GE CJ610-SER series

Service difficulty reports · 25

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 = 'CJ610'
  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 ZP7A20110311001Engine · flamed outMX PERFORMED AN ADJUSTMENT ON THE FUEL DENSITY AND IDLE RPM ON THE LT ENGINE, WHICH REQUIRES A MAX ALTITUDE ACCELERATION CHECK IAW THE MM CHAP 72-00. FLIGHT CREW LT RDU FOR THE PURPOSE OF PERFORMING THIS CHECK. FLIGHT CREW CLIMBED AND STARTED THE CHECK AT FLMar 8, 2011 · N606SM · Lear 25B · Engine (Turbine/Turboprop)SDR ZP72010F00000Motor · shortedCABIN BLOWER MOTOR SHORTED OUT, CAUSING ELECTRICAL SMOKE TO BE EMITTED INTO THE CABIN. SMOKE STOPPED WHEN THE CIRCUIT BREAKER POPPED.Mar 31, 2010 · N606SM · Lear 25B · Air Distribution FanSDR CED2006F00006Fuel Tank · leakingON TAKEOFF ROLL AND INITIAL CLIMBOUT, FUEL WAS OBSERVED LEAKING FROM THE LT WING TIP. INFORMED THE CREW OF THE LEAK AND INSTRUCTED THEM TO COME AROUND AND LAND. THE CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE LT FUEL VENT AND FOUND NO DIMay 21, 2005 · N140CA · Lear 25B · Fuel StorageSDR 2004F00189Line · looseWHILE EN ROUTE FROM MFE-LIT, CABIN ALTITUDE EXCEEDED 10,000 FT. THE FLIGHT CREW FOLLOWED EMERGENCY PROCEDURES BUT WAS UNABLE TO RETURN THE CABIN PRESSURIZATION WITHIN NORMAL PERIMETERS. THE FLIGHT CREW DECIDED TO DIVERT TO ADS AND LANDED WITHOUT FURTHER INCIDJun 17, 2004 · N8005Y · Lear 25B · Engine (Turbine/Turboprop)SDR CYO2003F00000Indicator · shortedAIRCRAFT WAS ENROUTE FROM BRO TO LIT. FLIGHT CREW EXPERIENCED SLIGHT SMOKE AND A BURNING ODOR, THEY THEN DIVERTED TO SHV. MAINTENANCE CREW INSPECTED AND FOUND DME INDICATOR SHORTED INTERNALLY.Jul 16, 2003 · N140CA · Lear 25B · DME/TACAN SystemSDR 070103Bleed Valve · out of adjustWHILE CLIMBING THROUGH FL40.5, NR 1 ENGINE FLAMEOUT. AIRCRAFT DESENDED TO FL290, THE ENGINE WAS RELIGHT AND AIRCRAFT CONTINUED TO SRQ AT FL240. MAINTENANCE DETERMINED THAT THE BLEED VALVES WERE OUT OF ADJUSTMENT.Jul 1, 2003 · N425JL · Lear 25B · Compressor Bleed ValveSDR 2003FA0000480Fire Loop · looseFIRE DETECTION LIGHT CAME ON IN FLIGHT. REDUCED ENGINE POWER TO IDLE, AFTER 1 MINUTE SHUT DOWN ENGINE AND EXTIGUISHED BOTH BOTTLES. ONCE ON THE GROUND ENGINE WAS INSPECTED, NO EVIDENCE OF FIRE, FOUND LOOSE CONNECTION ON FIRE LOOP.May 12, 2003 · N23RZ · Lear 25B · Smoke DetectionSDR 00085Line · inoperativePILOT REPORTED AFTER DEPARTURE FROM SHV HYDRULIC PRESSURE DROPPED TO 0 UPON GEAR RETRACTION AND FLAP RETRACTION, AIRCRAFT DIVERTED TO ADS STANDBY PUMP WAS USED TO EXTEND GEAR AND FLAPS FOR NORMAL LANDING. WILL UPDATE THIS REPORT AFTER MAINTENANCE. HYDRULIC (PRMar 4, 2003 · N330TW · Lear 24E · Hydraulic System, MainSDR 00080Transmitter · inoperativePILOT REPORTED AIRCRAFT WOULD NOT PRESSURIZE OUT OF 10,000 FT, ALSO COMS HAD STATIC, DIVERT INTO SDF FOR MAINTENANCE. WILL UPDATE REPORT AFTER MAINTENANCE. MAINTENANCE CLEANED SQUAT SWITCHES, JACKED AIRCRAFT AND PERFORMED OPERATIONAL CHECKS, PRESSURIZE CHECKEFeb 25, 2003 · N330TW · Lear 24E · Communications SystemSDR 00078Fire Loop · groundedAIRCRFT DEPARTED YIP FOR IND, ENGINE FIRE WARNING LT ENGINE, ALL OTHER INDICATIONS NORMAL, RETURNED TO DEPARTURE AIRPORT FOR MAINTENANCE. MAINTENANCE FOUND FIRELOOP GROUNDING OUT. ADJUSTED LOOP, OPS CHECK NORMAL.Feb 18, 2003 · N299TW · Lear 24D · Fire DetectionSDR 2002F01026Line · crackedDURING IN-FLIGHT OPERATIONS THE PILOT REPORTED AN UNSAT INDICATION OF THE RT ENGINE ANTI-ICE SYS. AFTER REMOVING THE COWLING, THE ANTI-ICE VALVE BLEED AIR SUPPLY LINE CONNECTOR HOSE WAS FOUND TO BE RUPTURED AND COMPLETELY TORN FREE. THE ANTI-ICE VALVE BLEED AINov 13, 2002 · N207RG · Lear 24E · Engine Bleed Air SystemSDR 2002F01027Line · crackedPILOT REPORTED AN UNSATISFACTORY INDICATION OF RT ENGINE ANTI-ICE SYSTEM. AFTER REMOVING ENGINE COWLING, ANTI-ICE VALVE BLEED AIR SUPPLY LINE CONNECTOR HOSE WAS FOUND TO BE RUPTURED AND COMPLETELY TORN FREE. ANTI-ICE VALVE BLEED AIR SUPPLY LINE HAD ALSO CRACKENov 13, 2002 · N207RG · Lear 24E · Engine Fuel DistributionSDR 110702Engine · flamed outENGINE FLAMED OUT AT FL 390, 20 MIN. INTO THE FLIGHT. PILOT DECLARED AN EMERGANCY. THE PILOT RELITE THE ENGINE. THE AIRCRAFT RETURNED TO THE GROUND AT FXE. THE PROBLEM COULD NOT BE DUPLITCATE ON THE GROUND. A/C WAS RETURNED TO SERVICE. AFTER A TEST FLIGHT WAS Nov 6, 2002 · N254SC · Lear 25B · Engine (Turbine/Turboprop)SDR 00060Seal · failedAIRCRAFT DEPARTED, ON THIRD LEG OF THE DAY, OIL PRESSURE DROPPED AND LOW OIL PRESSURE LIGHT ILLUMINATED. AIRCRAFT DIVERTED, NO EMERGENCY DECLARED. MAINTENANCE WAS SENT, REMOVED AND REPLACED AXIS GEAR SEAL. AIRCRAFT SERVICED AND OPS CHECK GOOD, RETURNED AIRNov 6, 2002 · N330TW · Lear 24E · Turbine Engine Oil SystemSDR 102402Oil System · leakingDURING DESENT INTO LIT, THE LT ENGINE OIL LIGHT ILLUMINATED. THE ENGINE WAS SHUT DOWN. THE CAUSE WAS A LOOSE OIL LINE, PRESSURE LINEOct 21, 2002 · N425JL · Lear 25B · Turbine Engine Oil SystemSDR KC82002F00004Terminal · corrodedNORMAL PITCH TRIM FAILED SHORTLY AFTER TAKE OFF. MAINTENANCE REPORTED FINDING MAIN TRIM POWER WIRE CORRODED AND LOOSE ON RELAY NR 354 LOCATED IN HELL HOLE AREA. TERMINAL END WAS CLEANED AND RESECURED. PERFORMED TRIM SYSTEMS OPERATIONAL CHECK IAW SRM.Sep 5, 2002 · N588CG · Lear 24D · Flight Control System WiringSDR IKM2002F00000Computer · inoperativeSTEERING COMPUTER. OPERATIONAL CHECK SHOWED THE NOSE WHEEL WOULD TURN PAST STEERING LIMIT. REPAIRED COMPUTER FIXED THIS PROBLEM. AFTER INCIDENT, NOSE WHEEL WITH NO POWER COULD TURN LEFT BUT WAS MECHANICALLY STOPPED FROM TURNING RIGHT. NOSE WHEEL STEERINGMar 18, 2002 · N118MB · Lear 25B · Landing Gear Steering SystemSDR 00010O-Ring · damagedRIGHT ENGINE FIRE WARNING ILLUMINATED. ENGINE BROUGHT BACK TO FLIGHT IDLE, LIGHT DID NOT GO OUT. SHUT DOWN ENGINE. MECHANIC DISPATCHED TO AIRCRAFT, INSPECTED ENGINE NO EVIDENCE OF FIRE, FOUND BLEED AIR LEAK AT PYLON REPLACED O-RING AND TWO FIRE BOTTLES RETUJan 14, 2002 · N277TW · Lear 24D · Pneumatic Distribution SystemSDR 00003Case · crackedRIGHT ENGINE FIRE LIGHT ILLUMINATED DURING CLIMB, REDUCTION IN POWER LIGHT WENT OUT. DIVERTED TO YIP FOR MAINTENANCE. CRACK DISCOVERED IN TURBINE EXHAUST CASE ASSEMBLY. CASE WAS WELD REPAIRED BY ENGINE SHOP.Oct 13, 2001 · N299TW · Lear 24D · Turbine SectionSDR 00002Fcu · out of adjRIGHT ENGINE FLAME-OUT DURING CLIMB FROM 390 TO 410. RESTART AT 240 CLIMB BACK TO 390, NO FURTHER PROBLEM. MAINTENANCE PERFORMED DENSITY ADJUSTMENT.Oct 4, 2001 · N333TW · Lear 24 · Fuel Control/Turbine EnginesSDR CJP2001F00000Hydraulic Line · chafedTUBE ASSEMBLY WAS FOUND CHAFED DURING A SCHEDULED INSPECTION OF HYDRAULIC PLUMBING IN TAILCONE. THE TUBE ASSEMBLY WAS REPLACED WITH A NEW TUBE ASSEMBLY. AIRCRAFT HAS HAD AFFECTED TUBE ASSEMBLY PREVIOUSLY REPLACED BY COMPLIANCE WITH SB 25-336. TUBE ASSEMBLYSJun 22, 2001 · N600GM · Lear 25D · Hydraulic System, MainSDR 20010411CW006Control Cable · bindingLT THROTTLE BINDING WHEN ADVANCED FOR TAKEOFF POWER. FOUND BINDING OF LEFT AFT ENGINE THROTTLE CONTROL DUE TO POSSIBLE EXCESSIVE ROUTING OF CONTROL TO CONFORM TO NACELLE SIZE. REROUTED CONTROL TO INCREASE RADIUS OF BEND INSIDE NACELLE AND CONTROL OPERATED NORMar 21, 2001 · N241JA · Lear 24 · Power LeverSDR 31101147KHWire · shortedSHORTLY AFTER DEPARTURE, FLIGHT CREW NOTED A PUSH FORWARD ON THE YOKE. AIRCRAFT RETURNED TO AIRPORT AND LANDED. MAINTENANCE PERSONNEL DISCOVERED A WIRE CHAFFED AND SHORTED TO GROUND GOING TO THE PITCH DISCONNECT BOX. WIRING WAS REPAIRED AND SYSTEM TESTED EXMar 16, 2001 · N147KH · Lear 24 · Auto Flight System WiringSDR 20010402CW005Fire Loop · malfunctionedRIGHT ENGINE FIRE LIGHT ILLUMINATED. CREW SHUT ENGINE DOWN, LIGHT STAYED ON. BLEW ONE FIRE BOTTLE, LIGHT STAYED ON. BLEW SECOND FIRE BOTTLE, LIGHT STAYED ON. LANDED WITHOUT INCIDENT. FALSE FIRE INDICATION. FOUND FORWARD FIRELOOP SENSOR MOUNTED ON UPPER CMar 1, 2001 · N252BK · Lear 25B · Fire DetectionSDR 96ZZZX915Engine · flamed outDURING CLIMB AT 450 FEET, NR 2 ENGINE FLAMED OUT. DESCENDED TO RESTART ALTITUDE, RESTARTED WITH NO APPARENT PROBLEM. LANDED AT NEAREST SUITABLE AIRPORT. INSPECTED ENGINE, FOUND NO IRREGULARITIES. OPERATOR SUSPECTED TURBULENCE AND HIGH ANGLE OF ATTACK DURINOct 30, 1995 · N470TR · Lear 24D · Engine (Turbine/Turboprop)
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