Pratt & Whitney JT15D-5

Service difficulty reports · 953

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 = 'JT15D5'
  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 2026FA0000640Engine · bird ingestionMASTER WARNING FOLLOWED BY LOSS OF OIL PRESSURE. ENGINE SHUT DOWN AND RETURNED TO KCCO. DISCOVERED BIRD STRIKE AND BENT FAN BLADES AFTER LANDINGAug 14, 2026 · N577X · Cessna 551 · Engine (Turbine/Turboprop)SDR 3N0A2025121800284Windshield · delaminatedTHE RIGHT WINDSHIELD SHOWED SIGNS OF DELAMINATION SHORTLY AFTER DEPARTING PWN. AFTER LANDING AT BNA A PICTURE WAS SENT TO DIR. OF MAINTENANCE AND TRIP SUPPORT, AND WE WERE ADVISED TO CONTINUE THE FLIGHT BACK TO BASE, AT FL 360 WE HEARD A LOUD CRACKING NOISE, Dec 13, 2025 · N661WD · Beech 400A · Flight Compartment WindowsSDR 2024FA0000040Duct · crackedPILOT REPORTED GETTING THE "BL AIR DCT FAIL" LIGHT IN FLIGHT, DURING CRUISE OPERATION. DURING TROUBLESHOOTING, IT WAS NOTED THAT THE BLEED AIR TUBE THAT CONNECTED TO THE LEFT ENGINE WAS CRACKED ALL THE WAY AROUND IN THE PYLON AREA.Jan 16, 2024 · N880MG · Beech 400A · Engine Bleed Air SystemSDR 2023F00225Turbine · out of positionRH AVIATION, LLC SENT ENGINE SERIAL NUMBER 108361 TO STANDARDAERO FOR INVESTIGATION AND REPAIR AFTER THE OPERATOR FOUND METAL DEBRIS IN THE EXHAUST OF THE ENGINE. FURTHER INVESTIGATION IN THE FIELD FOUND THAT THE LP TURBINE HAD MOVED AND MADE CONTACT WITH THE Mar 25, 2023 · N60QB · Engine (Turbine/Turboprop)SDR R3WA202108130001Engine · flamed outAT 43000 AIRCRAFT WAS CROSSING A SMALL LINE OF WEATHER. ENCOUNTERED SOME MODERATE TURBULENCE. RIGHT ENGINE SHUT OFF. CREW DECLARED AN EMERGENCY AND STARTED A DESCENT. CREW REPORTED RIGHT ENGINE LOOKED TO BE IN GOOD SHAPE STILL SHOWING ABOUT 8.7% AND TWO. CREW Aug 11, 2021 · N63FF · Gulstm 560 · Engine (Turbine/Turboprop)SDR YQSA2021062803Engine · leakingCREW TOOK OFF FROM KSDL ON 6/26. ON CLIMB OUT, THEY FELT A COUPLE OF THUMPS, LEFT ENGINE OIL TEMP INCREASED. CREW PULLED POWER BACK AND TURNED BACK. LEFT ENGINE OIL PRESSURE DROPPED BELOW THE GREEN AND OIL TEMP HIT REDLINE, SO CREW SHUT DOWN LEFT ENGINE, DECLAJun 26, 2021 · N811SH · Cessna 560XL · Turbine Engine Oil SystemSDR 2021FA0000289Igniter · crackedREMOVED IGNITER FOR INSPECTION, FOUND A CRACK 180 DEGREES AROUND THE BASE OF THE IGNITER ABOVE THE THREADS AND BELOW THE HEX AREA.Mar 25, 2021 · N116AD · Beech 400A · Spark Plug/IgniterSDR 9JLA2021021227023Anti-Ice Valve · defectiveTHE FLIGHT CREW REPORTED A RIGHT ENGINE TEMP LOW ANNUNCIATOR WHILE IN FLIGHT AND REMAINED ILLUMINATED WITH N2 AT 82%. THEY INDICATED THE ITT DID SHOW A RISE DURING SWITCH OPERATION. THE MAINTENANCE TEAM TROUBLESHOT AND DETERMINED THE ENGINE ANTI-ICE VALVE WAS Feb 6, 2021 · N61GB · Beech 400A · Engine Anti-Icing SystemSDR DBCA202102040001Anti-Ice Valve · failedAFTER TAKE-OFF CREW NOTED RT ENGINE ANTI-ICE FAIL INDICATION. CREW RETURNED TO HOME BASE. MX TROUBLESHOT. REPLACED RT ENGINE INLET ANTI-ICE SOLENOID VALVE WITH REPAIRED UNIT. OPS CHECKED GOODFeb 4, 2021 · N265CM · Cessna 560CESSNA · Engine Anti-Icing SystemSDR 9JLA2020120824759Engine · inoperativeA FLIGHT WAS CANCELLED DUE TO THE CREW NOT BEING ABLE TO START THE NR 1 ENGINE. THE MAINTENANCE TEAM TROUBLESHOT, BUT WAS UNABLE TO DUPLICATE THE DISCREPANCY. AS A PRECAUTIONARY MEASURE THE STARTER DISENGAGE SWITCH WAS CLEANED. OPERATIONAL CHECKS WERE SATISNov 18, 2020 · N1JP · Beech 400A · Engine (Turbine/Turboprop)SDR T17A20200811041Angle · crackedRIGHT TR FAN DUCT ANGLE CRACKED. REMOVED AND REPLACED TR FAN DUCT ANGLE, IAW HAWKER 400XP CMM 78-30-07.Sep 23, 2020 · N487TM · Beech 400A · Engine Thrust ReverserSDR T17A20200811031Inlet · crackedDURING SCHEDULED MX FOUND RT ENGINE INLET AT 9 O'CLOCK POSITON CRACKED. INSTALLED SERVICABLE R/H ENGINE INLET DUCTLAug 11, 2020 · N453TM · Raythn 400ARAYTHEON · Turbine Engine Air Inlet SectionSDR 2HGR2020012301Controller · intermittentCREW WAS RE-POSITIONING N233MW FROM KSBA TO KCRQ. DURING THE TAKE-OFF PHASE, THE CREW NOTICED A FLASHING MASTER CAUTION WARNING AND THE R EFC OFF ANNUNCIATIOR ILLUMINATED. CREW DECIDED TO ABORT THE TAKE-OFF. AFTER EXITING THE RUNWAY, CREW PROCEEDED TO RE-TEST Jan 12, 2020 · N233MW · Beech 400A · Engine Indicating SystemSDR CA190219004Fcu · malfunctioned(CAN) PILOT REPORTED THAT ON DOWNWIND, ENGINE ROLLED BACK FROM IDLE TO 24%. THEN, WHEN PILOT WAS ON FINAL APPROACH, THE ENGINE COMPLETELY CEASED TO PRODUCE POWER.Jan 30, 2019 · Raythn 400ARAYTHEON · Fuel Control/Turbine EnginesSDR 2019F00107Fuel Line · defectiveIN MAINTENANCE DURING ENGINE INSPECTION AND THE FUEL BOOST PUMP ON, A VERY TINY STREAM OF FUEL (ABOUT THE SIZE OF A FINE HAIR) WAS FOUND SPRAYING FROM THIS LINE ONTO THE SIDE OF THE ENGINE DRIVEN FUEL PUMP. WITH THE ENGINE RUNNING THE LEAK IS VIRTUALLY UNNOTICJan 4, 2019 · N498TM · Engine Fuel DistributionSDR ESMR201707130001Oil Cap · crackedDURING THE DEPARTURE, CLIMBING THROUGH FL240, WHEN THE OIL PRESSURE ON THE LEFT ENGINE STARTED DROPPING. THE MASTER WARNING LIGHT AND THE LOW OIL PRESSURE ANNUNCIATION LIGHT ILLUMINATED, CONFIRMING THE OIL PRESSURE GAUGE INDICATION. THE ENGINE WAS SHUTDOWN .Jul 12, 2017 · N500FZ · Cessna 560CESSNA · Turbine Engine Oil SystemSDR T17A201706134022Engine · malfunctionedDURING CRUISE FLIGHT AT 39,000 FT, CREW RECEIVED THE MASTER WARNING ANNUNCIATION, ACCOMPANIED BY A LT FUEL PRESSURE LOW LIGHT WITH IMMEDIATE ROLL BACK OF THE NR 1 ENGINE. RAN THE CHECKLIST FOR ENGINE FAILURE AND DESCENDED. AT 29,000 FT, THE CREW ATTEMPTED A Jun 10, 2017 · N460TM · Raythn 400ARAYTHEON · Engine (Turbine/Turboprop)SDR 2017FA0000194Switch · out of limitsDURING TROUBLESHOOTING OF THE ANTI-ICE SYSTEM, THE ENGINE ANTI-ICE TEMP SWITCH WAS FOUND OUT OF LIMITS ON THE INDICATION. THE SWITCH WAS REPLACED WITH NEW.May 17, 2017 · N6NY · Cessna 560CESSNA · Engine Anti-Icing SystemSDR CVGA20170406001Engine · shutdownNORMAL CLIMB THROUGH 10,000 FEET. ONCE WE PAST 18,000 FEET, THE AIRPLANE YAWED TO THE LEFT, I TOOK CONTROL AND AT THE SAME TIME I LOOKED AT MY ENGINE GAUGED FROM TOP TO BOTTOM, I SAW MY LEFT N1, LEFT ITT, LEFT FUEL FLOW AND LEFT N2 ROLL BACK. MY LEFT OIL PRESSApr 4, 2017 · N127SJ · Raythn 400ARAYTHEON · Engine (Turbine/Turboprop)SDR PAIR20170308S3720Engine · making metalDURING PRE-PURCHASE SURVEY, INSPECTED ENGINE OIL FILTER AND FOUND LARGE AMOUNT OF METAL DEBRIS. ENGINE REMOVED FROM SERVICE AND SENT TO OVERHAUL FACILITY FOR REPAIR OR OVERHAUL.Mar 8, 2017 · N362EA · Beech 400A · Engine (Turbine/Turboprop)SDR T17A201604154013Engine · power lossPILOT REPORTED RT ENG EXPERIENCED SLOW ROLLBACK ON BASE & FINAL APPROACH. THE APPROACH & LANDING WERE UNEVENTFUL. AFTER LANDING THE ENG WAS SECURED. PERFORMED NORMAL PERFORMANCE CHECK IAW AMM 71-00-00. UPON COMPLETING SEVERAL PERFORMANCE CHECKS NO ISSUES FApr 12, 2016 · N475TM · Raythn 400ARAYTHEON · Engine (Turbine/Turboprop)SDR T17A201603224011Fastener · shearedA LOCK FASTENER WAS NOTED MISSING FROM THE RT ENG INLET. UPON FURTHER INSPECTION, ENG FAN BLADE DAMAGED & COMPRESSOR VANE DAMAGE WAS FOUND. ENG IS BEING REMOVED FOR REPAIR.Mar 17, 2016 · N435CT · Raythn 400ARAYTHEON · Engine Air Intake SystemSDR 2016FA0000136Starter Gen · failedRIGHT STARTER GENERATOR FAILED IN FLIGHT, ACFT RETURNED TO BASE REMOVED RT STARTER GENERATOR AND FOUND THE FORWARD BEARING NEXT TO THE COOLING FAN FAILED.Mar 15, 2016 · N371CF · Beech 400A · Starter-GeneratorSDR CA160302004Hmu · malfunctioned(CAN) CUSTOMER REPORTED NR 1 ENGINE BARELY MAKES TAKE OFF OF THE DAY AND THEN ROLLS BACK ONE PERCENT. THE ENGINE HAS JUST RECEIVED FROM AN HOT SECTION INSPECTION AND HMU REPLACEMENT. DURING TROUBLESHOOTING THE ISSUE WAS DUPLICATE. THE HMU HAS BEEN SWAPPED AND Feb 23, 2016 · Raythn 400ARAYTHEON · Fuel Control/Turbine EnginesSDR CA160205002Ground Stud · corroded(CAN) DURING A POST FLIGHT INSPECTION OF THE ACFT IT WAS OBSERVED THAT THE SIDE OF THE FUSELAGE, ADJACENT THE EXTERNAL POWER PLUG WAS WARN TO TOUCH. INVESTIGATION OF THE AREA REVEALED THAT THE GROUND CABLE OF THE EXTERNAL POWER PLUG WAS NOT CORRECTLY INSTALLEFeb 2, 2016 · Cessna 560CESSNA · External Power SystemSDR CA151229002Oil Filter · bypassing(CAN) WHILE GETTING READY FOR TAKEOFF, THE CREW REPORTED THAT THE OIL FILTER BYPASS INDICATION CAME ON MOMENTARILY AND WENT OUT WITH A CORRESPONDING SPIKE IN OIL PRESSURE INTO THE RED. WHEN THEY BROUGHT THE THROTTLE BACK, THE OIL PRESSURE RETURNED TO THE GREEDec 20, 2015 · Raythn 400ARAYTHEON · Turbine Engine Oil SystemSDR CA151201007Engine · shutdown(CAN) FLYING LEVEL AT FL 360, PILOT NOTICED A VIBRATION ON THE ACFT, FOLLOWED BY THE MESSAGE RT GENERATOR OFF, GENERATOR RESET PERFORMED AND THE SYS WORKED FOR 3 MINUTES. VIBRATION WAS STILL PRESENT. AFTER 3 MINUTES, THE WARNING FOR RT GENERATOR OFF ACTIVATENov 25, 2015 · Raythn 400ARAYTHEON · Engine (Turbine/Turboprop)SDR CA151130007Flow Divider · defective(CAN) THE ENGINE HAD AN UNCOMMANDED FLAMEOUT ON APPROACH AT AROUND 2000 FT. ACFT LANDED UNEVENTFULLY. AFTER TROUBLESHOOTING, IT WAS DECIDED TO REPLACE THE FUEL FLOW DIVIDER.Nov 14, 2015 · Cessna 560CESSNA · Fuel DividerSDR CA151029011Engine · shutdown(CAN) DURING DESCENT THROUGH APPROXIMATELY 2500, THE ENGINE SHUT ITSELF DOWN FROM A SETTING OF 5-10 PERCENT ABOVE FLIGHT IDLE. THE WARNING INDICATIONS CAME ON WITH LOSS OF OIL PRESSURE, FUEL FLOW, N2 ETC. THERE WERE NO PROBLEMS SEEN DURING THE PREVIOUS 4.5 HROct 15, 2015 · Cessna 560XL · Engine (Turbine/Turboprop)SDR CA151029012Unknown · smoke(CAN) THE CREW REPORTED SMOKE IN THE COCKPIT DURING TAKEOFF. THEY ELECTED TO RETURN TO THE POINT OF DEPARTURE WHERE A SAFE LANDING WAS MADE. POST FLIGHT ENGINE RUNS REVEALED SMOKE COMING FROM THE AIR CONDITIONING DUCTS BEHIND THE CREW SEATS. TROUBLESHOOTING IOct 13, 2015 · Air Distribution SystemSDR CA150817005Engine · flamed out(CAN) AT FLIGHT LEVEL 45000 FEET, BOTH LEFT AND RIGHT HAND ENGINE FLAMEOUT THE MOMENT PILOT REDUCED POWER TO BEGIN DESCENT. PILOT HAD UNSUCCESSFUL ATTEMPTS OF RE-STARTING BOTH ENGINES. PILOT UNEVENTFULLY LANDED AIRCRAFT, GLIDING, WITHOUT ENGINES` ASSISTANCE. NAug 4, 2015 · Raythn 400ARAYTHEON · Engine (Turbine/Turboprop)SDR CA150727009Engine · malfunctioned(CAN) THE PILOT REPORTED THAT DURING FLIGHT AT CRUISE, THE LT ENGINE POWER INCREASES BY ITSELF. THE PILOT MUST REDUCE THE POWER WITH THE THROTTLE TO MATCH THE RT ENGINE. THEN AFTER SEVERAL MINUTES THE POWER DECREASES BY ITSELF AND THE PILOT MUST BRING THE LTJul 15, 2015 · Raythn 400ARAYTHEON · Engine (Turbine/Turboprop)SDR 9JLA201504038653Pressure Switch · defectiveDURING LANDING THE RT THRUST REVERSER ARM LIGHT TESTS, BUT DOES NOT ILLUMINATE WHEN THE THRUST REVERSER SYS WAS ARMED. THRUST REVERSER OPERATION WAS REPORTED TO BE NORMAL. TROUBLESHOOTING FOUND THE RT THRUST REVERSER PRESS SWITCH TO BE DEFECTIVE, PN 6607-7-7Mar 23, 2015 · N602JC · Gulstm 200 · Engine Thrust ReverserSDR VIB42015FA0000091Pcb · deactivatedIGNITER WOULD NOT FUNCTION, NO POWER TO UNIT. NO POWER TO UNIT IN IGNITER ON OR STANDBY POSITION OR DURING START. ENGINE LIP HEAT VALVE NOT POWERED WITH BATTERY ON. POWERS CLOSES VALVE BATTERY ON. OPENS ON ACTIVATION BY REMOVING POWER. DISCOVERED SOMEONE HAMar 17, 2015 · N1116R · Beech 400A · Ignition SystemSDR CA150325011Engine · flamed out(CAN) FOLLOWING THROTTLE REDUCTION TO IDLE DURING DESCENT THE ENGINE FLAMED OUT. THE PILOT WAS ABLE TO RESTART THE ENGINE WHICH FLAMED OUT AGAIN TWICE WHILE BRINGING THROTTLE TO IDLE. ALL EVENTS OCCURRED IN EEC MODE.Mar 10, 2015 · Engine (Turbine/Turboprop)SDR CA150128005Engine · making metal(CAN) THE AIRCRAFT RETURNED FROM A SERIES OF FLIGHTS DEC 18/2014 . THE CREW REPORTED NO DEFECTS. DURING A POST/PRE-FLIGHT OF THE AIRCRAFT MAINTENANCE NOTED METALLIC DEBRIS IN THE TAILPIPE OF THE LT ENGINE. THIS DEBRIS CONSISTED OF SEVERAL SMALL METALLIC PIECESDec 18, 2014 · Cessna 560CESSNA · Turbine SectionSDR CA140908014Engine · power loss(CAN) THE PILOT REPORTED AN UNCOMMANDED POWER ROLLBACK AND IFSD OF NR 2 ENGINE ON APPROACH. UNEVENTFUL SINGLE ENGINE LANDING WAS CARRIED OUT. THE PILOT ATTEMPTED TO RESTART THE ENGINE ON TAXIING IN TO STAND. THE START WAS ABORTED DUE TO NO LIGHT OFF. TROUBLAug 28, 2014 · Cessna 560CESSNA · Engine (Turbine/Turboprop)SDR 2014FA0000611Display · failedON OUR ABOVE DATED FLIGHT, WE DISCOVERED THE LOSS OF 2 DU-870 EFIS DISPLAYS. AT FIRST THE MFD WENT BLANK AND ABOUT 15 MINUTES LATER PFD NR 2 FAILED AND WENT BLANK. ABOUT 45 MINUTES LATER DURING THE FLIGHT PFD NR 2 CAME BACK TO WORK. EVERY TIME WE HAVE FLOWN Aug 26, 2014 · N808AC · Cessna 560CESSNA · Central DisplaySDR R3W2014F00001Coupling · separatedDURING CLIMB TO 38,000 FT TO FLIGHT LEVEL OF 40,000 FT, THE CABIN STARTED TO CLIMB 2000 FT PER MINUTE. CAPTAIN DECLARED AN EMERGENCY AND DESCENDED TO A SAFE OXYGEN LEVEL AND LANDED. TROUBLESHOOTING THE SYS FOUND NUT, PN MS210433 HAD SEPARATED FROM COUPLING, Aug 25, 2014 · N470DP · Cessna 560CESSNA · Humidity Control SystemSDR 9JLA2014081304054Wire Harness · defectiveTHE LT ENG ANTI-ICE ANNUNCIATOR WOULD NOT ILLUMINATE WHEN THE SYS WAS ACTIVATED. EXTENSIVE TROUBLESHOOTING FOUND THE LT ENG WIRING HARNESS PN 3052134-01 SN AA87179 DEFECTIVE. A NEW WIRING HARNESS OF THE SAME PART NUMBER WAS INSTALLED. FUNCTIONAL CHECKS WEREAug 2, 2014 · N426GF · Beech 400A · Engine Bleed Air System WiringSDR R3WA2014082200001Switch · burnedDURING TAXIING FOR TAKEOFF, A STRONG ODOR WAS DETECTED IN COCKPIT. CAPTAIN ELECTED TO RETURN TO THE TERMINAL BEFORE TAKEOFF. THE LANDING GEAR LIGHT SWITCH HAD SHORTED OUT AND THAT WAS THE CAUSE OF THE BURNED ODOR. FLIGHT WAS CANCELLED. THE CIRCUIT BREAKERSJul 26, 2014 · N63FF · Cessna 560CESSNA · Landing Gear Position and WarningSDR CA140602019Engine · malfunctioned(CAN) PILOT ABORTED TAKEOFF DURING TAKEOFF ROLL DUE TO UNCOMMANDED ACCELERATION. PILOT SECURED THE ENGINE AND RETURNED TO RAMP.May 19, 2014 · Raythn 400ARAYTHEON · Engine (Turbine/Turboprop)SDR CA140508003Elbow · failed(CAN) DURING CLIMB OUT ITT ON LT ENGINE APPROACHED UPPER LIMIT. ACFT RETURNED TO BASE. ON APPROACH ENGINE IGNITERS WERE SELECTED BUT LT SIDE DID NOT INDICATE THAT IT WAS FUNCTIONAL. INSPECTION OF LT ENGINE INDICATED FAILED LT ENGINE OTBD BLEED AIR FLEX PIPEMay 5, 2014 · Cessna 560CESSNA · Engine Bleed Air SystemSDR 9JLA2014050604051Wire Harness · intermittentDURING THE CLIMB AFTER TAKEOFF THE CREW REPORTED THAT THE LT EFC FAILED. ONCE THE ACFT WAS IN CRUISE FLIGHT THE EFC WAS RESET & NO FAULTS WERE NOTED UNTIL THE DESCENT FOR LANDING WHERE THE EFC FAILED ONCE MORE. TROUBLESHOOTING FOUND THAT THE LT ENG PROBE HARMay 2, 2014 · N426GF · Beech 400A · Engine Fuel System WiringSDR CA140401006Warning Light · illuminated(CAN) DURING TAKEOFF ROLL, AN EEC INDICATION LIGHT OCCURRED FOLLOWED BY A N1 ROLLBACK. THE PILOTS SECURED THE ENGINE, AND TAXIED BACK TO HANGAR. EEC TROUBLESHOOTING ON-GOING.Mar 27, 2014 · Raythn 400ARAYTHEON · Fuel Controlling SystemSDR CA140326013Oil System · low pressure(CAN) THE PILOT SHUTDOWN THE ENGINE IN CRUISE DUE TO LOW OIL PRESSURE. THE ENGINE WAS SECURED FOLLOWED BY A UNEVENTFUL LANDING. IT WAS REPORTED 3 OIL QUARTZ WERE NECESSARY FOR THE OIL LEVEL TO START TOUCHING THE DEEP STICK. THE ENGINE EXHAUST IS COVERED WITH Mar 17, 2014 · Cessna 560CESSNA · Engine Oil Indicating SystemSDR CA140313008Float Valve · unserviceableDURING SINGLE POINT REFUELING, FUEL LEAKED OUT OF THE LT NACA VENT. FOUND THE LT VENT FLOAT VALVE FAILED CLOSED. THE SCREW ATTACHING THE VALVE FLAP TO THE FLOAT HAD COME LOOSE. SERVICEABLE VENT FLOAT VALVE, PN 9914268-4, SN 397, REMOVED FROM ACFT, INSTALLED Mar 10, 2014 · Cessna 560CESSNA · Fuel StorageSDR CA140313006Engine · smokeACFT WAS ON TAXI PREPARING FOR TAKEOFF WHEN CONTROL TOWER CONTACTED THE PILOT TO ADVISE OF SIGNIFICANT SMOKE FROM LT ENGINE EXHAUST. PILOT SECURED ENGINE AND RETURNED TO FBO.Feb 28, 2014 · Raythn 400ARAYTHEON · Engine (Turbine/Turboprop)SDR CA140224009Engine · power loss(CAN) WHILE TAXIING FOR A REGULAR FLIGHT THE NR 2 ENGINE POWER ROLLED BACK AND IT FLAMED OUT. TROUBLESHOOTING IS ONGOING.Feb 15, 2014 · Raythn 400ARAYTHEON · Engine (Turbine/Turboprop)SDR CA140203006Duct · contaminated(CAN) THE CREW ABORTED A MISSION DUE TO FUMES AND A STRONG OIL ODOR COMING FROM THE BLEED AIR SYSTEM. DECLARED AN IN-FLIGHT EMERGENCY, IFE AND LANDED WITHOUT INCIDENT. THE MAINTENANCE TROUBLESHOOTING COFIRMED THAT THE ODOR WAS COMING FROM THE NR 1 ENGINE. DJan 26, 2014 · Engine (Turbine/Turboprop)
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