# Service difficulty reports: GE CJ610-6

A list on [GE CJ610-6](https://openairdocs.org/engine/ge-cj610-6.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 131 reports

- [SDR KC8A20121116001](https://openairdocs.org/sdr/KC8A20121116001.md): Engine · flamed out · Nov 16, 2012 · N150CK · Lear 25B · Engine (Turbine/Turboprop)
  > DURING CLIMBOUT FROM KOSC EN ROUTE TO KJFK THROUGH FLIGHT LEVEL 390, THE RIGHT ENGINE FLAMED OUT. ATC WAS CONTACTED, A LOWER ALTITUDE AND RETURNED TO KYIP WAS REQUESTED. DURING DESCENT THROUGH THE RE-LIGHT ENVELOPE, THE ENGINE WAS RE-STARTED AND THE AIRCRAFT
- [SDR 2011F00033](https://openairdocs.org/sdr/2011F00033.md): Filter · contaminated · Feb 10, 2011 · N26AT · Lear 25B · Air Distribution System
  > CABIN WAS PRESSURIZING BUT PILOT REPORTED ERRATIC CABIN RATE OF CLIMB AND ELECTED TO RETURN TO BASE. MX CHECKED TAILCONE FOR PRESSURE LEAKS NONE FOUND. MX CHECKED PRESSURE CONTROLLER AND FOUND CONTAMINATION IN THE FILTER WHICH APPEARED TO BE AN INSECT. REPL
- [SDR KC8AN76CK](https://openairdocs.org/sdr/KC8AN76CK.md): Engine · flamed out · Jun 19, 2009 · N76CK · Lear 25 · Engine (Turbine/Turboprop)
  > LT ENGINE FLAMED OUT AT 40,000FT, DURING CRUISE IN TURBULENT AIR. PILOT DESCENDED TO A LOWER ALTITUDE AND PERFORMED A SUCCESSFUL RELIGHT OF THE ENGINE. NO ABNORMAL ENGINE PERFORMANCE ISSUES NOTED. ACFT CONTINUED TO THE INTENDED DESTINATION. THE ACFT LANDED, W
- [SDR HAEA200800205A](https://openairdocs.org/sdr/HAEA200800205A.md): Pump · failed · Nov 10, 2008 · N525TW · Lear 25 · Fuel Controlling System
  > ENGINE RPM ROLLED BACK FL430 PLUS 30 MINUTES. AIRCRAFT DESCENDED TO FL 150 AND DIVERTED TO GSP. MAINTENANCE DISCOVERED ENGINE DRIVEN FUEL PUMP FAILED. REPLACED FUEL CONTROL/FUEL PUMP ASSY. NO FURTHER DEFECTS.
- [SDR G41A2007003](https://openairdocs.org/sdr/G41A2007003.md): Engine · flamed out · Oct 9, 2007 · N26AT · Lear 25B · Engine (Turbine/Turboprop)
  > LEARJET N26AT WAS ON THE WAY FROM ELP TO LAX AT FL 410, THE CREW WAS EXPERIENCING SEVERE WEATHER AND REQUESTED TO GO TO FL 450. DURING THE CLIMB THEY HIT TURBULENCE AND THE LT ENGINE FLAMED OUT. THEN REQUESTED TO GO DOWN TO FL 250, RELIT THE LT ENGINE, THEN
- [SDR N76CK80606](https://openairdocs.org/sdr/N76CK80606.md): Engine · fod · Aug 6, 2006 · N76CK · Lear 25 · Engine (Turbine/Turboprop)
  > CREW REPORTED RT FIRE WARNING LIGHT FLICKERING WHEN POWER LEVER WAS PULLED BACK TO THE IDLE POSITION. NO SECONDARY INDICATIONS NOTED. FOUND EXHAUST CASE LEAKING AT A FLANGE BOSS. FURTHER INVESTIGATION AFTER REMOVAL OF THE EXHAUST CASE, FOUND SLIGHT TURBINE FOD
- [SDR KC8A0608001](https://openairdocs.org/sdr/KC8A0608001.md): Gasket · blown · Aug 3, 2006 · N76CK · Lear 25 · Fire Detection
  > PILOT REPORTED RT ENGINE FIRE WARNING LIGHT FLICKERING ON DESCENT WITH POWER LEVER REDUCED TO IDLE SPEED. FOUND EXHAUST CASE, CENTER BODY, UPPER RIGHT STRUT SUPPORT FLANGE GASKET BROKEN. REPLACED GASKET WITH NEW GASKET. PERFORMED ENGINE RUN UP AND LEAK-CHECK O
- [SDR HAEA200600191](https://openairdocs.org/sdr/HAEA200600191.md): Engine · power loss · Jun 27, 2006 · N147TW · Lear 25 · Engine (Turbine/Turboprop)
  > AIRCRAFT ENCOUNTERED TURBULENCE AT FL430 AND RT ENGINE LOST POWER. AIRCRAFT DESCENDED AND ENGINE REGAINED POWER AT FL250. MAINTENANCE PERFORMED POST OPERATION INSPECTION. NO VISIBLE INTERNAL/EXTERNAL DAMAGE OR FLUID LEAKAGE EVIDENT ON ENGINE OR COMPONENTS.
- [SDR 4262006N236CA](https://openairdocs.org/sdr/4262006N236CA.md): Compressor Wheel · fod · Apr 26, 2006 · N236CA · Lear 25B · Turbine Engine Compressor Section
  > AT 285 KNOTS AT FL270 THE LT ENGINE WENT DOWN TO 20 PERCENT N1. THE AIRCRAFT DIVERTED AND LANDED UNEVENTFUL. MAINTENANCE FOUND FOD ON THE 1ST STAGE OF THE COMPRESSOR.
- [SDR CED2006F00000](https://openairdocs.org/sdr/CED2006F00000.md): Rudder Pedal · stiff · Nov 1, 2005 · N233CA · Lear 25B · Rudder Control System
  > THE FLIGHT CREW ABORTED TAKEOFF ROLL. THE FLIGHT CREW NOTICED ON TAKEOFF ROLL THAT THE RUDDER PEDALS FELT STIFF AND HAD VERY LITTLE MOVEMENT. MAINTENANCE INSPECTED AIRCRAFT RUDDER CONTROL CABLE SYSTEM AND FOUND NO DEFECTS. (K)
- [SDR CED2006F00021](https://openairdocs.org/sdr/CED2006F00021.md): Engine · shutdown · Oct 4, 2005 · N233CA · Lear 25B · Engine (Turbine/Turboprop)
  > THE NR 2 ENGINE SHUTDOWN. THE FLIGHT CREW FOLLOWED THE EMERGENCY CHECKLIST AND DIVERTED WITHOUT INCEDENT. MAINTENANCE HAS NOT YET INSPECTED THE AIRCRAFT TO DETERMINE THE SPECIFIC PROBLEM. ADDITIONAL INFORMATION WILL BE SUPPLIED AT YOU REQUEST AFTER MAINTENA
- [SDR CED2006F00020](https://openairdocs.org/sdr/CED2006F00020.md): Indicator · defective · Oct 3, 2005 · N238CA · Lear 25 · Engine Pressure Ratio (EPR)
  > THE AIRCRAFT ABORTED TAKEOFF ROLL, THE NR 2 ENGINE WAS NOT MAKING TAKEOFF EPR. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A DEFECTIVE EPR GAUGE. MAINTENANCE REPLACED THE DEFECTIVE GAUGE. (K)
- [SDR CED2006F00005](https://openairdocs.org/sdr/CED2006F00005.md): Altimeter · failed · Sep 1, 2005 · N233CA · Lear 25B · Altimeter, Barometric/Encoder
  > ON DEPARTURE, THE CAPTAIN`S ALTIMETER FAILED. REMOVED AND REPLACED ALTIMETER. SYSTEM OPS CHECK GOOD. (K)
- [SDR CED2006F00010](https://openairdocs.org/sdr/CED2006F00010.md): Engine · malfunctioned · Aug 21, 2005 · N238CA · Lear 25 · Engine (Turbine/Turboprop)
  > HAD TO ABORT THE TAKEOFF WHILE ATTEMPTING TO DEPART. THE REASON FOR THE ABORT WAS THAT THE NR 2 ENGINE WOULD NOT PRODUCE TAKEOFF FOR THE CONDITIONS. MAINTENANCE CHECKED AIRCRAFT AND FOUND IT TO MAKE TAKEOFF EPR ON PERFORMANCE RUN. (K)
- [SDR CED2006F00018](https://openairdocs.org/sdr/CED2006F00018.md): Insulator · dirty · Aug 21, 2005 · N273CA · Lear 25 · Fire Protection System Wiring
  > WHILE DESCENDING THROUGH FL 220 FOR APPROACH INTO AIRPORT, THE NR2 FIRE LIGHT CAME ON MOMENTARILY. IMMEDIATELY REDUCED THE RT THRUST LEVER TO IDLE. MAINTENANCE INSPECTED AIRCRAFT AND FOUND BAD FIRE LOOP CONNECTION. (K)
- [SDR CED2006F00023](https://openairdocs.org/sdr/CED2006F00023.md): Engine · malfunctioned · Jul 21, 2005 · N238CA · Lear 25 · Engine (Turbine/Turboprop)
  > ON TAKEOFF ROLL, THE NR 2 ENGINE WOULD NEVER PRODUCE TAKEOFF. THE CREW ABORTED TAKEOFF ROLL AND EXITED THE RUNWAY. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO DEFECTS. ALL ENGINE PARAMETERS WERE WITHIN NORMAL LIMITATIONS. (K)
- [SDR 7032005N213CA](https://openairdocs.org/sdr/7032005N213CA.md): Hose · kinked · Jul 3, 2005 · N213CA · Lear 25D · Engine Fuel Distribution
  > ENROUTE, UPON THE AIRCRAFT REACHING ITS ASSIGNED LEVEL OF FL 430 POWER WAS REDUCED FOR CRUISE AND THE NR 2 ENGINE QUIT. AIRCRAFT DESCENDED TO FL 250 AND THE ENGINE WAS RESTARTED. THE AIRCRAFT LANDED WITHOUT FURTHER PROBLEMS. (K)
- [SDR 6252004N8005Y](https://openairdocs.org/sdr/6252004N8005Y.md): Cabin Pressure · malfunctioned · Jun 25, 2005 · N8005Y · Lear 25B · Cabin Pressure Control System
  > WHILE ENROUTE, AT FLIGHT LEVEL 410 THE CABIN ALTITUDE EXCEEDED 10000 FT, THE FLIGHT CREW FOLLOWED THE CHECKLIST PROCEDURES AND DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE HAS NOT YET INSPECTED THE AIRCRAFT TO DETERMINE THE SPECIFIC PROBLEM. I W
- [SDR 6242004N238CA](https://openairdocs.org/sdr/6242004N238CA.md): Fire Loop · out of position · Jun 24, 2005 · N238CA · Lear 25 · Fire Detection
  > ON DECENT, THE FLIGHT CREW RECEIVED INDICATION OF FIRE IN THE NR1 ENGINE. THE FLIGHT CREW PERFORMED THE CHECKLIST AND COULD NOT CANCEL THE FIRE LIGHT. THE FLIGHT CREW THEN DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE CREW INSPECTED THE AIR
- [SDR 2006FA0000120](https://openairdocs.org/sdr/2006FA0000120.md): Static Line · loose · Jun 17, 2005 · N8005Y · Lear 25B · Cabin Pressure Control System
  > WHILE ENROUTE, CABIN ALTITUDE EXCEEDED 10,000 FT. THE FLIGHT CREW FOLLOWED EMERGENCY PROCEDURES BUT WAS UNABLE TO RETURN THE CABIN PRESSURIZATION WITHIN NORMAL PIRAMETERS. THE FLIGHT CREW DECIDED TO DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. UPON INSPECT
- [SDR CED2006F00007](https://openairdocs.org/sdr/CED2006F00007.md): Tire · destroyed · Jun 14, 2005 · N236CA · Lear 25B · Tire
  > ON TAKEOFF ROLL THE AIRCRAFT BLEW THE LT MAIN GEAR TIRES IN ELP. (K)
- [SDR CED2006F00019](https://openairdocs.org/sdr/CED2006F00019.md): Fire Detector · false activation · May 28, 2005 · N8005Y · Lear 25B · Fire Detection
  > WHILE ENROUTE, THE CREW EXPERIENCED INDICATION OF FIRE ON THE NR2 ENGINE. THE CREW THEN FOLLOWED THE EMERGENCY CHECK LIST AND COULD NOT EXTINGUISH THE FIRE LIGHT. THE CREW THEN DECLARED AN EMERGENCY AND LANDED AT THEIR DESTINATION WITHOUT FURTHER INCIDENT.
- [SDR CED2006F00014](https://openairdocs.org/sdr/CED2006F00014.md): Element · false indication · May 19, 2005 · N273CA · Lear 25 · Fire Detection
  > AFTER TAKEOFF AT FLIGHT LEVEL 220, THE CREW OBSERVED A FIRE INDICATION LIGHT ON THE NR 1 ENGINE. THE FLIGHT CREW FOLLOWED STANDARD EMERGENCY PROCEDURES AND RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. ONCE BACK, MAINTENANCE FOUND THE FIRE LOOP ELEMENT TOU
- [SDR CED2006F00008](https://openairdocs.org/sdr/CED2006F00008.md): Case · cracked · May 17, 2005 · N239CA · Lear 25B · Engine Collector/Tailpipe/Nozzle
  > WHILE ENROUTE, AT FLIGHT LEVEL 390, FLIGHT CREW OBSERVED A FIRE INDICATION ON THE NR 2 ENGINE. THE FLIGHT CREW WAS ABLE TO EXTINGUISH THE FIRE INDICATION LIGHT USING STANDARD EMERGENCY PROCEDURES. THE FLIGHT CREW THEN DECLARED AN EMERGENCY AND RETURNED TO DE
- [SDR CED2006F00017](https://openairdocs.org/sdr/CED2006F00017.md): Plate · malfunctioned · May 6, 2005 · N140CA · Lear 25B · Compressor Bleed Valve
  > ON DESCENT, THE NR 1 ENGINE STALLED. THE FLIGHT CREW LT THE ENGINE RUNNING AT IDLE AND LANDED WITHOUT INCIDENT. (K)
- [SDR 2004F00421](https://openairdocs.org/sdr/2004F00421.md): Engine · shutdown · Oct 4, 2004 · N233CA · Lear 25B · Engine (Turbine/Turboprop)
  > AT FL370, THE NR 2 ENGINE SHUTDOWN. THE FLIGHT CREW FOLLOWED THE EMERGENCY CHECKLIST AND DIVERTED TO LIT WITHOUT INCIDENT. MAINTENANCE HAS NOT YET INSPECTED THE AIRCRAFT TO DETERMINE THE SPECIFIC PROBLEM. ADDITIONAL INFORMATION WILL BE SUPPLIED AT YOUR REQU
- [SDR 2004F00338](https://openairdocs.org/sdr/2004F00338.md): Control Cable · broken · Sep 1, 2004 · N82TS · Lear 25B · Power Lever
  > THROTTLE CABLE BROKEN 12 INCHES FROM END OF CABLE. BROKEN AT AFT END OF FORWARD CABLE WHERE FORWARD CABLE ATTACHES TO AFT CABLE. (SO13200405891)
- [SDR HAEA200400165](https://openairdocs.org/sdr/HAEA200400165.md): Landing Gear · lack of lube · Aug 18, 2004 · N324TW · Lear 24D · Main Landing Gear
  > LANDING GEAR WOULD NOT RETRACT AFTER TAKE OFF. AIRCRAFT RETURNED TO BASE. MAINTENANCE LUBED LANDING GEAR AND PERFORMED GEAR SWING. CYCLED GEAR AT LEAST 20 TIMES WITH NO FAILURE. MAINTENANCE ITEM CLEARED. [CLOSED]
- [SDR CED2004F00004](https://openairdocs.org/sdr/CED2004F00004.md): Fire Warning · false activation · May 28, 2004 · N8005Y · Lear 25B · Fire Detection
  > WHILE ENROUTE, THE CREW EXPERIENCED INDICATION OF FIRE ON THE NR 2 ENGINE. THE CREW THEN FOLLOWED THE EMERGENCY CHECK LIST AND COULD NOT EXTINGUISH THE FIRE LIGHT. THE CREW THEN DECLARED AN EMERGENCY AND LANDED AT THEIR DESTINATION WITHOUT FURTHER INCIDENT.
- [SDR 00141](https://openairdocs.org/sdr/00141.md): Engine · flamed out · May 24, 2004 · N444TW · Lear 24F · Engine (Turbine/Turboprop)
  > AIRCRAFT ENCOUNTERED TURBULENCE AT FL390K. LT ENGINE FLAMED OUT. ENGINE RELIGHT NORMAL.
- [SDR CED2004F00003](https://openairdocs.org/sdr/CED2004F00003.md): Fuel Sys · leaking · May 21, 2004 · N140CA · Lear 25B · Fuel Storage
  > ON TAKEOFF ROLL AND INITIAL CLIMB OUT, FUEL WAS OBSERVED LEAKING FROM THE LEFT WING TIP. ATC 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 FOUN
- [SDR CED2004F00002](https://openairdocs.org/sdr/CED2004F00002.md): Fire Detector · malfunctioned · May 19, 2004 · N273CA · Lear 25 · Fire Detection
  > AFTER TAKEOFF AT FLIGHT LEVEL 220 THE CREW OBSERVED A FIRE INDICATION LIGHT ON THE NR 1 ENGINE. THE FLIGHT CREW FOLLOWED STARNDARD EMERGENCY PROCEDURES AND RETURNED WITHOUT FURTHER INCIDENT. ONCE BACK IN MAINTENANCE FOUND THE FIRELOOP ELEMENT TOUCHING THE CO
- [SDR CED2004F00001](https://openairdocs.org/sdr/CED2004F00001.md): Case · cracked · May 17, 2004 · N239CA · Lear 25B · Engine Collector/Tailpipe/Nozzle
  > WHILE ENROUTE, AT FLIGHT LEVEL 390 FLIGHT CREW OBSERVED A FIRE INDICATION ON THE NR 2 ENGINE. THE FLIGHT CREW WAS ABLE TO EXTINGUISH THE FIRE INDICATION LIGHT USING STANDARD EMERGENCY PROCEDURES. THE FLIGHT CREW THEN DECLARED AN EMERGENCY AND RETURNED WITH N
- [SDR 00140](https://openairdocs.org/sdr/00140.md): Engine · flamed out · May 14, 2004 · N147TW · Lear 25 · Engine (Turbine/Turboprop)
  > PILOT REPORTED LT ENGINE FLAMED OUT AT FL430 IN SEVERE TURBULANCE ON TRIP FROM HKS TO LRD. ENGINE RELET NORMALLY AT FL 250. CONTINUED TRIP TO LRD. MAINTENANCE PERFORMED INSPECTION IN ACCORDANCE WITH GE M/M 77-00. AIRCRAFT RETURNED TO SERVICE.
- [SDR 2004F00424](https://openairdocs.org/sdr/2004F00424.md): Engine · stalled · May 6, 2004 · N140CA · Lear 25B · Engine (Turbine/Turboprop)
  > ON DESCENT INTO MEMPHIS, TN, THE NR 1 ENGINE STALLED. THE FLIGHT CREW LEFT THE ENGINE RUNNING AT IDLE AND LANDED WITHOUT INCIDENT. (M)
- [SDR 00133](https://openairdocs.org/sdr/00133.md): Engine · flamed out · Mar 20, 2004 · N888TW · Lear 24D · Engine (Turbine/Turboprop)
  > PILOT REPORTED, LT ENGINE FLAMED OUT CLIMBING THRU FL38.5, ENGINE RELET AT FL25. CONTINUED FLIGHT WITH NO FURTHER PROBLEM, PILOT INSPECTED ENGINE AT DESTINATION NO FOD DAMAGE OR LEAKS, AIRCRAFT ROUTED TO MAINTENANCE BASE. YIP, MAINTENANCE PERFORMED FLAMEOUT
- [SDR 00132](https://openairdocs.org/sdr/00132.md): Engine · flamed out · Mar 19, 2004 · N233TW · Lear 24D · Engine (Turbine/Turboprop)
  > PILOT REPORTED RT ENGINE FLAMMED OUT CLIMBING THROUGH FL 39.5 AIRCRAFT DIVERTED TO GRI. MAINTENANCE DISPATCHED FROM ADS, FOUND NO FOD DAMAGE OR LEAKS, RESTRICTED AIRCRAFT 39K ALT AND HAD AIRCRAFT FLOWN TO ADS. WILL UPDATE AFTER FURTHER MAINTENANCE. CORRECTION
- [SDR 00131](https://openairdocs.org/sdr/00131.md): Engine · flamed out · Feb 10, 2004 · N888TW · Lear 24D · Engine (Turbine/Turboprop)
  > PILOT REPORTED LT ENGINE FLAMED OUT CLIMBING FROM FL 370. WILL UPDATE THIS SDR AFTER MAINTENANCE. LT ENGINE REMOVED FOR HSI INSPECTION NO ABNORMAL WEAR REPORTED, PERFORMANCE RUN COMPLETED, ENGINE AND AIRCRAFT RETURN TO SERVICE.
- [SDR CED2004F00000](https://openairdocs.org/sdr/CED2004F00000.md): Tire · separated · Jan 8, 2004 · N233CA · Lear 25B · Tire
  > ON CLIMB OUT, THE NOSE GEAR UNSAFE LIGHT ILLUMINATED. THE CREW CYCLED THE GEAR NUMEROUS TIMES WITH NO CHANGE IN THE UNSAFE INDICATION, THEY THEN RETURNED WITHOUT INCIDENT AND NOTICED THE NOSE WHEEL TIRE WAS MISSING TREAD. UPON INSPECTION OF THE AIRCRAFT, FOU
- [SDR 2004F00223](https://openairdocs.org/sdr/2004F00223.md): Nozzle · damaged · Jan 8, 2004 · N233CA · Lear 25B · Engine Collector/Tailpipe/Nozzle
  > BRO - ON CLIMB-OUT, THE NR 1 ENGINE FLAMED OUT AT 39,600 FEET. THE AIRCRAFT DESCENDED TO FLIGHT LEVEL 25,000 FEET AND RESTARTED THE ENGINE. THE AIRCRAFT THEN DIVERTED TO ADS, AND LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS INSPECTED AND THE EXHAUST NOZZLE
- [SDR 2004FA0000020](https://openairdocs.org/sdr/2004FA0000020.md): Pump · leaking · Jan 6, 2004 · Lear 25B · Engine Fuel Pump
  > INSTALLED OVERHAULED FUEL PUMP FROM MFG ON 4NOV03. DURING AIRCRAFT INSPECTION 22DEC04 HAD FUEL SEEP FROM WIRES ON PUMP.
- [SDR CED2003F00000](https://openairdocs.org/sdr/CED2003F00000.md): Filter · inoperative · Nov 15, 2003 · N233CA · Lear 25B · Aircraft Fuel Filter/Strainer
  > ON NOV 20, 2003, THE AIRCRAFT EXPERIENCED LOW FUEL PRESSURE WARNING LIGHTS. UPON INVESTIGATION OF THE DISCREPANCY WE CHANGED THE FUEL FILTERS BECAUSE THE FELT SEAL HAD CONE UNGLUED AND CLOGGED THE FILTER. THE AIRCRAFT WAS IN FOR A INSPECTION OF THE 15 NOV 20
- [SDR 00117](https://openairdocs.org/sdr/00117.md): Engine · flamed out · Oct 8, 2003 · N237TW · Lear 24D · Engine (Turbine/Turboprop)
  > PILOT REPORTED LT ENGINE FLAMED OUT WHILE CLIMBING TO FL410 IN CONTINOUS LIGHT TO MODERATE TURBULANCE, NO EMERGENCY WAS DECLARED, RELIGHT NORMAL AT FL250, CLIMB TO FL390 FOR REMAINDER OF TRIP, INSPECTION OF ENGINE CONDUCTED AT THE COMPLETION OF TRIP NO FOD OR
- [SDR 00107](https://openairdocs.org/sdr/00107.md): Engine · flamed out · Aug 27, 2003 · N888TW · Lear 24D · Engine (Turbine/Turboprop)
  > PILOT REPORTED LT ENGINE FLAMED OUT CLIMBING FROM FL400 TO FL410 NORMAL RESTART PERFORMED AND RETURN TO FL410 FOR REMAINDER OF FLIGHT WITH NO FURTHER PROBLEM, ENGINE INSPECTED IAW MM AT YIP BASE REPLACED T2 LINE AND OPS CHECKED GOOD.
- [SDR 2003FA0001156](https://openairdocs.org/sdr/2003FA0001156.md): Starter · vibration · Jul 11, 2003 · N99NJ · Lear 25D · Engine Starter
  > WHILE IN CRUISE FLIGHT AT 370, THE FLIGHT CREW HEARD TWO FLUTTERING VIBRATION SOUNDS. THE VIBRATION NOISES BECAME LOUDER AND LOUDER. ADJUSTING THE THROTTLE ISOLATED THE VIBRATION TO THE NR 1 ENGINE. THE PILOTS DESCENDED TO FL 250 AND SHUT DOWN THE NR 1 ENGI
- [SDR 00100](https://openairdocs.org/sdr/00100.md): Uplock Switch · inoperative · Jun 25, 2003 · N324TW · Lear 24D · Landing Gear Position and Warning
  > PILOT REPORTED GEAR WOULD NOT RETRACT AFTER DEPARTING YIP, CREW RETURNED TO YIP WITH GEAR DOWN AND LOCKED INDICATION. MAINTENANCE CLEANED LUBED AND ADJUSTED ALL UPLOCK SWITCHES IAW LEAR M/M AIRCRAFT RETURNED TO SERVICE.
- [SDR 00098](https://openairdocs.org/sdr/00098.md): Engine · flamed out · Jun 11, 2003 · N233TW · Lear 24B · Engine (Turbine/Turboprop)
  > PILOT REPORTED RT ENGINE FLAMED-OUT CLIMBING THRU FL410 FOR FL430. DESCENDED AND RELIGHT NORMAL, CLIMB BACK TO FL410 FOR REMAINDER OF LEG. UPDATE AFTER MAINTENANCE. AIRCRAFT RESTRICTED TO FL410.
- [SDR 00096](https://openairdocs.org/sdr/00096.md): Engine · flamed out · Jun 2, 2003 · N324TW · Lear 24D · Engine (Turbine/Turboprop)
  > PILOT REPORTED LT ENGINE FLAMED-OUT WHILE CLIMBING FROM FL42.5 FOR FL430, DESCEND AND RELIGHT. WILL UPDATE AFTER MAINTENANCE. MAINTENANCE PERFORMED ENGINE INSPECTION AND GROUND RUNS IAW WITH GE M/M AIRCRAFT RETURNED TO SERVICE.
- [SDR 00095](https://openairdocs.org/sdr/00095.md): Engine · flamed out · Jun 1, 2003 · N237TW · Lear 24D · Engine (Turbine/Turboprop)
  > PILOT REPORTED WHILE CLIMBING FROM 410 TO 430 THE LT ENGINE FLAMED-OUT. DESCEND TO RELIGHT ALTITUDE, RELIGHT AND CLIMB BACK TO 410 FOR THE REST OF FLIGHT. WILL UPDATE AFTER MAINTENANCE. NO DEFECTS NOTED. RESTRICTED AIRCRAFT TO FL410.
- [SDR 00094](https://openairdocs.org/sdr/00094.md): Engine · flamed out · May 30, 2003 · N299TW · Lear 24D · Engine (Turbine/Turboprop)
  > PILOT REPORTED LT ENGINE FLAME-OUT WHILE CLIMBING THRU 41,300 FT. DESCEND AND RELIGHT PERFORMED. UPDATE AFTER MAINTENANCE.

Next page: https://openairdocs.org/engine/ge-cj610-6/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 = 'CJ6106'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/ge-cj610-6/reports

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