# Service difficulty reports: GE CJ610-8 A list on [GE CJ610-8](https://openairdocs.org/engine/ge-cj610-8.md). Newest first. General aviation reporting is voluntary. - [SDR 2016FA0000151](https://openairdocs.org/sdr/2016FA0000151.md): Tube · failed · Mar 22, 2016 · Lear 28 · Fuel Controlling System > DURING A ROUTINE FLIGHT THIS TUBE RUPTURED AT THE BASE OF THE FLARE SLEEVE FOR THE B-NUT. THE RUPTURE WAS APPROXIMATELY 50 PERCENT AROUND THE TUBE. THE RUPTURED TUBE CAUSED THE ENGINE TO BE STARVED OF FUEL AND RESULTED IN THE ENGINE SHUTTING DOWN. - [SDR ZP7A2010F00117](https://openairdocs.org/sdr/ZP7A2010F00117.md): Engine · bird ingestion · May 26, 2010 · N25PW · Lear 25D · Engine (Turbine/Turboprop) > BIRD WAS INGESTED INTO LEFT ENGINE JUST AFTER V-1. ENGINE FLAMED OUT, TAKE OFF WAS CONTINUED TO A SAFE ALTITUDE. CREW DECLARED AN EMERGENCY ON CTAF AND RETURNED FOR LANDING. AIRCRAFT LANDED SAFELY, ALL PASSENGERS AND CREWMEMBERS WERE SAFE, NO INJURIES. D - [SDR CJP2006F00000](https://openairdocs.org/sdr/CJP2006F00000.md): Ball Joint · out of adjust · Nov 17, 2006 · N600GM · Lear 25D · Power Lever > NR 1 ENGINE FLAMED OUT WHEN THROTTLED TO IDLE FOR DESCENT. ENGINE WAS SUCCESSFULLY AIR STARTED. UPON LANDING THROTTLES WERE RETARDED AND NR 1 ENGINE FLAMED OUT AGAIN. MAINTENANCE PERSONNEL INSPECTED ENGINE INSTALLATION AND RE-RIGGED NR 1 ENGINE AIRCRAFT THR - [SDR 2005FA0000188](https://openairdocs.org/sdr/2005FA0000188.md): Pump · flaking · Feb 3, 2005 · N101VS · Lear 24D · Engine Fuel Pump > THE INTERNAL COATING IN THE GEAR SECTION OF THE FUEL PUMP STARTED FLAKING OFF AND GOT INTO THE HIGH PRESSURE FUEL LINE THAT GOES TO THE JET PUMPS IN THE RT WING. THE MATERIAL CLOGGED UP THE ORIFICES IN THE JET PUMPS, NOT ALLOWING FUEL TO BE TRANSFERRED FROM - [SDR 4019](https://openairdocs.org/sdr/4019.md): Warning Light · illuminated · Aug 13, 2004 · N228SW · Lear 25D · Fire Detection > ON APPROACH INTO CLT RIGHT ENGINE FIRE LIGHT CAME ON, FIRST STARTED FLICKERING THEN CAME ON STEADY. REDUCED POWER LIGHT WENT OUT, THEN CAME BACK ON AND STAYED ON. SHUT DOWN ENGINE AND BLEW BOTH BOTTLES. - [SDR 4020](https://openairdocs.org/sdr/4020.md): Warning Light · illuminated · Aug 13, 2004 · N228SW · Lear 25D · Fire Detection > ON APPROACH INTO CLT RIGHT ENGINE FIRE LIGHT CAME ON, FIRST STARTED FLICKERING THEN CAME ON STEADY. REDUCED POWER LIGHT WENT OUT, THEN CAME BACK ON AND STAYED ON. SHUT DOWN ENGINE AND BLEW BOTH BOTTLES. - [SDR YDB2004FBBB](https://openairdocs.org/sdr/YDB2004FBBB.md): Tube · unserviceable · Jul 21, 2004 · N4488W · Lear 25D · Landing Gear Brake System > PILOT REPORTED BRAKES WERE VERY WEAK ON LANDING ROLL OUT. FOUND LARGE AMOUNT OF HYDRAULIC FLUID ON AFT PORTION OF AIRCRAFT BELLY. T/S AND FOUND LT ENGINE HYDRAULIC PRESSURE LINE LEAKING AT SUPPORT CLAMP IN TAIL COMPARTMENT. ADEL SUPPORT CLAMP RUBBER CUSHION - [SDR 2004F00045](https://openairdocs.org/sdr/2004F00045.md): Fire Loop · dirty · Jan 13, 2004 · N7810W · Lear 25B · Fire Detection > FALSE FIRE WARNING DURING FLIGHT. AFTER A/C LANDED, PILOT REPORTED INDICATION WAS INTERMITTENT. COWL WAS REMOVED, ENGINE INSPECTED, NO INDICATION OF FIRE/OVERHEAT. DETECTION LOOP INTACT/NO DAMAGE. WIRING CONNECTIONS AT FIREWALL DISCONNECTED, APPEARED TO BE - [SDR DRU2004F00000](https://openairdocs.org/sdr/DRU2004F00000.md): Fire Detector · false indication · Jan 13, 2004 · N7810W · Lear 25B · Fire Detection > FALSE FIRE WARNING DURING FLIGHT. AFTER THE AIRCRAFT LANDED, THE PILOT REPORTED THAT THE INDICATION WAS INTERMITTENT. THE RT ENGINE COWLING WAS REMOVED, AND THE ENGINE WAS INSPECTED. THERE WAS NO INDICATION OF FIRE IN THE ENGINE AREA. THE FIRE LOOP LOOKED - [SDR 2003006](https://openairdocs.org/sdr/2003006.md): Engine · malfunctioned · Dec 17, 2003 · N947TC · Lear 25D · Engine (Turbine/Turboprop) > DURING FLT AT APPROXIMATELY 2:00 AM, AIRCRAFT WAS ENROUTE WHEN THE PILOT NOTICED THAT THE LT ENGINE OIL PRESSURE WAS DECREASING. THE PILOT ALSO NOTICED THAT THE LT EGT WAS CLIMBING. THE PILOT ELECTED TO SHUT DOWN THE LT ENGINE AND RETURN AT THIS TIME. NO EM - [SDR CJP2003F00002](https://openairdocs.org/sdr/CJP2003F00002.md): Control Box · intermittent · Feb 17, 2003 · N800GM · Cessna 650 · Fire Detection > FLIGHT CREW EXPERIENCED INTERMITTENT RIGHT ENGINE FIRE WARNING. AIRCRAFT LANDED AT INTENDED DESTINATION. MAINTENANCE TROUBLESHOT ENGINE PYLON WIRING WHICH IS THE USUAL CAUSE OF INTERMITTENT FIRE WARNINGS, AND COULD NOT RESOLVE PROBLEM. TROUBLESHOOTING MOVED - [SDR DRU2003F00000](https://openairdocs.org/sdr/DRU2003F00000.md): Blanket · burned · Feb 10, 2003 · N7810W · Lear 25B · Airfoil Anti/De-ice System > DURING INSP BY MECH, A BLACK STREAK (FORE TO AFT) WAS NOTICED ON LT HORIZ STAB, THAT BOOT LOOKED BURNT ON L.E. EXAMINATION REVEALED THAT BOOT MUST HAVE SHORTED AGAINST L.E., BURNING BOTH BOOT AND HORIZ STAB CONSISTED OF NICKEL SIZE HOLE BEING COMPLETELY BURNT - [SDR ESUA116360](https://openairdocs.org/sdr/ESUA116360.md): Line · loose · Sep 13, 2002 · N81AX · Lear 25D · Hydraulic System, Main > PILOT DECLARED AN EMERGENCY ON APPROACH, IT WAS DISCOVERED THAT THE HYDRAULIC PRESSURE INDICATED (0). THE GEAR WAS ABLE TO BE PLACED IN THE DOWN AND LOCKED POSITION WITH NO EMERGENCY PROCEDURES. AIRCRAFT LANDED ON 13L. THE AIRCRAFT WAS STOPPED ON THE RUNWAY - [SDR ESY2002F00000](https://openairdocs.org/sdr/ESY2002F00000.md): Engine · failed · Aug 15, 2002 · N947TC · Lear 25D · Engine (Turbine/Turboprop) > FIFTEEN MINUTES AFTER TAKE-OFF, EXPERIENCED FAILURE OF RT ENGINE, WHILE CLIMBING, LEAVING, EVERYTHING WAS NORMAL. NO PREVIOUS ENG ABNORMALITY HAD BEEN NOTED. AT APPROX 20,000 FEET, HEARD LOUD BANG AND EXPERIENCED VIBRATIONS FROM RT ENGINE. ENGINE LOST POWE - [SDR IKM2002F00001](https://openairdocs.org/sdr/IKM2002F00001.md): Wheel · cracked · Apr 5, 2002 · N347JV · Lear 25D · Wheel/Ski/Float > WHEEL, CRACKED, BEAD SEAL AREA. - [SDR IY22002F00000](https://openairdocs.org/sdr/IY22002F00000.md): Structure · corroded · Dec 13, 2001 · N972H · Lear 25D · Wing Main, Frame Structure > DURING PREPARATION OF AIRCRAFT FOR PAINT, CORROSION WAS FOUND ON THE TOP OF THE LEFT WING BETWEEN WING STATIONS 125.00 TO 181.10 AND SPAR NR 5 TO 8 UNDER A RAISED BACK COVER. THE CORROSION IS AS MUCH AS.044 INCHES DEEP. WHEN THE COVER WAS REMOVED, NUMEROUS - [SDR JDMA648B](https://openairdocs.org/sdr/JDMA648B.md): Line · cracked · Feb 14, 2001 · N28AY · Lear 28 · Hydraulic System, Main > HYDRAULIC TRANSFER LINE IN AUXILARY SYSTEM, LINE WAS FOUND BROKEN AT FLAIR CAUSING LOSS OF HYDRAULIC FLUID AND HYDRAULIC SYSTEM FAILURE. AIRCRAFT WAS REPAIRED AND RETURNED TO SERVICE. - [SDR 20010205CW013](https://openairdocs.org/sdr/20010205CW013.md): Hydraulic Line · chafed · Jan 9, 2001 · N25HF · Lear 25D · Hydraulic System, Main > PILOT LOST HYDRAULIC PRESSURE IN FLIGHT. INSPECTION REVEALED HYDRAULIC PRESSURE LINE FROM LEFT ENGINE TO AUXILLARY HYDRALUIC PUMP MANIFOLD LINE, CHAFFED AT CLAMP, RECOMMENDED REMOVING CLAMPS ON THIS SPECIFIC HYDRAULIC LINE ON AIRCRAFT WITH THE SAME HYDRAULIC - [SDR CA001019018](https://openairdocs.org/sdr/CA001019018.md): Accumulator · separated · Sep 21, 2000 · Lear 25B · Engine Thrust Reverser > (CAN) AFTER FLAPS SELECTED TO 10 DEGREES HYDRAULIC PRESSURE DROPPED TO 0 PSI ALTERNATE GEAR EXTENSION USED. FOUND THRUST REVERSER ACCUMULATOR SPLIT IN TWO. WHICH DRAINED ALL HYDRAULIC FLUID AND PUT HOLE IN REAR FUSELAGE. 1. ACCUMULATOR REPLACED SYSTEM GROUND T - [SDR 20010117AP001](https://openairdocs.org/sdr/20010117AP001.md): Engine · flamed out · Sep 20, 2000 · N23RZ · Lear 25B · Engine (Turbine/Turboprop) > ENGINE FLAMED OUT DURING CRUISE-FOUND EXCESSIVE CORROSION OF COMPRESSOR CASING - [SDR 20001016SH006](https://openairdocs.org/sdr/20001016SH006.md): Control Unit · malfunctioned · Aug 3, 2000 · N228SW · Lear 25D · Cabin Pressure Control System > CMH - LOST CABIN PRESSURIZATION AFTER DEPARTURE OUT OF COLUMBUS. RETURNED TO CMH. INSPECTED BLEED AIR LINES IN HEX HOSE AND IN CABIN, RAN BOTH ENGINES, NO LEAKS FOUND. TEST FLEW AIRCRAFT TO 27,000 FEET. ALL FUNCTIONS, PRESSURIZATION SYSTEM, CHECKED GOOD. - [SDR 20000329SH050](https://openairdocs.org/sdr/20000329SH050.md): Starter Gen · failed · Jan 10, 2000 · N988AS · Lear 25D · Starter-Generator > DURING FLIGHT ON 1-10-2000, PILOT NOTICED VIBRATION IN AIRCRAFT, SHORTLY THEREAFTER, GENERATOR OFF-LINE. PILOT LANDED AIRCRAFT AT GJT. STARTER/GENERATOR WAS REPLACED AND GROUND TESTED NORMAL. AIRCRAFT RETURNED TO BASE AT PSP. (X) - [SDR CA991209027](https://openairdocs.org/sdr/CA991209027.md): Transceiver · malfunctioned · Nov 2, 1999 · Lear 25B · VHF Communications System > (CAN) AFTER FLYING THROUGH RAIN ON APPROACH, COMMUNICATION RADIOS BECAME GARBLED/UNREADABLE. BENCH CHECK OF UNITS REVEALED TRANSCEIVER UNITS TO BE INTERNALLY CONTAMINATED WITH WATER. NO LEAKS IN THE NOSE CONE COULD BE FOUND. - [SDR 95ZZZX6579](https://openairdocs.org/sdr/95ZZZX6579.md): Hose · failed · Nov 17, 1995 · N1U · Lear 25D · Engine Anti-Icing System > PILOT STATED LT NACELLE ANTI-ICE INOP AND TRIPPING CIRCUIT BREAKER ON LANDING. AFTER REMOVAL OF TOP COWLING, FOUND HOSE CONNECTING ANTI-ICE TUBE AND ANTI-ICE TEE TUBE WAS TORN IN HALF CAUSING EXPELLED BLEED AIR TO DISCONNECT ANTI-ICE VALVE POWER WIRE FROM CAN ## 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 = 'CJ6108' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/engine/ge-cj610-8/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.