GE CJ610-6

Service difficulty reports · 131

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 = 'CJ6106'
  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 00093Engine · flamed outAIRCRAFT CLIMBING FROM FL410 LT ENGINE FLAMEOUT, RELIGHT AT FL250, CLIMB BACK TO FL330 TO DESTINATION, WILL UPDATE REPORT AFTER MAINTENANCE. MAINTENANCE PERFORMED FLAMEOUT INSPECTION IAW MFG/ MM SEI-186 AND R & R P2 LINE. OPS CK GOOD.May 28, 2003 · N330TW · Lear 24E · Engine (Turbine/Turboprop)SDR 00092Engine · flamed outAIRCRAFT INROUTE FROM MNM TO RWI CLIMBING TO FL450 INCOUNTERED LIGHT TURBULANCE, SPEED DECREASED BELOW .72 LT ENGINE FLAMED OUT. NO EMERGENCY WAS DECLARED REQUESTED LOWER FOR RELIGHT, ENGINE RELIGHT AND CLIMB BACK TO FL410. AIRCRAFT CONTINUED TO DESTINATION,, May 21, 2003 · N324TW · Lear 24D · Engine (Turbine/Turboprop)SDR 00091Engine · flamed outAIRCRAFT DEPARTED ADS DURING CLIMB TO FL430 RH ENGINE FLAMED OUT, ENGINE RELET AND AIRCRAFT LANDED AT LRD, DURING POST FLIGHT INSPECTION NO EVIDENCE OF FOD DAMAGE OR LEAKS FOUND. AIRCRAFT ROUTED TO ADS FOR INSPECTION MAINTENANCE TIGHTENED P3 LINE TO FUEL CONTRMay 15, 2003 · N233TW · Lear 24B · Engine (Turbine/Turboprop)SDR 00087Hose · damagedPILOT REPORTED RT ENGINE FLAMED OUT AT 390, ENGINE RELIGHT AT 250, UNEVENTFUL LANDING AT ADS. MAINTENANCE REPLACED P2 ASPIRATOR HOSE PERFORMED GROUND RUNS, CHECK GOOD.Apr 7, 2003 · N324TW · Lear 24D · Engine (Turbine/Turboprop)SDR 2003F00265Hose · damagedTHE AIRCRAFT EXPERIENCED A FLAME OUT ON THE NR 1 ENGINE AT FL400. ENGINE RESTARTED AT FL250, THE AIRCRAFT ARRIVED IN PHX WITHOUT FURTHER INCIDENT. ENGINE INSPECTED FOR FOD. NONE FOUND. INSPECTED ENGINE PER CJ610 M/M. FOUND ASPIRATOR HOSE BAD. REPLACED HOMar 29, 2003 · N273CA · Lear 25 · Engine Air Intake SystemSDR KC82003F00000Case · warpedFOUND EXHAUST CASE FORWARD FLANGE WARPED CAUSING EXHAUST LEAKAGE AND A FALSE FIRE WARNING. REPLACED EXHAUST CASE WITH OVERHAULED CASE SN GGM1158. TESTED FIRE LOOP SYSTEM IAW MFG MM. GROUND RUN AND LEAK CHECKED EXHAUST CASE. ALL WORK PERFORMED IAW SEI186 AJan 31, 2003 · N75CK · Lear 25D · Engine Collector/Tailpipe/NozzleSDR 00072Engine · flamed outPILOT REPORTED ENGINE LT FLAMEOUT DURING CLIMB AT FL400. DESCENDED AND NORMAL RESTART AT FL220, RETURN TO DEPARTURE AIRPORT FOR MAINTENANCE. WILL UPDATE REPORT AFTER MAINTENANCE. MAINTENANCE COMPLIED WITH FLAMEOUT FLOW CHART FROM CJ610 MM SEI 186 FIG 101, NO Jan 18, 2003 · N233TW · Lear 24B · Engine (Turbine/Turboprop)SDR 00073Engine · flamed outPILOT REPORTED ENGINE FLAME OUT DURING CLIMB, AT FL400, DECEND AND NORMAL RESTART AT FL220, RETURN TO DEPARTURE AIRPORT FOR MAINTENANCE. WILL UPDATE REPORT AFTER MAINTENANCE. MAINTENANCE COMPLIED WITH FLAME OUT FLOW CHART FROM CJ610 MM SEI 186 FIG 1011 NO DEFEJan 18, 2003 · N233TW · Lear 24B · Engine (Turbine/Turboprop)SDR 00067Engine · flamed outPILOT REPORTED LEFT ENGINE FLAMMED OUT DURING CLIMB, PASSING 40,300FT. ATC CLEARED FOR DECENT RELIGHT AT 28K CLIMB BACK TO FL370 TO COMPLETE TRIP. PILOT INSPECTED ENGINE FOR FOD DAMAGE AND LEAKS, NONE FOUND. WILL UPDATE REPORT AFTER AIRCRAFT RETURNS TO MAINTDec 16, 2002 · N324TW · Lear 24D · Engine (Turbine/Turboprop)SDR CA030110006Starter Gen · failed(CAN) DEPARTED AIRPORT AND LEVELED OFF AT FL410. VERY LIGHT TURBULENCE WAS ENCOUNTERED. APPROXIMATELY TWO MINUTES INTO CRUISE, THE RT ENGINE PRODUCED A LIGHT BANG & BEGAN TO SPOOL DOWN. THE RPM'S SETTLED A T 25-30 PERCENT. THE R/H THROTTLE WAS REDUCED TO IDLDec 12, 2002 · Lear 25B · Starter-GeneratorSDR 00066Engine · flamed outPILOT REPORTED THE LT ENGINE FLAMED OUT CLIMBING FROM 41,800 TO 43,000. CENTER CLEARED THEM TO 24,000 FOR RELIGHT. AFTER RELIGHT, CLIMBED BACK TO 39,000. AFTER COMPLETION OF THIS LEG, PILOT INSPECTED ENGINE AND FOUND NO INDICATION OF DAMAGE OR LEAKAGE. ONDec 3, 2002 · N233TW · Lear 24B · Engine (Turbine/Turboprop)SDR 00053Engine · flamed outAIRCRAFT IN ROUTE FROM BRO TO ADS, AT FLT LVL 410 RT ENGINE FLAMED OUT, REQUEST LOWER TO PERFORM RESTART, NORMAL RESTART AND CLIMB TO 390, MAINTENANCE PERFORMED ENGINE CHECKS AT ADS PER THE GE MM SEI 186 FLAMEOUT TROUBLE SHOOTING GUIDE AND PERFORMED GROUND RUNOct 18, 2002 · N233TW · Lear 24B · Engine (Turbine/Turboprop)SDR CED2002F00000Regulator · crackedAIRCRAFT WAS ENROUTE, LOST HYDRAULIC PRESSURE. AIRCRAFT DIVERTED, MAINTENANCE FOUND HYDRAULIC PRESSURE REGULATOR LEAKING. THE VALVE BODY WAS CRACKED AT ONE OF THE BORES. THE TIME ON THE VALVE WAS APPROX 3 HOURS SINCE REPAIR.Sep 5, 2002 · N273CA · Lear 25 · Hydraulic System, MainSDR HAEA00037Engine · damagedPILOT REPORTED NORMAL DEPARTURE FROM KSHV, DURING CLIMB RT ENGINE FIRE WARNING CAME ON AT 10,000FT. CREW SHUTDOWN ENGINE AND RETURNED TO KSHV FOR UNEVENTFUL LANDING. DURING TROUBLESHOOTING FOR ENGINE FIRE LIGHT MAINTENANCE DISCOVERED FOD DAMAGE. REMOVED ANDAug 11, 2002 · N233TW · Lear 24B · Engine (Turbine/Turboprop)SDR 00034Engine · flamed outAIRCRAFT EN ROUTE FROM ADDISON TX TO WINDSOR CANADA RT ENGINE FLAME-OUT CLIMBING FROM 390 TO 410. RESTART NORMAL, CLIMB BACK TO 410 AND CONTINUED TRIP. PILOT INSPECTED ENGINE FOR FOD DAMAGE AT DESTINATION, NO DAMAGE FOUND. AIRCRAFT MOVED TO MAINTENANCE BASEJul 11, 2002 · N525TW · Lear 25 · Engine (Turbine/Turboprop)SDR EAS2002F00000Fuel Control · malfunctionedLT ENGINE FLAMED OUT AT 45,000 FT WITH NO PRIOR ABNORMAL INDICATIONS NOTED. LT ENGINE RESTARTED AT 19,000 FT AND A/C LANDED SAFELY. INSPECTED THE LT ENGINE FUEL SYS, REMOVED FUEL PUMP FILTER. NO DEFECTS OR NOTED. REINSTALLED. REMOVED LT ENGINE FUEL CONTJul 4, 2002 · N701SC · Lear 24D · Fuel Control/Turbine EnginesSDR SO12002F00000Filter · failedFILTERS, LT AND RT ENGINE LOW FUEL PRESSURE LIGHT CAME ON DURING ENGINE POWER RUN. REPLACED LOW PRESSURE FUEL FILTERS AND REMOVED CUSTOMER FURNISHED FILTER FROM MFG NOTIFIED CUSTOMER OF MALFUNCTION AND RECOMMENDED NOT TO USE FUEL FILTERS FROM CERTAIN MFG. BOJul 1, 2002 · N233W · Lear 24B · Aircraft Fuel Filter/StrainerSDR 00030Engine · flamed outAIRCRAFT EN ROUTE FROM ELP TO MCI CLIMBING THROUGH FL420 TO FL450 RT ENGINE FLAMED OUT. DESCENT TO FL250, PERFORMED RESTART AND CLIMBED BACK TO FL410, COMPLETED TRIP NO FURTHER INCIDENT. PILOT INSPECTED FOR FOD OR OTHER DAMAGE AT MCI, NONE FOUND. C/W FLAME-Jun 19, 2002 · N444TW · Lear 24F · Engine (Turbine/Turboprop)SDR 00029Engine · flamed outACFT ROUTE FROM FNT TO ADS CLIMBING THROUGH FL398 FOR FL430 RT ENGINE FLAME-OUT, REQUEST LOWER ALT FL260. ENGINE RESTARTED AND CLIMB BACK TO FL390 PROCEEDED TO ADS. MAINTENANCE AT ADS PERFORMED FLAME-OUT INSPECTION PER THE GE M/M AND PERFORMED ENGINES RUNS, May 29, 2002 · N525TW · Lear 25 · Engine (Turbine/Turboprop)SDR 00027Engine · flamed outAIRCRAFT EN ROUTE FROM MMV TO DKB RT ENGINE FLAME-OUT CLIMBING THROUGH FL410 TO 430, DESCENT TO FL250 PERFORMED AIR START ALL INDICATIONS NORMAL CONTINUED FLT. AT DESTINATION CREW INSPECTED ENGINE, NO DAMAGE NOTED. WILL UPDATE WHEN AIRCRAFT AT MAINTENANCE BAMay 22, 2002 · N233TW · Lear 24B · Engine (Turbine/Turboprop)SDR 00026Engine · flamed outAIRCRAFT EN ROUTE FROM MDW TO MCI AT FL450 CRUISE ENCOUNTERED TURBULENCE LT ENGINE FLAME OUT. REQUESTED LOWER FOR RELIGHT, RELIGHT NORMAL, ALL INDICATIONS NORMAL. CONTINUED FLIGHT, ENGINE INSPECTED ON GROUND, NOTHING FOUND.May 10, 2002 · N266TW · Lear 24D · Engine (Turbine/Turboprop)SDR 00024Engine · flamed outROUTE JVL TO GKY ATTEMPTED TO CLIMB OVER WEATHER FL430 TO FL450 TO TOP THUNDERSTORM RT ENGINE FLAME-OUT. DESCENDED TO FL250 PERFORMED AIR START, ALL OPERATION NORMAL. CONTINUED TO FINAL DESTINATION ADS. MAINTENANCE TO CK ENGINE WILL UPDATE REPORT. MAINTENAMay 1, 2002 · N324TW · Lear 24D · Engine (Turbine/Turboprop)SDR 00021Cotter Pin · out of positionPILOT REPORTED STUCK THROTTLE, FOUND COTTER PIN CATCHING QUADRANT. REPAIRED COTTER PIN , OP'S CHECK GOOD. RETURN AIRCRAFT TO SERVICE.Apr 23, 2002 · N266TW · Lear 24D · FastenersSDR 00015Engine · flamed outMODERATE TURBULENCE CLIMB FLAME-OUT RT ENGINE. DESCENT NORMAL RESTART.Apr 11, 2002 · N666TW · Lear 25B · Engine (Turbine/Turboprop)SDR 00008Engine · flamed outDURING CLIMB THROUGH FLT LEVEL 43.8 LT ENGINE FLAMED OUT. AT FL250 AIRSTART PERFORMED AND CONTINUED FLT AT 370.Jan 7, 2002 · N299TW · Lear 24D · Engine (Turbine/Turboprop)SDR 00009Engine · flamed outDURING CLIMB THROUGH FLT LEVEL 43.8 LT ENGINE FLAMED-OUT, AT FL250 AIRSTART PERFORMED AND CONTINUED FLT AT 370. PILOT PERFORMED VISUAL INSPECTION OF ENGINE AND FUEL SAMPLE. ENGINE INSPECTED AT YIP BY MAINTENANCE WITH NO DEFECTS NOTED.Jan 7, 2002 · N299TW · Lear 24D · Engine (Turbine/Turboprop)SDR 2002F00002Fcu · failedENGINE FLAME OUT DUE TO FUEL CONTROL FAILURE.Dec 28, 2001 · N600XJ · Lear 24B · Fuel Control/Turbine EnginesSDR ESU2002F00000Fuel Control · failedAS THE AIRCRAFT WAS CLIMBING THROUGH FLIGHT 370. THE RIGHT ENGINE FLAMED OUT. THERE WAS NO FIRE AND NO EMERGENCY WAS DECLARED. THE PILOTS WENT THROUGH THE RELIGHT PROCEDURE WHEN THEY ARRIVED AT THE RELIGHT ENVELOPE WITH NO SUCCESS AS THEY WERE UNABLE TO OBTDec 28, 2001 · N600XJ · Lear 24B · Fuel Control/Turbine EnginesSDR HAEA200100003Fire Warning · activatedDURING CLIMB AT FLT LVL 390 RT ENGINE FIRE WARNING ILLUMINATED. REDUCED POWER, LIGHT WENT OUT. RETURNED TO DEPARTURE AIRPORT.Oct 13, 2001 · N299TW · Lear 24D · Fire DetectionSDR BSY2001F00014Engine · flamed outAIRCRAFT WAS AT FL 440 CLIMBING ABOVE SOME STORMS, RIGHT ENGINE FLAMED OUT DUE TO HEAVY TURBULENCE WHICH CAUSED INTERRUPTION OF AIR INTO INLET. AIRCRAFT DESCENDED TO LOWER ALTITUDE, RELIGHT OF ENGINE ACCOMPLISHED. THIS ENGINE HAS HAD NO FLAME-OUT PROBLEMS, OJul 19, 2001 · N121EL · Lear 25 · Engine (Turbine/Turboprop)SDR 20010327CW014Check Valve · failedCABIN COULD NOT MAINTAIN PRESSURIZATION AT FL350, MAINTENANCE PERFORMED A GROUND PRESSURIZATION FUNCTIONAL CHECK NORMALLY. A PNEUMATIC CHECK VALVE DISCOVERED WITH BROKEN SPRING WAS REPLACED, HOWEVER, INITIAL FLIGHT TEST WAS NOT SUCCESSFUL. MAINTENANCE TROUBLFeb 1, 2001 · N241JA · Lear 24 · Cabin Pressure Control SystemSDR CA010209009Blade · separated(CAN) AIRCRAFT IN CLIMB FL110, LOUD BANG HEARD, RT FIRE WARNING ACTIVATED. POWER REDUCED, FUEL SHUT OFF, FIRE WARNING DE-ACTIVATED. AIRCRAFT RETURNED TO DEPARTURE AIRPORT AND SINGLE ENGINE LANDING CARRIED OUT WITHOUT FURTHER INCIDENT. GROUND INSPECTION REVEALEJan 16, 2001 · Lear 25B · Turbine Engine Compressor SectionSDR 20010117AP002Control Cable · seizedLEFT THROTTLE CABLE FROZEN IN FLIGHT-INSPECTION REVEALED THAT CHAFFED ELECTRICAL WIRE CONTACTED THROTTLE, THROTTLE SIEZED IN PLACE.Nov 29, 2000 · N483DM · Lear 24D · Power LeverSDR CA001206006Window · cracked(CAN) DURING AN INSPECTION THE RT FORWARD CABIN WINDOW WAS FOUND CRACKED. THE CRACKS WERE FROM ONE FASTENER HOLE TO THE NEXT. THE WINDOW WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE.Nov 17, 2000 · Lear 25B · Passenger Compartment WindowsSDR CA001206007Window · cracked(CAN) DURING AN INSPECTION THE EMERGENCY EXIT WINDOW WAS FOUND CRACKED. THE CRACKS WERE FROM ONE FASTENER HOLE TO THE NEXT. THE WINDOW WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE.Nov 17, 2000 · Lear 25B · Passenger Compartment WindowsSDR CA001206008Rib · cracked(CAN) DURING AN INSPECTION THE TOP RIB OF THE RUDDER WAS FOUND CRACKED. THE CRACKS WERE LOCATED AROUND THE FORWARD ANCHOR NUT PLATES. THE RIB WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE.Nov 17, 2000 · Lear 25B · Rudder, Spar/RibSDR 20001025SH023Exciter · failedMWD - ON START, LEFT ENGINE WOULD NOT START. FOUND IGNITION EXCITER NOT FIRING TOP OR BOTTOM IGNITER PLUGS. (X)Sep 25, 2000 · N25FM · Lear 25 · ExciterSDR 20000816SH024Fuel Control · malfunctionedON DESCENT TO SLN, ENGINE FLAMED OUT. RE-LIGHT NORMAL AT ALTITUDE 250. INSPECTED ENGINE PER SEI 186. REMOVED AND REPLACED FUEL CONTROL. TEST FLIGHT PERFORMED, NORMAL. (X)Aug 4, 2000 · N251DS · Lear 25D · Fuel Control/Turbine EnginesSDR 20000721SH023Manifold · leakingFUEL MANIFOLD STARTED TO LEAK AT THE SILVER SOLDER JOINT BY THE LARGE B-NUT. FUEL CAUGHT FIRE AND BURNED ENGINE COWL ON TAKEOFF. (X)May 31, 2000 · N239CA · Lear 25B · Engine Fuel DistributionSDR 20000424SH020Engine · flamed outDURING FLIGHT AT ALTITUDE OF 41,000 FEET, RIGHT HAND ENGINE FLAMED OUT. AIRCRAFT WAS CHECKED FOR FOD. AIRCRAFT RETURNED TO P.S.P. AT LOWER ALTITUDE. ENGINE REMOVED FOR REPAIR AT CRS IY2R915K. (X)Mar 20, 2000 · N251DS · Lear 25D · Engine (Turbine/Turboprop)SDR CA000215008Bearing · stuck(CAN) MAIN TRIM ACTUATOR ERRATIC, STICKYJan 11, 2000 · Lear 25B · Stabilizer ActuatorSDR 20000329SH049Engine · flamed outAIRCRAFT AT 43,000 CRUISE M.780, RT ENGINE ROLL BACK RE-LIGHT AT 35,000. PERFORMED INSPECTION OF BLEED AIR SYSTEM, COMPRESSOR FOR FOD. NONE NOTED. PERFORMED MAXIMUM ALTITUDE ACCEL CHECK. ALL WORK PERFORMED IAW MFG MM SEI 186. (X)Dec 15, 1999 · N251DS · Lear 25D · Engine (Turbine/Turboprop)SDR 99ZZZX4247Engine · flamed outDURING CLIMB-OUT, THE LEFT ENGINE EXPERIENCED A FLAME OUT. THE FLIGHT CREW SAID THEY HEARD A POP AND EXPERIENCED ENGINE INDICATIONS ON THE LEFT ENGINE ROLL BACK. THEY DESCENDED AND PROCEEDED TO COMPLETE EMERGENCY AND NORMAL CHECK LISTS. THEY CONCLUDED THE FLOct 30, 1999 · N800GG · Lear 25 · Engine (Turbine/Turboprop)SDR 99ZZZX2971Engine · failedTHE AIRCRAFT WAS EN ROUTE TO PICK UP PASSENGERS IN SARASOTA, FL PASSING THROUGH 41,000 FEET HEADING FOR 43,000 FEET, THE LEFT ENGINE FLAMED OUT. PILOT'S DESCENDED TO 25,000 FEET AND RELIT THE ENGINE ACCORDING TO CHECKLIST PROCEDURES. ACFT WAS LANDED WITHOUT Aug 9, 1999 · N78MC · Lear 35A · Engine (Turbine/Turboprop)SDR CA990715030Bleed Valve · out of adjust(CAN) ENGINE FLAME-OUT AT 41,000 FEET UNDER NORMAL CONDITIONS. FURTHER INSPECTION CARRIED OUT, ADJUSTMENT OF BLEED VALVES INLET BLANKET REPOSITIONED. NO FURTHER FAULTS EXPERIENCED. CONTACTED OPERATOR, NO ACTION REQUIRED.Jun 27, 1999 · Lear 25B · Compressor Bleed ValveSDR 99ZZZX1360O Ring · leakingWHILE EN ROUTE, FLIGHT CREW NOTICED LT RPM FLUCTUATION. ADJUSTMENT OF POWER LEVER ONLY REDUCED RPM. ENGINE POWER WAS LOST. CREW ELECTED TO DIVERT TO TYS AND AN UNEVENTFUL LANDING WAS MADE. MAINTENANCE FOUND A FUEL LEAK AT A DEFECTIVE O-RING FITTING ON THE Mar 1, 1999 · N500JS · Lear 25 · Engine Fuel DistributionSDR 99ZZZX485Fuel Control · malfunctionedLEFT ENGINE COMPRESSOR STALLNG FROM ROTATION TO 2,000 FEET. REPLACED LEFT FUEL CONTROL UNIT. GROUND RUN, LEAK CHECKED, AND TEST FLEW AIRCRAFT, OPS CHECKED GOOD. NO RECOMMENDATIONS TO PREVENT RECURRENCE.Jan 8, 1999 · N63CK · Lear 24 · Fuel Control/Turbine EnginesSDR CA990111009Brushes · worn(CAN) BRUSHES WORN IN JUST 100 HOURS TIME IN-SERVICE THE FIRST TIME. THEN REPAIRED AND WORN IN 76 HOURS THE SECOND TIME. BRUSH HOLDER END BELL ASSY INCORRECTLY RIGGED CAUSING A HIGH FIELD CURRENT.Dec 21, 1998 · Lear 25B · Starter-GeneratorSDR 99ZZZX12Filter · contaminatedWHILE EN ROUTE, FLIGHT CREW NOTICED RT OIL PRESSURE INCREASE FOLLOWED BY RPM FLUCTUATION. CREW DIVERTED TO MOR. MAINTENANCE FOUND OIL SERVICED TO PROPER LEVEL, HOWEVER, THE OIL FILTER WAS CONTAMINATED. ENGINE WAS REMOVED AND REPLACED.Dec 3, 1998 · N95CK · Lear 25D · Turbine Engine Oil SystemSDR 98ZZZM906Ignitor Box · failedRIGHT ENGINE FLAMED OUT AT FL 400, DESCENDED BELOW FL 250, ATTEMPTED RESTART 3 TIMES, SECURED ENGINE LANDED ILM. FOUND IGNITOR BOX. INOP, REPLACED IGNITOR BOX GROUND RUN/POWER RUN NORMAL. UNABLE TO DETERMINE CAUSE OF FLAME OUT AT THIS TIME.Oct 17, 1998 · N20HJ · Lear 25 · Exciter
Back to GE CJ610-6