBE ITSELF. THE 4 MOUNTING BOLTS WERE TIGHT TO Jun 1, 2004 · N7232R · Beech B200C · Elevator StructureSDR ACO2004F00000Screen · making metalENGINE LOW OIL PRESSURE LIGHT ILLUMINATED ON FINAL. ENGINE WAS CHECKED AND FILTER HAD METAL IN IT. UPON FURTHER INSPECTION, BYPASS FILTER SCREEN APPEARED DAMAGED. AFTER CLOSURE INSPECTION, BYPASS FILTER SCREEN SEAM DETACHED. THIS WOULD ALLOW OIL TO FLOW UNMay 27, 2004 · N540CB · Beech 300BEECH · Turbine Engine Oil SystemSDR CA040519010O-Ring · pinched(CAN) RT ENGINE SHUTDOWN DUE TO OIL PRESSURE, LIGHT ON AND OIL PRESSURE BETWEEN 60 AND 60 PSI. AFTER INVESTIGATION FOUND ONE O-RING LEAKING ON RT ENGINE REDUCTION GEARBOX OIL TRANSFER TUBE, REPLACED O-RING P/N AS3209-114. AFTER DISCUSSION WITH PILOTS, DID NOT May 13, 2004 · Beech B300B350C · Turbine Engine Oil System
Back to U/A Canada PT6A-60A