# Service difficulty reports: GE CJ610-SER series

A list on [GE CJ610-SER series](https://openairdocs.org/engine/ge-cj610-ser-series.md).

Newest first. General aviation reporting is voluntary.

- [SDR ZP7A20110311001](https://openairdocs.org/sdr/ZP7A20110311001.md): Engine · flamed out · Mar 8, 2011 · N606SM · Lear 25B · Engine (Turbine/Turboprop)
  > MX 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 FL
- [SDR ZP72010F00000](https://openairdocs.org/sdr/ZP72010F00000.md): Motor · shorted · Mar 31, 2010 · N606SM · Lear 25B · Air Distribution Fan
  > CABIN BLOWER MOTOR SHORTED OUT, CAUSING ELECTRICAL SMOKE TO BE EMITTED INTO THE CABIN. SMOKE STOPPED WHEN THE CIRCUIT BREAKER POPPED.
- [SDR CED2006F00006](https://openairdocs.org/sdr/CED2006F00006.md): Fuel Tank · leaking · May 21, 2005 · N140CA · Lear 25B · Fuel Storage
  > ON 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 DI
- [SDR 2004F00189](https://openairdocs.org/sdr/2004F00189.md): Line · loose · Jun 17, 2004 · N8005Y · Lear 25B · Engine (Turbine/Turboprop)
  > WHILE 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 INCID
- [SDR CYO2003F00000](https://openairdocs.org/sdr/CYO2003F00000.md): Indicator · shorted · Jul 16, 2003 · N140CA · Lear 25B · DME/TACAN System
  > AIRCRAFT 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.
- [SDR 070103](https://openairdocs.org/sdr/070103.md): Bleed Valve · out of adjust · Jul 1, 2003 · N425JL · Lear 25B · Compressor Bleed Valve
  > WHILE 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.
- [SDR 2003FA0000480](https://openairdocs.org/sdr/2003FA0000480.md): Fire Loop · loose · May 12, 2003 · N23RZ · Lear 25B · Smoke Detection
  > FIRE 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.
- [SDR 00085](https://openairdocs.org/sdr/00085.md): Line · inoperative · Mar 4, 2003 · N330TW · Lear 24E · Hydraulic System, Main
  > PILOT 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 (PR
- [SDR 00080](https://openairdocs.org/sdr/00080.md): Transmitter · inoperative · Feb 25, 2003 · N330TW · Lear 24E · Communications System
  > PILOT 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 CHECKE
- [SDR 00078](https://openairdocs.org/sdr/00078.md): Fire Loop · grounded · Feb 18, 2003 · N299TW · Lear 24D · Fire Detection
  > AIRCRFT 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.
- [SDR 2002F01026](https://openairdocs.org/sdr/2002F01026.md): Line · cracked · Nov 13, 2002 · N207RG · Lear 24E · Engine Bleed Air System
  > DURING 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 AI
- [SDR 2002F01027](https://openairdocs.org/sdr/2002F01027.md): Line · cracked · Nov 13, 2002 · N207RG · Lear 24E · Engine Fuel Distribution
  > PILOT 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 CRACKE
- [SDR 110702](https://openairdocs.org/sdr/110702.md): Engine · flamed out · Nov 6, 2002 · N254SC · Lear 25B · Engine (Turbine/Turboprop)
  > ENGINE 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
- [SDR 00060](https://openairdocs.org/sdr/00060.md): Seal · failed · Nov 6, 2002 · N330TW · Lear 24E · Turbine Engine Oil System
  > AIRCRAFT 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 AIR
- [SDR 102402](https://openairdocs.org/sdr/102402.md): Oil System · leaking · Oct 21, 2002 · N425JL · Lear 25B · Turbine Engine Oil System
  > DURING DESENT INTO LIT, THE LT ENGINE OIL LIGHT ILLUMINATED. THE ENGINE WAS SHUT DOWN. THE CAUSE WAS A LOOSE OIL LINE, PRESSURE LINE
- [SDR KC82002F00004](https://openairdocs.org/sdr/KC82002F00004.md): Terminal · corroded · Sep 5, 2002 · N588CG · Lear 24D · Flight Control System Wiring
  > NORMAL 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.
- [SDR IKM2002F00000](https://openairdocs.org/sdr/IKM2002F00000.md): Computer · inoperative · Mar 18, 2002 · N118MB · Lear 25B · Landing Gear Steering System
  > STEERING 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 STEERING
- [SDR 00010](https://openairdocs.org/sdr/00010.md): O-Ring · damaged · Jan 14, 2002 · N277TW · Lear 24D · Pneumatic Distribution System
  > RIGHT 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 RETU
- [SDR 00003](https://openairdocs.org/sdr/00003.md): Case · cracked · Oct 13, 2001 · N299TW · Lear 24D · Turbine Section
  > RIGHT 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.
- [SDR 00002](https://openairdocs.org/sdr/00002.md): Fcu · out of adj · Oct 4, 2001 · N333TW · Lear 24 · Fuel Control/Turbine Engines
  > RIGHT ENGINE FLAME-OUT DURING CLIMB FROM 390 TO 410. RESTART AT 240 CLIMB BACK TO 390, NO FURTHER PROBLEM. MAINTENANCE PERFORMED DENSITY ADJUSTMENT.
- [SDR CJP2001F00000](https://openairdocs.org/sdr/CJP2001F00000.md): Hydraulic Line · chafed · Jun 22, 2001 · N600GM · Lear 25D · Hydraulic System, Main
  > TUBE 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 ASSEMBLYS
- [SDR 20010411CW006](https://openairdocs.org/sdr/20010411CW006.md): Control Cable · binding · Mar 21, 2001 · N241JA · Lear 24 · Power Lever
  > LT 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 NOR
- [SDR 31101147KH](https://openairdocs.org/sdr/31101147KH.md): Wire · shorted · Mar 16, 2001 · N147KH · Lear 24 · Auto Flight System Wiring
  > SHORTLY 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 EX
- [SDR 20010402CW005](https://openairdocs.org/sdr/20010402CW005.md): Fire Loop · malfunctioned · Mar 1, 2001 · N252BK · Lear 25B · Fire Detection
  > RIGHT 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 C
- [SDR 96ZZZX915](https://openairdocs.org/sdr/96ZZZX915.md): Engine · flamed out · Oct 30, 1995 · N470TR · Lear 24D · Engine (Turbine/Turboprop)
  > DURING 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 DURIN

## 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 = 'CJ610'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/ge-cj610-ser-series/reports

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