# Service difficulty reports: Pratt & Whitney JT15D-5

A list on [Pratt & Whitney JT15D-5](https://openairdocs.org/engine/pratt-whitney-jt15d-5.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 20 · 953 reports

- [SDR 2026FA0000640](https://openairdocs.org/sdr/2026FA0000640.md): Engine · bird ingestion · Aug 14, 2026 · N577X · Cessna 551 · Engine (Turbine/Turboprop)
  > MASTER WARNING FOLLOWED BY LOSS OF OIL PRESSURE. ENGINE SHUT DOWN AND RETURNED TO KCCO. DISCOVERED BIRD STRIKE AND BENT FAN BLADES AFTER LANDING
- [SDR 3N0A2025121800284](https://openairdocs.org/sdr/3N0A2025121800284.md): Windshield · delaminated · Dec 13, 2025 · N661WD · Beech 400A · Flight Compartment Windows
  > THE 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,
- [SDR 2024FA0000040](https://openairdocs.org/sdr/2024FA0000040.md): Duct · cracked · Jan 16, 2024 · N880MG · Beech 400A · Engine Bleed Air System
  > PILOT 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.
- [SDR 2023F00225](https://openairdocs.org/sdr/2023F00225.md): Turbine · out of position · Mar 25, 2023 · N60QB · Engine (Turbine/Turboprop)
  > RH 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
- [SDR R3WA202108130001](https://openairdocs.org/sdr/R3WA202108130001.md): Engine · flamed out · Aug 11, 2021 · N63FF · Gulstm 560 · Engine (Turbine/Turboprop)
  > AT 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
- [SDR YQSA2021062803](https://openairdocs.org/sdr/YQSA2021062803.md): Engine · leaking · Jun 26, 2021 · N811SH · Cessna 560XL · Turbine Engine Oil System
  > CREW 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, DECLA
- [SDR 2021FA0000289](https://openairdocs.org/sdr/2021FA0000289.md): Igniter · cracked · Mar 25, 2021 · N116AD · Beech 400A · Spark Plug/Igniter
  > REMOVED IGNITER FOR INSPECTION, FOUND A CRACK 180 DEGREES AROUND THE BASE OF THE IGNITER ABOVE THE THREADS AND BELOW THE HEX AREA.
- [SDR 9JLA2021021227023](https://openairdocs.org/sdr/9JLA2021021227023.md): Anti-Ice Valve · defective · Feb 6, 2021 · N61GB · Beech 400A · Engine Anti-Icing System
  > THE 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
- [SDR DBCA202102040001](https://openairdocs.org/sdr/DBCA202102040001.md): Anti-Ice Valve · failed · Feb 4, 2021 · N265CM · Cessna 560CESSNA · Engine Anti-Icing System
  > AFTER 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 GOOD
- [SDR 9JLA2020120824759](https://openairdocs.org/sdr/9JLA2020120824759.md): Engine · inoperative · Nov 18, 2020 · N1JP · Beech 400A · Engine (Turbine/Turboprop)
  > A 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 SATIS
- [SDR T17A20200811041](https://openairdocs.org/sdr/T17A20200811041.md): Angle · cracked · Sep 23, 2020 · N487TM · Beech 400A · Engine Thrust Reverser
  > RIGHT TR FAN DUCT ANGLE CRACKED. REMOVED AND REPLACED TR FAN DUCT ANGLE, IAW HAWKER 400XP CMM 78-30-07.
- [SDR T17A20200811031](https://openairdocs.org/sdr/T17A20200811031.md): Inlet · cracked · Aug 11, 2020 · N453TM · Raythn 400ARAYTHEON · Turbine Engine Air Inlet Section
  > DURING SCHEDULED MX FOUND RT ENGINE INLET AT 9 O'CLOCK POSITON CRACKED. INSTALLED SERVICABLE R/H ENGINE INLET DUCTL
- [SDR 2HGR2020012301](https://openairdocs.org/sdr/2HGR2020012301.md): Controller · intermittent · Jan 12, 2020 · N233MW · Beech 400A · Engine Indicating System
  > CREW 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
- [SDR CA190219004](https://openairdocs.org/sdr/CA190219004.md): Fcu · malfunctioned · Jan 30, 2019 · Raythn 400ARAYTHEON · Fuel Control/Turbine Engines
  > (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.
- [SDR 2019F00107](https://openairdocs.org/sdr/2019F00107.md): Fuel Line · defective · Jan 4, 2019 · N498TM · Engine Fuel Distribution
  > IN 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 UNNOTIC
- [SDR ESMR201707130001](https://openairdocs.org/sdr/ESMR201707130001.md): Oil Cap · cracked · Jul 12, 2017 · N500FZ · Cessna 560CESSNA · Turbine Engine Oil System
  > DURING 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.
- [SDR T17A201706134022](https://openairdocs.org/sdr/T17A201706134022.md): Engine · malfunctioned · Jun 10, 2017 · N460TM · Raythn 400ARAYTHEON · Engine (Turbine/Turboprop)
  > DURING 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
- [SDR 2017FA0000194](https://openairdocs.org/sdr/2017FA0000194.md): Switch · out of limits · May 17, 2017 · N6NY · Cessna 560CESSNA · Engine Anti-Icing System
  > DURING 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.
- [SDR CVGA20170406001](https://openairdocs.org/sdr/CVGA20170406001.md): Engine · shutdown · Apr 4, 2017 · N127SJ · Raythn 400ARAYTHEON · Engine (Turbine/Turboprop)
  > NORMAL 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 PRESS
- [SDR PAIR20170308S3720](https://openairdocs.org/sdr/PAIR20170308S3720.md): Engine · making metal · Mar 8, 2017 · N362EA · Beech 400A · Engine (Turbine/Turboprop)
  > DURING 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.
- [SDR T17A201604154013](https://openairdocs.org/sdr/T17A201604154013.md): Engine · power loss · Apr 12, 2016 · N475TM · Raythn 400ARAYTHEON · Engine (Turbine/Turboprop)
  > PILOT 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 F
- [SDR T17A201603224011](https://openairdocs.org/sdr/T17A201603224011.md): Fastener · sheared · Mar 17, 2016 · N435CT · Raythn 400ARAYTHEON · Engine Air Intake System
  > A 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.
- [SDR 2016FA0000136](https://openairdocs.org/sdr/2016FA0000136.md): Starter Gen · failed · Mar 15, 2016 · N371CF · Beech 400A · Starter-Generator
  > RIGHT STARTER GENERATOR FAILED IN FLIGHT, ACFT RETURNED TO BASE REMOVED RT STARTER GENERATOR AND FOUND THE FORWARD BEARING NEXT TO THE COOLING FAN FAILED.
- [SDR CA160302004](https://openairdocs.org/sdr/CA160302004.md): Hmu · malfunctioned · Feb 23, 2016 · Raythn 400ARAYTHEON · Fuel Control/Turbine Engines
  > (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
- [SDR CA160205002](https://openairdocs.org/sdr/CA160205002.md): Ground Stud · corroded · Feb 2, 2016 · Cessna 560CESSNA · External Power System
  > (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 INSTALLE
- [SDR CA151229002](https://openairdocs.org/sdr/CA151229002.md): Oil Filter · bypassing · Dec 20, 2015 · Raythn 400ARAYTHEON · Turbine Engine Oil System
  > (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 GREE
- [SDR CA151201007](https://openairdocs.org/sdr/CA151201007.md): Engine · shutdown · Nov 25, 2015 · Raythn 400ARAYTHEON · Engine (Turbine/Turboprop)
  > (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 ACTIVATE
- [SDR CA151130007](https://openairdocs.org/sdr/CA151130007.md): Flow Divider · defective · Nov 14, 2015 · Cessna 560CESSNA · Fuel Divider
  > (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.
- [SDR CA151029011](https://openairdocs.org/sdr/CA151029011.md): Engine · shutdown · Oct 15, 2015 · Cessna 560XL · Engine (Turbine/Turboprop)
  > (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 HR
- [SDR CA151029012](https://openairdocs.org/sdr/CA151029012.md): Unknown · smoke · Oct 13, 2015 · Air Distribution System
  > (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 I
- [SDR CA150817005](https://openairdocs.org/sdr/CA150817005.md): Engine · flamed out · Aug 4, 2015 · Raythn 400ARAYTHEON · Engine (Turbine/Turboprop)
  > (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. N
- [SDR CA150727009](https://openairdocs.org/sdr/CA150727009.md): Engine · malfunctioned · Jul 15, 2015 · Raythn 400ARAYTHEON · Engine (Turbine/Turboprop)
  > (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 LT
- [SDR 9JLA201504038653](https://openairdocs.org/sdr/9JLA201504038653.md): Pressure Switch · defective · Mar 23, 2015 · N602JC · Gulstm 200 · Engine Thrust Reverser
  > DURING 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 6607-7-7
- [SDR VIB42015FA0000091](https://openairdocs.org/sdr/VIB42015FA0000091.md): Pcb · deactivated · Mar 17, 2015 · N1116R · Beech 400A · Ignition System
  > IGNITER 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 HA
- [SDR CA150325011](https://openairdocs.org/sdr/CA150325011.md): Engine · flamed out · Mar 10, 2015 · Engine (Turbine/Turboprop)
  > (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.
- [SDR CA150128005](https://openairdocs.org/sdr/CA150128005.md): Engine · making metal · Dec 18, 2014 · Cessna 560CESSNA · Turbine Section
  > (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 PIECES
- [SDR CA140908014](https://openairdocs.org/sdr/CA140908014.md): Engine · power loss · Aug 28, 2014 · Cessna 560CESSNA · Engine (Turbine/Turboprop)
  > (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. TROUBL
- [SDR 2014FA0000611](https://openairdocs.org/sdr/2014FA0000611.md): Display · failed · Aug 26, 2014 · N808AC · Cessna 560CESSNA · Central Display
  > ON 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
- [SDR R3W2014F00001](https://openairdocs.org/sdr/R3W2014F00001.md): Coupling · separated · Aug 25, 2014 · N470DP · Cessna 560CESSNA · Humidity Control System
  > DURING 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,
- [SDR 9JLA2014081304054](https://openairdocs.org/sdr/9JLA2014081304054.md): Wire Harness · defective · Aug 2, 2014 · N426GF · Beech 400A · Engine Bleed Air System Wiring
  > THE 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 WERE
- [SDR R3WA2014082200001](https://openairdocs.org/sdr/R3WA2014082200001.md): Switch · burned · Jul 26, 2014 · N63FF · Cessna 560CESSNA · Landing Gear Position and Warning
  > DURING 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 BREAKERS
- [SDR CA140602019](https://openairdocs.org/sdr/CA140602019.md): Engine · malfunctioned · May 19, 2014 · Raythn 400ARAYTHEON · Engine (Turbine/Turboprop)
  > (CAN) PILOT ABORTED TAKEOFF DURING TAKEOFF ROLL DUE TO UNCOMMANDED ACCELERATION. PILOT SECURED THE ENGINE AND RETURNED TO RAMP.
- [SDR CA140508003](https://openairdocs.org/sdr/CA140508003.md): Elbow · failed · May 5, 2014 · Cessna 560CESSNA · Engine Bleed Air System
  > (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 PIPE
- [SDR 9JLA2014050604051](https://openairdocs.org/sdr/9JLA2014050604051.md): Wire Harness · intermittent · May 2, 2014 · N426GF · Beech 400A · Engine Fuel System Wiring
  > DURING 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 HAR
- [SDR CA140401006](https://openairdocs.org/sdr/CA140401006.md): Warning Light · illuminated · Mar 27, 2014 · Raythn 400ARAYTHEON · Fuel Controlling System
  > (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.
- [SDR CA140326013](https://openairdocs.org/sdr/CA140326013.md): Oil System · low pressure · Mar 17, 2014 · Cessna 560CESSNA · Engine Oil Indicating System
  > (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
- [SDR CA140313008](https://openairdocs.org/sdr/CA140313008.md): Float Valve · unserviceable · Mar 10, 2014 · Cessna 560CESSNA · Fuel Storage
  > DURING 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
- [SDR CA140313006](https://openairdocs.org/sdr/CA140313006.md): Engine · smoke · Feb 28, 2014 · Raythn 400ARAYTHEON · Engine (Turbine/Turboprop)
  > ACFT 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.
- [SDR CA140224009](https://openairdocs.org/sdr/CA140224009.md): Engine · power loss · Feb 15, 2014 · Raythn 400ARAYTHEON · Engine (Turbine/Turboprop)
  > (CAN) WHILE TAXIING FOR A REGULAR FLIGHT THE NR 2 ENGINE POWER ROLLED BACK AND IT FLAMED OUT. TROUBLESHOOTING IS ONGOING.
- [SDR CA140203006](https://openairdocs.org/sdr/CA140203006.md): Duct · contaminated · Jan 26, 2014 · Engine (Turbine/Turboprop)
  > (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. D

Next page: https://openairdocs.org/engine/pratt-whitney-jt15d-5/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 = 'JT15D5'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/pratt-whitney-jt15d-5/reports

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