# GE CF34-3A1 - Type: Engine model (FAA registry) - Registry code: 30068 - Manufacturer (registry): GE - Model: CF34-3A1 - 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: 15 registered aircraft - Page: https://openairdocs.org/engine/ge-cf34-3a1 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 2005-18-16](https://openairdocs.org/ad/2005-18-16): High pressure turbine (HPT) rotating components · General Electric Aircraft Engines CF34-3A1. Effective Oct 13, 2005 - [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 2003-05-10 R1](https://openairdocs.org/ad/2003-05-10-R1): B-Sump Scavenge Screens · General Electric Aircraft Engines CF34-3A1, CF34-3B and CF34-3B1. Effective Nov 18, 2003 - [AD 2002-05-02](https://openairdocs.org/ad/2002-05-02): Life-Limited Rotating Parts · General Electric Aircraft Engines CF34-3A1 and CF34-3B1. Effective Apr 12, 2002 - [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 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 2007-05-16](https://openairdocs.org/ad/2007-05-16) (historical): Fan disks for an arc-out defect · General Electric Aircraft Engines CF34-3A1, CF34-3B and CF34-3B1. Effective Mar 12, 2007 - [AD 2007-04-51](https://openairdocs.org/ad/2007-04-51) (historical): Uncontained fan disk failure during flight operation · General Electric Aircraft Engines CF34-3A1, CF34-3B and CF34-3B1 - [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 2004-15-03 R1](https://openairdocs.org/ad/2004-15-03-R1) (historical): Stage 5 low pressure turbine (LPT) disks · General Electric Aircraft Engines CF34-3A1 and CF34-3B1. Effective Aug 31, 2004 - [AD 2004-15-03](https://openairdocs.org/ad/2004-15-03) (historical): Stage 5 Low Pressure Turbine (LPT) Disks · General Electric Aircraft Engines CF34-3A1 and CF34-3B1. Effective Aug 16, 2004 - [AD 2003-05-10](https://openairdocs.org/ad/2003-05-10) (historical): B-sump Oil Scavenge System · General Electric Aircraft Engines CF34-3A1, CF34-3B and CF34-3B1. Effective Apr 2, 2003 - [AD 2001-19-02](https://openairdocs.org/ad/2001-19-02) (historical): B-sump Scavenge Screens · General Electric Aircraft Engines CF34-3A1, CF34-3B and CF34-3B1. Effective Oct 9, 2001 - [AD 2000-03-03 R1](https://openairdocs.org/ad/2000-03-03-R1) (historical): Life-limited Parts · General Electric Aircraft Engines CF34-3A1 and CF34-3B1. Effective Jun 19, 2001 - [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 2000-03-03](https://openairdocs.org/ad/2000-03-03) (historical): Critical Life-Limited Rotating Engine Parts · General Electric Aircraft Engines CF34-3A1 and CF34-3B1. Effective Mar 13, 2000 - [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 (15) - [N1DH](https://openairdocs.org/aircraft/N1DH): [Bc Leasing LLC](https://openairdocs.org/faa-owner/BC%20LEASING%20LLC), [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta), built 1993, S/N 5145 - [N207JB](https://openairdocs.org/aircraft/N207JB): [Cypress Cove Air LLC](https://openairdocs.org/faa-owner/CYPRESS%20COVE%20AIR%20LLC), [Phoenix, AZ](https://openairdocs.org/faa-place/AZ/Phoenix), built 1996, S/N 5194 - [N222PH](https://openairdocs.org/aircraft/N222PH): [N915tf Leasing LLC](https://openairdocs.org/faa-owner/N915TF%20LEASING%20LLC), [Benton, KS](https://openairdocs.org/faa-place/KS/Benton), built 1994, S/N 5151 - [N22FY](https://openairdocs.org/aircraft/N22FY): [Fya LLC](https://openairdocs.org/faa-owner/FYA%20LLC), [Milwaukee, WI](https://openairdocs.org/faa-place/WI/Milwaukee), built 1993, S/N 5142 - [N242CK](https://openairdocs.org/aircraft/N242CK): [Kalitta Air LLC](https://openairdocs.org/faa-owner/KALITTA%20AIR%20LLC), [Ypsilanti, MI](https://openairdocs.org/faa-place/MI/Ypsilanti), built 1995, S/N 5181 - [N320TM](https://openairdocs.org/aircraft/N320TM): [Worldwide Option LLC](https://openairdocs.org/faa-owner/WORLDWIDE%20OPTION%20LLC), [Lewes, DE](https://openairdocs.org/faa-place/DE/Lewes), built 1995, S/N 5175 - [N441PJ](https://openairdocs.org/aircraft/N441PJ): [Novajet Holdings Inc](https://openairdocs.org/faa-owner/NOVAJET%20HOLDINGS%20INC), [Fort Lauderdale, FL](https://openairdocs.org/faa-place/FL/Fort%20Lauderdale), S/N 5170 - [N501KV](https://openairdocs.org/aircraft/N501KV): [Roman Empire Aba Services Inc](https://openairdocs.org/faa-owner/ROMAN%20EMPIRE%20ABA%20SERVICES%20INC), [Goodyear, AZ](https://openairdocs.org/faa-place/AZ/Goodyear), built 1995, S/N 5173 - [N580KR](https://openairdocs.org/aircraft/N580KR): [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 1994, S/N 5148 - [N601JP](https://openairdocs.org/aircraft/N601JP): [Love Aviation LLC](https://openairdocs.org/faa-owner/LOVE%20AVIATION%20LLC), [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas), built 1994, S/N 5168 - [N61FF](https://openairdocs.org/aircraft/N61FF): [Payne Aviation Weslaco LLC](https://openairdocs.org/faa-owner/PAYNE%20AVIATION%20WESLACO%20LLC), [Weslaco, TX](https://openairdocs.org/faa-place/TX/Weslaco), built 1994, S/N 5166 - [N67RS](https://openairdocs.org/aircraft/N67RS): [Labell Aviation LLC](https://openairdocs.org/faa-owner/LABELL%20AVIATION%20LLC), [Spring Hill, FL](https://openairdocs.org/faa-place/FL/Spring%20Hill), built 1994, S/N 5149 - [N7164](https://openairdocs.org/aircraft/N7164): [Crj Capital Corp](https://openairdocs.org/faa-owner/CRJ%20CAPITAL%20CORP), [Miami, FL](https://openairdocs.org/faa-place/FL/Miami), built 1997, S/N 7164 - [N719AV](https://openairdocs.org/aircraft/N719AV): [Lead And Steel LLC](https://openairdocs.org/faa-owner/LEAD%20AND%20STEEL%20LLC), [Fountain Valley, CA](https://openairdocs.org/faa-place/CA/Fountain%20Valley), built 1996, S/N 7159 - [N998CA](https://openairdocs.org/aircraft/N998CA): [M&D Aviation LLC](https://openairdocs.org/faa-owner/M%26D%20AVIATION%20LLC), [Sachse, TX](https://openairdocs.org/faa-place/TX/Sachse), built 1992, S/N 7008 ## NTSB investigations (2) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB ERA15WA034](https://openairdocs.org/ntsb/ERA15WA034), Nov 11, 2013: Bombardier CL 600 2B16 (N54VS), Charallave, Venezuela, substantial damage - [NTSB ERA12LA356](https://openairdocs.org/ntsb/ERA12LA356), May 23, 2012: Canadair CL-600-2B16 (N207JB), Hallandale, FL, substantial damage. Probable cause: The failure of the co-pilot to properly close and latch the passenger door before departure, and the flight crew's failure to ensure that the door was secure by using the door warning system.… ## FAA accident and incident reports (5) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20260316010809I](https://openairdocs.org/incident/20260316010809I), Mar 16, 2026: Canadair CL-600-2B19 (N719AV), Ewing, NJ, Minor damage. During landing approach to runway 24 at Trenton-Mercer Airport, at approximately 10-feet AGL, the aircraft encountered a sudden and severe wind disturbance or… - [Incident 20241004014669I](https://openairdocs.org/incident/20241004014669I), Oct 4, 2024: Bombardier Inc CL-600-2B16 (N1DH), Lexington, KY, No damage. A Bombardier challenger 601 departed from cobb county international/mccollum field with five passengers aboard on October 4, 2024. After landing at the… - [Incident 20180520005639I](https://openairdocs.org/incident/20180520005639I), May 20, 2018: Bombardier CL-600-2B16 (N242CK), West Chicago, IL, Minor damage. The 20th of may 2018 at 2033 local time N242CK hit birds while landing on runway 02L at Dupage Airport (kdpa) West Chicago, Illinois. N242CK sustained damage.… - [Accident 20120523011149A](https://openairdocs.org/incident/20120523011149A), May 23, 2012: Canadair Ltd CL-600-2B16 (N207JB), Hallendale, FL, Substantial damage. N207JB departed from opf at 15:45 for a planned 10 minute repositioning flight to its base at pmp. The flight was filed on an IFR flight plan. Two required… - [Incident 20040417014819I](https://openairdocs.org/incident/20040417014819I), Apr 17, 2004: Cndair CL6002B19 (N981CA), Evansville, IN. (-23) Investigated occurrence received via fax from great lakes roc; comair flight number 5311 enroute from Evansville, IN, to atlanta, GA, reported excessive… ## Service difficulty reports (1,372, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR CA190801004](https://openairdocs.org/sdr/CA190801004), Jul 25, 2019: BRAKE DISC. DISINTEGRATED. (CAN) WHEN TECHNICIAN TOW THE A/C INTO THE HANGAR, HE SAW BLACK POWDER ON THE GROUND. THE TECHNICIAN FOUND MAIN WHEEL BRAKE ASSY #3 OUTER STATOR & ROTOR DAMAGED - [SDR SWIA2019071946078](https://openairdocs.org/sdr/SWIA2019071946078), Jul 17, 2019: ENGINE. FAILED. LEFT ENGINE FAILURE DURING CLIMB OUT. DECLARED EMERGENCY, COMPLETED QRH, SHUTDOWN LEFT ENGINE IN FLIGHT. (FLT#3780) FO: 07/19/2019 CLOSED REMOVED AND REPLACED L - [SDR CA190815007](https://openairdocs.org/sdr/CA190815007), Jul 9, 2019: LANDING GEAR. MALFUNCTIONED. (CAN) NOSE GEAR DID NOT RETRACT AFTER SELECTING GEAR UP ON TAKE OFF . NOSE LANDING GEAR DOWN WHEN WHEN GEAR DISAGREE WARNING MESSAGE OCCURRED MSG OCCURRED 28 SE - [SDR CA190620001](https://openairdocs.org/sdr/CA190620001), Jun 15, 2019: AUTOPILOT SYS. FAULTED. (CAN) FLT CREW EXPERIENCED AN UNCOMMANDED YAW MOTION, FULL DEFLECTION NOSE RIGHT WITH AP ON WHILE CRUISING AT MACH 0.74. MAINTENANCE ACTION: PERFORMED OPS TEST - [SDR CA190529003](https://openairdocs.org/sdr/CA190529003), May 25, 2019: DIRECTOR. FAULTED. (CAN) DISPLAY COOL CAUTION MESSAGE. RAN QRH DIDN`T RESOLVE ISSUE ,REMOVED AND REPLACED DISPLAY COOL LOW FLOW EXHAUST SENSOR. (TC# 20190529003) - [SDR CA190527016](https://openairdocs.org/sdr/CA190527016), May 15, 2019: FAIRING. DAMAGED. (CAN) LEFT WINGLET FAIRING DAMAGED DURING FLIGHT DESCENDING THROUGH 14000 FEET. MOST OF THE FAIRING WAS RIPPED OFF IN FLIGHT ALONG WITH THE LIGHTNING PROTECTION - [SDR CA190521026](https://openairdocs.org/sdr/CA190521026), May 13, 2019: SKIN. CRACKED. (CAN) DURING INSPECTION OF THE PASSENGER DOOR INNER SKIN WE HAVE NOTICED 2-OFF CRACKS. (TC# 20190521026) - [SDR CA190522004](https://openairdocs.org/sdr/CA190522004), May 3, 2019: SKIN. CORRODED. (CAN) PAX DOOR INNER SKIN BLENDED TO REMOVE SURFACE CORROSION UNDER CLOSING PLATE REF 601R318059. (TC# 20190522004) - [SDR CA190522001](https://openairdocs.org/sdr/CA190522001), May 2, 2019: TIRE. FAILED. (CAN) ABORTED TAKEOFF AT APPROXIMATELY 90 KTS DUE TO A BURST TIRE. UPON INSPECTION #3 AND #4 MAIN TIRES WERE BURST. NOTHING WAS HIT ON THE RUNWAY DURING THE TAK - [SDR CA190522005](https://openairdocs.org/sdr/CA190522005), May 2, 2019: SKIN. CORRODED. (CAN) PAX DOOR INNER SKIN BLENDED UNDER ACCESS PANEL 832ER (TC# 20190522005) - [SDR CA190522009](https://openairdocs.org/sdr/CA190522009), May 2, 2019: PANEL. CRACKED. (CAN) PAX DOOR AFT SIDE PANEL CORROSION AND CRACK. CORROSION HAS BEEN BLENDED IN SEVERAL AREAS. 1EA AREA IS DOWN TO .028 MIN. REMAINING. MAT. THK. SRM ALLOWS .0 - [SDR CA190425026](https://openairdocs.org/sdr/CA190425026), Apr 20, 2019: FRAME. CORRODED. (CAN) FRAME AT FS319 BLENDED TO REMOVE CORROSION BETWEEN STGR 25L AND 26L. (TC# 20190425026) - [SDR CA190425027](https://openairdocs.org/sdr/CA190425027), Apr 20, 2019: SPLICE STRAP. CORRODED. (CAN) FS333 SPLICE STRAP BLENDED TO REMOVE SURFACE CORROSION BETWEEN STGR 25L AND 26L, FWD AND AFT OF THE FRAME AT FS333. (TC# 20190425027) - [SDR CA190405014](https://openairdocs.org/sdr/CA190405014), Apr 3, 2019: BPSU. FAILED. (CAN) FLAP FAIL ON DEPARTURE, FLAPS AT 0, LEVER AT 0. COMPLIED WITH QRH. REPLACED FLAP BRAKE POSITION SENSOR UNIT (BPSU) (SEE ALSO FAA SDR #2019090100924/SWIA20 - [SDR CA190403010](https://openairdocs.org/sdr/CA190403010), Apr 1, 2019: FLOORBEAM. CORRODED. (CAN) 1-OFF CORROSION DAMAGE TO FLOOR BEAM OUTBOARD FLANGE DIMENSIONS POST BLEND OUT ARE AS FOLLOWS: 0 1.625`L X 1.090`W X 0.035` MIN. REMAINING THK (0.060` NOM - [SDR CA190322012](https://openairdocs.org/sdr/CA190322012), Mar 13, 2019: INTERCOSTAL. CORRODED. (CAN) OPERATOR REPORTS CORROSION DAMAGE TO PAX DOOR INTERCOSTAL (TC# 20190322012) - [SDR CA190227008](https://openairdocs.org/sdr/CA190227008), Feb 21, 2019: PRESSURE SWITCH. FAILED. (CAN) RIGHT WING ANTI ICE CAUTION MESSAGE ON CLIMB OUT (SEE ALSO FAA SDR #2019081703527/SWIA2019022145537) (TC# 20190227008) - [SDR CA190225008](https://openairdocs.org/sdr/CA190225008), Feb 19, 2019: WINDSHIELD. CRACKED. (CAN) UPON DESCENT, WINDSHIELD CRACKED (TC# 20190225008) - [SDR CA190220017](https://openairdocs.org/sdr/CA190220017), Feb 15, 2019: STATOR VANE. WORN. (CAN) ENGINE ASSY P/N 6078T7G01, WAS INSTALLED. AT 12054 :22 ENGINE HOURS, 11860 CYCLES, AS A PREVENTIVE ACTION, A SPECIAL DETAILED INSPECTION OF COMPRESSOR VAR - [SDR CA180404014](https://openairdocs.org/sdr/CA180404014), Apr 1, 2018: GEARBOX. DAMAGED. (CAN) AIR TURNBACK, N1, N2 AND ITT FLUCTUATION ON CLIMB OUT. CORRECTIVE ACTION: REMOVED AND REPLACED RT THROTTLE GEAR BOX. PERFORMED IDLE SPEED CHECK. PERFORMED - [SDR SWIA201642426](https://openairdocs.org/sdr/SWIA201642426), Aug 7, 2016: ENGINE. FAILED. DURING APP BASE LEG RIGHT ENGINE N1 FLUCTUATED AND NOTABLE A/C ENGINE VIBRATION @ 58 N1. VIBRATION STOPPED. DECLARED EMERGENCY WITH ATC. ON TAXI IN ENG TEMP WEN - [SDR SWIA201641901](https://openairdocs.org/sdr/SWIA201641901), Feb 19, 2016: ENGINE. FLAMED OUT. NR 2 ENGINE FLAMED OUT AFTER TAKEOFF. ATTEMPTED TO RELIGHT ENGINE, UNSUCCESSFUL. CREW DECLARED AN EMERGENCY AND DIVERTED. CABIN WAS BRACED AND THE ACFT LANDED S - [SDR VNAA2016021900022](https://openairdocs.org/sdr/VNAA2016021900022), Feb 19, 2016: CARBON SEAL. LEAKING. CREW REPORTED RECEIVING A RT ENGINE OIL PRESSURE MESSAGE DURING CRUISE AT FL310. THE CREW DECLARED AN EMERGENCY, DIVERTED TO NEAREST FIELD AND LANDED WITHOUT FU - [SDR VNAA2016021900023](https://openairdocs.org/sdr/VNAA2016021900023), Feb 19, 2016: CARBON SEAL. LEAKING. CREW REPORTED RECEIVING A RT ENGINE OIL PRESSURE MESSAGE DURING CRUISE AT FL310. THE CREW DECLARED AN EMERGENCY, DIVERTED TO NEAREST FIELD AND LANDED WITHOUT FU - [SDR CA160126009](https://openairdocs.org/sdr/CA160126009), Jan 24, 2016: SKIN. CRACKED. (CAN) LEFT WING LOWER PLANK 601R10045-11 DRAIN HOLE AT WS 85.5 BETWEEN S-14 AND S-15 HAS TWO (2) EACH CRACKS. THE FORWARD CRACK EMANATES FROM THE EDGE OF THE DR - [SDR CA160120016](https://openairdocs.org/sdr/CA160120016), Jan 18, 2016: INDICATOR. MALFUNCTIONED. (CAN) DURING APPROACH GGN7336 CREW REPORTED FLAPS FAILURE TO ATC. WEATHER AT THE TIME INCLUDED LIGHT SNOW SHOWERS. CREW ELECTED TO CONTINUE TO DESTINATION AND P - [SDR CA160121013](https://openairdocs.org/sdr/CA160121013), Jan 18, 2016: FLAP SYSTEM. FAILED. (CAN) FLAPS FAIL AT 2 DURING APPROACH, QRM ACTIONED, MOC ADVISED. CARRIED OUT RESET OF FLAP SKEW DETECTION SYSTEM CARRIED OUT. LUBRICATION CARRIED OUT. OPERATIO - [SDR CA160121014](https://openairdocs.org/sdr/CA160121014), Jan 18, 2016: FLAP SYSTEM. WARNING MESSAGE. (CAN) FLAP FAIL MESSAGE ON LANDING, FLAP 0 LANDING CONDUCTED AS PER QRM CARRIED OUT LUBRICATION CARRIED OUT REMOVAL OF FLEX DRIVE SHAFTS CARRIED OUT LUBRICATION - [SDR CA151221009](https://openairdocs.org/sdr/CA151221009), Dec 21, 2015: CONTROL LEVER. CORRODED. (CAN) ELEVATOR JAM DUE TO CORRODED ELEVATOR CONTROL LEVERS. SOME OF THE MOVING PARTS IN THIS MECHANISM WERE FOUND STUCK DUE TO CORROSION AND THE ELEVATOR COULD - [SDR CA151123008](https://openairdocs.org/sdr/CA151123008), Nov 23, 2015: ROTOR. FAILED. (CAN) AFTER LANDING, THE PILOT REPORTED RT INBD BRAKE JAM DURING TAXI. THE TECH FOUND 1 OF THE BRAKE ROTORS DESTROYED. THE UNIT WAS INSTALLED LAST WEEK AND OPER - [SDR CA151113003](https://openairdocs.org/sdr/CA151113003), Nov 11, 2015: HARNESS. DAMAGED. (CAN) ON TAKEOFF ROLL F/O HAD NO DIRECTIONAL CONTROL, ABORTED TO, THE TERM NO DIRECTIONAL CONTROL MEANT THEY LOST NOSE WHEEL STEERING. REPLACED THE NOSE WHEEL S - [SDR CA151026002](https://openairdocs.org/sdr/CA151026002), Oct 22, 2015: SHIELD. WORN. (CAN) ON INVESTIGATION OF THE DOOR LOCKING SYS CAUTION MESSAGE ON THE EICAS, IT WAS NOTED THAT THE HINGE SHIELDS ON THE RAILING WERE NOT STAYING INSIDE THE RAIL - [SDR CA150916012](https://openairdocs.org/sdr/CA150916012), Sep 15, 2015: FITTING. CRACKED. (CAN) COCKPIT WINDSHIELD CENTER POST LT LOWER FITTING CRACK DAMAGE. - [SDR CA150908007](https://openairdocs.org/sdr/CA150908007), Sep 3, 2015: SKIN. CRACKED. (CAN) RT LOWER WING PLANK IS CRACKED AT WS148.019 AFT EDGE. CRACK WAS DISCOVERED WHILE PERFORMING S/B 601R-57-031 FOR THE INSPECTION OF THE LOWER WING PLANKS IN - [SDR CA150809002](https://openairdocs.org/sdr/CA150809002), Aug 6, 2015: PRIORITY VALVE. FAILED. (CAN) AFTER T/O NOSE GEAR WOULD NOT COME UP. RECEIVED A GEAR DISAGREE WARNING MSG THEN NOSE GEAR RETRACTED ON ITS OWN AFTER A FEW MORE SECONDS. - [SDR CA150730013](https://openairdocs.org/sdr/CA150730013), Jul 29, 2015: TIRE. SEPARATED. (CAN) AFTER LANDING, FLIGHT CREW DURING WALK AROUND INSPECTION NOTICED THAT NR 3 TIRE WAS MISSING A STRIP OF RUBBER, APPROXIMATELY 18" LONG X 4" WIDE. TIRE PRES - [SDR CA150728009](https://openairdocs.org/sdr/CA150728009), Jul 24, 2015: SELECTOR VALVE. FAILED. (CAN) ON LANDING APPROACH COMING INTO THE AIRPORT, UPON LANDING GEAR SELECTED DOWN IT WAS INDICATED THAT THERE WAS A PROBLEM WITH THE NOSE GEAR. THE PILOTS FLEW - [SDR CA150724002](https://openairdocs.org/sdr/CA150724002), Jul 20, 2015: HANDLE. FAILED. (CAN) AFTER MLG SYSTEM COMPONENT REPLACEMENT, ROUTINE GEAR SWINGS WERE CARRIED OUT ON AIRCRAFT. DURING ALTERNATE EXTENSION FUNCTION TEST, IT WAS DISCOVERED THAT - [SDR CA150713017](https://openairdocs.org/sdr/CA150713017), Jul 2, 2015: ACTUATOR. FAILED. (CAN) ON APPROACH GEAR DISAGREE W, UPON LG EXTENSION SELECTION WITH RT MLG UNLOCKED INDICATION. LG RECYCLED & ALL DOWN LOCKED INDICATIONS OK. REPLACED RT MLG SI - [SDR CA150602017](https://openairdocs.org/sdr/CA150602017), May 31, 2015: QUICK DISCONNECT. DISCONNECTED. (CAN) DURING LANDING GEAR RETRACTION FOLLOWING MESSAGES APPEARED: NOSE DOOR OPEN GEAR DISAGREE WOW INPUT CAUTION MSG WOW OUTPUT FAIL THE CAPTAIN MADE THE EMERGE - [SDR CA150519027](https://openairdocs.org/sdr/CA150519027), May 16, 2015: DISK. DISINTEGRATED. (CAN) UPON LANDING, 2 ROTATING DISKS OF NR 4 BRAKE ASSEMBLY HAVE DISINTEGRATED INTO FRAGMENTS. MAINTENANCE PERSONEL REPLACED THE ASSY TO CORRECT THE SITUATION A - [SDR CA150312002](https://openairdocs.org/sdr/CA150312002), Mar 12, 2015: LINE. WORN. (CAN) DURING INSPECTION, FULE LINES IN THE LT WING TANK AT BS, LBL 22.50 DAMAGE TO PIPE ASSY AND RIB SUPPORT STRUCTURE WAS FOUND. WHILE IN AN UNLOADED CONDITION - [SDR CA150112010](https://openairdocs.org/sdr/CA150112010), Jan 7, 2015: TRANSMITTER. FAILED. (CAN) IAS HI SPEED Q POPPED OUT AND THE ACFT STARTED TO CLIMB. FLAPS WERE MOVING UNCOMMANDED WITH FLAP HANDLE AT 0,FROM 0-2,0-8, 0-20. HYD 2B AND 3B CAUTION MSG - [SDR CA141215012](https://openairdocs.org/sdr/CA141215012), Nov 28, 2014: WIRE. CHAFED. (CAN) AFTER TOUCHDOWN, THE RIGHT THRUST REVERSER DEPLOYED WHEN COMMANDED BUT THE CREW WAS UNABLE TO STOW IT. ON THE SAME TIME, NO LIGHTS WERE SHOWN ON T/R CONTR - [SDR CA141008018](https://openairdocs.org/sdr/CA141008018), Oct 4, 2014: THROTTLE CABLE. BROKEN. (CAN) LOSS OF CONTROL OF LEFT THROTTLE ON CLIMB OUT. MAINTENANCE FOUND LEFT THROTTLE CABLE TO THROTTLE GEAR BOX BROKEN. - [SDR VNAA2014083000019](https://openairdocs.org/sdr/VNAA2014083000019), Aug 30, 2014: SKIN. DENTED. DURING SCHEDULED MAINTENANCE, THE RT ENGINE TRANSLATING COWL HAD TWO DENTS. REPAIRED IAW AMM. ACFT WAS RELEASED FOR SERVICE. - [SDR CA140821003](https://openairdocs.org/sdr/CA140821003), Aug 19, 2014: PROXIMITY SWITCH. FAILED. (CAN) AT TAKEOFF, CREW SELECTED GEAR UP. THE MAIN GEAR RETRACTED AS NORMAL BUT THE NOSE GEAR FAILED TO RETRACT. INDICATIONS SHOWED NOSE GEAR STILL DOWN AND LOCK - [SDR CA160219006](https://openairdocs.org/sdr/CA160219006), Jul 29, 2014: FLOOR SKIN. CRACKED. (CAN) FOUND CRACKS LOCATED ON PRESSURE FLOOR STRUCTURE BS 461.5 BETWEEN RBL 9 AND LBL 9 - [SDR SWIA2014062338265](https://openairdocs.org/sdr/SWIA2014062338265), Jun 21, 2014: BUSHING. GALLED. LEFT ENGINE, YOKE MOUNT LINK BUSHINGS ARE GALLED. R & R LT ENGINE YOKE LINK IAW AMM. - [SDR SWIA2014062338266](https://openairdocs.org/sdr/SWIA2014062338266), Jun 21, 2014: PIN. SCORED. LEFT ENGINE, YOKE MOUNT PINS AND BOLTS SCORED. R & R LT ENGINE FWD YOKE MOUNT PINS AND BOLTS IAW AMM. All 1,372: https://openairdocs.org/engine/ge-cf34-3a1/reports.md ## STCs that may be installed (OpenAirDocs) (1) Approved for this engine model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has. - [STC SE01271LA](https://openairdocs.org/stc/SE01271LA): Installation of anti-ice shut-off/regulator valve p/n 5399-00-1. Dukes Inc --- 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.