# GE CF34-3A2 - Type: Engine model (FAA registry) - Registry code: 30067 - Manufacturer (registry): GE - Model: CF34-3A2 - Engine type: Turbo-fan - Power: 9,220 lb thrust - Data sheet: [TCDS E15NE](https://openairdocs.org/tcds/E15NE) (OpenAirDocs) - Holder: General Electric Company GE Aerospace - Installed in: 20 registered aircraft - Page: https://openairdocs.org/engine/ge-cf34-3a2 Model codes come from the FAA registry's reference file. ## ADs that may apply (OpenAirDocs) Matched to this engine model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. - [AD 2020-08-01](https://openairdocs.org/ad/2020-08-01): Turbine Engine Inlet Section · General Electric CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective May 15, 2020 - [AD 2009-26-09](https://openairdocs.org/ad/2009-26-09): Fan disks · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Feb 11, 2010 - [AD 2010-01-04](https://openairdocs.org/ad/2010-01-04): Fan blade · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Jan 25, 2010 - [AD 2009-07-12](https://openairdocs.org/ad/2009-07-12): High-pressure (HP) · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective May 7, 2009 - [AD 2006-04-12](https://openairdocs.org/ad/2006-04-12): Stage 5 low pressure turbine (LPT) disks · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Mar 30, 2006 - [AD 2004-26-02](https://openairdocs.org/ad/2004-26-02): Certain high pressure compressor (HPC) · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Jan 26, 2005 - [AD 2001-12-06](https://openairdocs.org/ad/2001-12-06): Lubrication System for the Engine Bearings · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Jul 20, 2001 - [AD 99-23-26 R1](https://openairdocs.org/ad/99-23-26-R1): Main Fuel Control (MFC) · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Feb 17, 2000 - [AD 99-22-10](https://openairdocs.org/ad/99-22-10): High Pressure Compressor (HPC) Spool and Disk · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 1 more. Effective Dec 27, 1999 - [AD 97-06-15](https://openairdocs.org/ad/97-06-15): HPC Stage 1 rotor disk · General Electric Aircraft Engines CF34-1A, CF34-3A and CF34-3A2. Effective May 27, 1997 - [AD 97-06-14](https://openairdocs.org/ad/97-06-14): Fan Disk · General Electric Aircraft Engines CF34-1A, CF34-3A and CF34-3A2. Effective May 27, 1997 Historical (superseded or no longer in force): - [AD 2009-24-11](https://openairdocs.org/ad/2009-24-11) (historical): Fan blades · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Jan 4, 2010 - [AD 2007-07-07 R1](https://openairdocs.org/ad/2007-07-07-R1) (historical): Fan disks · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Sep 12, 2007 - [AD 2007-07-07](https://openairdocs.org/ad/2007-07-07) (historical): Fan disks · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Apr 23, 2007 - [AD 2006-05-04](https://openairdocs.org/ad/2006-05-04) (historical): Fan disks · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Apr 7, 2006 - [AD 2001-10-03](https://openairdocs.org/ad/2001-10-03) (historical): Fan Disks · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective May 31, 2001 - [AD 99-23-26](https://openairdocs.org/ad/99-23-26) (historical): Main Fuel Control (MFC) · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Dec 6, 1999 - [AD 99-11-08](https://openairdocs.org/ad/99-11-08) (historical): Main Fuel Control (MFC) · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Jul 27, 1999 ## Information bulletins (advisory) (1) - [SAIB NE-04-77](https://openairdocs.org/saib/NE-04-77): . Issued Aug 12, 2004 ## Registered aircraft (20) - [N117AA](https://openairdocs.org/aircraft/N117AA): [Corsair Two LLC](https://openairdocs.org/faa-owner/CORSAIR%20TWO%20LLC), [Hillsboro, OR](https://openairdocs.org/faa-place/OR/Hillsboro), built 1990, S/N 5060 - [N226EC](https://openairdocs.org/aircraft/N226EC): [Bcp Fa Ap LLC](https://openairdocs.org/faa-owner/BCP%20FA%20AP%20LLC), [Providence, RI](https://openairdocs.org/faa-place/RI/Providence), built 1991, S/N 5090 - [N360](https://openairdocs.org/aircraft/N360): [Lga Trading LLC](https://openairdocs.org/faa-owner/LGA%20TRADING%20LLC), [Sheridan, WY](https://openairdocs.org/faa-place/WY/Sheridan), built 1990, S/N 5068 - [N360RL](https://openairdocs.org/aircraft/N360RL): [Tvpx Aircraft Solutions Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20AIRCRAFT%20SOLUTIONS%20INC%20TRUSTEE), [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake), built 1991, S/N 5089 - [N366LP](https://openairdocs.org/aircraft/N366LP): [Alliance Air Parts Acquisitions Corp](https://openairdocs.org/faa-owner/ALLIANCE%20AIR%20PARTS%20ACQUISITIONS%20CORP), [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City), S/N 5091, Non-citizen corporation, flight hours not reported - [N368FJ](https://openairdocs.org/aircraft/N368FJ): [Valiair Lc Trustee](https://openairdocs.org/faa-owner/VALIAIR%20LC%20TRUSTEE), [Casper, WY](https://openairdocs.org/faa-place/WY/Casper), built 1989, S/N 5049 - [N403JC](https://openairdocs.org/aircraft/N403JC): [Lawsuit Air LLC](https://openairdocs.org/faa-owner/LAWSUIT%20AIR%20LLC), [Onalaska, TX](https://openairdocs.org/faa-place/TX/Onalaska), built 1989, S/N 5059 - [N601LC](https://openairdocs.org/aircraft/N601LC): [Mannu 03 Holding LLC](https://openairdocs.org/faa-owner/MANNU%2003%20HOLDING%20LLC), [Locust Grove, GA](https://openairdocs.org/faa-place/GA/Locust%20Grove), built 1993, S/N 5129 - [N601WY](https://openairdocs.org/aircraft/N601WY): [601 Assets LLC](https://openairdocs.org/faa-owner/601%20ASSETS%20LLC), [Lighthouse Point, FL](https://openairdocs.org/faa-place/FL/Lighthouse%20Point), built 1992, S/N 5117 - [N602NP](https://openairdocs.org/aircraft/N602NP): [Six Hundred Np LLC](https://openairdocs.org/faa-owner/SIX%20HUNDRED%20NP%20LLC), [Valparaiso, IN](https://openairdocs.org/faa-place/IN/Valparaiso), built 1992, S/N 5121 - [N64JS](https://openairdocs.org/aircraft/N64JS): [Celebration Tv America Inc](https://openairdocs.org/faa-owner/CELEBRATION%20TV%20AMERICA%20INC), [Houston, TX](https://openairdocs.org/faa-place/TX/Houston), built 1992, S/N 5119 - [N691CC](https://openairdocs.org/aircraft/N691CC): [Wilmington Trust Co Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20CO%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 1993, S/N 5126 - [N723GH](https://openairdocs.org/aircraft/N723GH): [Starship 1 LLC](https://openairdocs.org/faa-owner/STARSHIP%201%20LLC), [Houston, TX](https://openairdocs.org/faa-place/TX/Houston), built 1991, S/N 5086 - [N836CM](https://openairdocs.org/aircraft/N836CM): [Bel Aviation LLC](https://openairdocs.org/faa-owner/BEL%20AVIATION%20LLC), [Nokomis, FL](https://openairdocs.org/faa-place/FL/Nokomis), built 1990, S/N 5079 - [N856JL](https://openairdocs.org/aircraft/N856JL): [Zjets Aviation LLC](https://openairdocs.org/faa-owner/ZJETS%20AVIATION%20LLC), [Richmond, TX](https://openairdocs.org/faa-place/TX/Richmond), built 1991, S/N 5094 - [N868RB](https://openairdocs.org/aircraft/N868RB): [Sav Aviation LLC](https://openairdocs.org/faa-owner/SAV%20AVIATION%20LLC), [Jacksonville, TX](https://openairdocs.org/faa-place/TX/Jacksonville), built 1993, S/N 5128 - [N878EM](https://openairdocs.org/aircraft/N878EM): [Core Systems](https://openairdocs.org/faa-owner/CORE%20SYSTEMS), [Poway, CA](https://openairdocs.org/faa-place/CA/Poway), built 1990, S/N 5074 - [N939CC](https://openairdocs.org/aircraft/N939CC): [601 Assets LLC](https://openairdocs.org/faa-owner/601%20ASSETS%20LLC), [Lighthouse Point, FL](https://openairdocs.org/faa-place/FL/Lighthouse%20Point), built 1992, S/N 5124 - [N9771C](https://openairdocs.org/aircraft/N9771C): [Bimo 3.0 LLC](https://openairdocs.org/faa-owner/BIMO%203.0%20LLC), [Spring Hill, FL](https://openairdocs.org/faa-place/FL/Spring%20Hill), S/N 5063 - [N999AT](https://openairdocs.org/aircraft/N999AT): [Aircraft Guaranty Corp Trustee](https://openairdocs.org/faa-owner/AIRCRAFT%20GUARANTY%20CORP%20TRUSTEE), [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City), S/N 5178 ## NTSB investigations None matched to aircraft with this engine model. ## FAA accident and incident reports None matched to aircraft with this engine model. ## Service difficulty reports (24) As reported by operators and repair stations, by the model named in the report. - [SDR 2019FA0000302](https://openairdocs.org/sdr/2019FA0000302), Aug 30, 2019: BLEED VALVE. LEAKING. DUCT AIR FLASHING LIGHT ILLUMINATED. LOOKED ON OVERHEAD PANEL AND SAW DUCT FAIL LIGHT ILLUMINATED. TURNED BOTH 14TH STAGE VALVES OFF ACCORDING TO CHECKLIST AND - [SDR J6BA2019091200000](https://openairdocs.org/sdr/J6BA2019091200000), Aug 13, 2019: BLEED VALVE. LEAKING. DUCT AIR FLASHING LIGHT ILLUMINATED. LOOKED ON OVERHEAD PANEL AND SAW DUCT FAIL LIGHT ILLUMINATED. TURNED BOTH 14TH STAGE VALVES OFF ACCORDING TO CHECKLIST AND - [SDR WWQA20190403102](https://openairdocs.org/sdr/WWQA20190403102), Apr 2, 2019: GEARBOX. BROKEN. AIRCRAFT WAS IN FLIGHT WHEN LEFT ENGINE RPM ROLLED BACK AND ENGINE SHUTDOWN UN-COMMANDED, AIRCRAFT DIVERTED AND LANDED. MAINTENANCE TROUBLESHOT TO A FAULTY ACCE - [SDR CA190402010](https://openairdocs.org/sdr/CA190402010), Mar 31, 2019: PITOT SYSTEM. CONTAMINATED. (CAN) AIRPLANE DIVERTED FOR UNSCHEDULED LANDING WITH FOLLOWING ISSUE: AT FLIGHT LEVEL CRUISE AT FL370 WITH MODERATE RAIN AND BUMPINESS THE AIRSPEED OF THE LH PR - [SDR 2017F00074](https://openairdocs.org/sdr/2017F00074), Mar 20, 2017: HYDRAULIC SYSTEM. MALFUNCTIONED. AFTER LANDING, AND DURING TAXI LEAVING THE RUNWAY, LOST HYDRAULIC POWER, RECEIVED A STICK SHAKER AND AURAL ALERT FOR A STALL. LOST NOSE WHEEL STEERING AND BRAKE - [SDR 2017FA0000108](https://openairdocs.org/sdr/2017FA0000108), Mar 16, 2017: TIRE. FAILED. WHEN ACFT DEPARTED, THE NR 2 TIRE TREAD SEPARATION, SIDEWALL OF THE TIRE. THE CREW DID NOT FEEL OR HEAR ANYTHING. TIRE DAMAGE FOUND ON POST FLIGHT INSPECTION. - [SDR CA151111001](https://openairdocs.org/sdr/CA151111001), Oct 16, 2015: BOLT. FAILED. (CAN) DURING PRE-FLIGHT, FOUND ONE BOLT SHEARED ON NUMBER 3 MAIN WHEEL. AFTER INVESTIGATION IT WAS FOUND THAT THE WHEEL HAD LAST BEEN OVERHAULED AND NO BOLT WER - [SDR CA151002001](https://openairdocs.org/sdr/CA151002001), Oct 2, 2015: LINE. LEAKING. (CAN) IN FLIGHT, LH HYDRAULIC ENGINE PUMP FAIL LIGHT CAME ON - PRESSURE 0 PSI AT NR 1 HYDRAULIC SYSTEM, AS REPORTED BY CREW. ON GROUND, FOUND EVIDENCE OF HYDRAU - [SDR CA150820012](https://openairdocs.org/sdr/CA150820012), Aug 4, 2015: TRANSCEIVER. FAILED. (CAN) WEATHER RADAR TRANSCEIVER FAILED DURING CRUISE. WEATHER RADAR WAS INOPERATIVE. - [SDR 2013FA0000766](https://openairdocs.org/sdr/2013FA0000766), Nov 12, 2013: TIRE. FAILED. AFTER LANDING, THE CREW FOUND THAT THE NR 1 MLG TIRE HAD LOST MOST OF THE TIRE TREAD. THE TIRE ONLY HAD 101 LANDING ON IT WITH .0937 TREAD REMAINING. - [SDR CA131121013](https://openairdocs.org/sdr/CA131121013), Nov 5, 2013: TIRE. DAMAGED. (CAN) ON CREW WALK AROUND, FOUND TIRE WITH PARTIAL TREAD LOSS. - [SDR CA130916007](https://openairdocs.org/sdr/CA130916007), Sep 14, 2013: FITTING. LEAKING. (CAN) FITTING, PN MS 21926-6D IN MLG RUN AROUND AND DUMP VALVE STARTED TO LEAK DURING GEAR SWINGS DUE TO GEAR REPLACEMENT. FITTING WAS REMOVED AND INSPECTED. A - [SDR CA130114012](https://openairdocs.org/sdr/CA130114012), Jan 11, 2013: TIE BOLT. SHEARED. (CAN) DURING WALK AROUND INSPECTION, NOTICED NR 3 MAIN WHEEL ASSY MISSING TIE BOLT. REMOVED WHEEL AND FOUND THE BOLT HAD SHEARED LEAVING THE HEAD AND WASHER BET - [SDR 2012FA0000545](https://openairdocs.org/sdr/2012FA0000545), Jul 12, 2012: TIRE. WORN. AFTER LANDING, CREW FOUND THAT THE NR 2 MLG TIRE HAD LOST MOST OF THE TIRE TREAD. THE TIRE ONLY HAD 131 LANDINGS, WITH .1562 TREAD REMAINING. - [SDR CA110908001](https://openairdocs.org/sdr/CA110908001), Sep 7, 2011: ENGINE. MALFUNCTIONED. (CAN) AFTER DEPARTURE, THE ACFT WAS CLIMBING THROUGH, APPROX 20,000- 21,000 FEET, WHEN THE CREW NOTICED THE RT ENGINE, "RED LOW OIL PRESSURE LIGHT", ON, AS WELL - [SDR CA110803015](https://openairdocs.org/sdr/CA110803015), Aug 2, 2011: ENGINE. INOPERATIVE. (CAN) THEY WERE AT CRUISE ALTITUDE WHEN THE CAPTAIN NOTICED THE LT ENGINE OIL PRESSURE WAS ON THE RISE AND REACHING THE YELLOW BAND. HE PULLED THE POWER BACK A - [SDR CA110106010](https://openairdocs.org/sdr/CA110106010), Jan 6, 2011: ACTUATOR. WORN. DURING AN APPROACH AT QB, THE CAPTAIN DURING THE DESCENT TRIED TO SET THE FLAPS DOWN AND HE HAD FLAP FAIL AT 15 DEGREES (JAM), CALLED THE TOWER FOR EMERGENCY LA - [SDR 2012FA0000557](https://openairdocs.org/sdr/2012FA0000557), Dec 8, 2010: TIRE. WORN. AFTER LANDING, THE CREW FOUND THAT THE NR3 MLG TIRE HAD LOST MOST OF THE TIRE TREAD. THE TIRE HAD 115 LANDING ON IT WITH .1562 TREAD REMAINING. - [SDR 2012FA0000556](https://openairdocs.org/sdr/2012FA0000556), Sep 27, 2010: TIRE. WORN. AFTER LANDING, CREW FOUND THA THE NR 2 MLG TIRE HAD LOST MOST OF THE TIRE TREAD. TIRE HAD 113 LANDINGS WITH .1562 TREAD REMAINING. - [SDR CA081017005](https://openairdocs.org/sdr/CA081017005), Oct 17, 2008: LINE. BURST. (CAN) AFTER TAKEOFF IN CRUISE AND ON THE WAY NR 2 HYD PRESS LOST MASTER CAUTION ON REPORT BY THE CAPTAIN, HE STILL HAD HIS NR 1 AND NR 3 HYD SYSTEM. ACFT LANDED - [SDR CA080813003](https://openairdocs.org/sdr/CA080813003), Aug 12, 2008: HYDRAULIC LINE. BURST. (CAN) IN FLIGHT NR 2 HYDR "LO PRESS" CAME ON, FWD BY "LO LEVEL". NR 2 HYDR FLUID COMPLETLY LOST THROUGH A BURST HYDR PRESSURE HOSE IN RT NACELLE. - [SDR CA080225005](https://openairdocs.org/sdr/CA080225005), Feb 22, 2008: SHAFT. BROKEN. (CAN) 3 MINUTES AFTER TAKEOFF, GENERATOR FAILED, AC RETURNED TO BASE. GENERATOR REMOVED, FOUND BROKEN SHAFT INSIDE THE IDG (NOT THE MAIN SHAFT). IT BROKE, MELTE - [SDR CA080304001](https://openairdocs.org/sdr/CA080304001), Feb 4, 2008: COMPUTER. FAULTY. (CAN) IT TOOK (3) STALL WARNING COMPUTER BEFORE GETTING ONE THAT WAS SERVICEABLE , THEY ALL FAIL THE TEST IAW TEST PROCEDURE MM PSP601-2 CHAP 27-39-00 P 206 207 - [SDR CA071022001](https://openairdocs.org/sdr/CA071022001), Oct 19, 2007: TUBE. CRACKED. (CAN) DURING POWER PLANT BUILD UP, FOUND LINE P/N 228-52402-115 FOR PYLON STATIC PRESSURE TO FCU CRACKED AT MIDDLE. THE CRACK WAS HIDDEN BY A LINE IDENTIFICATIO --- 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.