# GE CF34-3A

- Type: Engine model (FAA registry)
- Registry code: 30066
- Manufacturer (registry): GE
- Model: CF34-3A
- 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-cf34-3a

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
- [AD 88-06-07](https://openairdocs.org/ad/88-06-07): Fuel Controls · General Electric Aircraft Engines CF34-1A and CF34-3A. Effective Mar 23, 1988

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 (15)

- [N253LA](https://openairdocs.org/aircraft/N253LA): [One World Aviation 253 LLC](https://openairdocs.org/faa-owner/ONE%20WORLD%20AVIATION%20253%20LLC), [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta), S/N 5037
- [N304CT](https://openairdocs.org/aircraft/N304CT): [Adams Aviation Services Inc Trustee](https://openairdocs.org/faa-owner/ADAMS%20AVIATION%20SERVICES%20INC%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 1985, S/N 3044
- [N411JE](https://openairdocs.org/aircraft/N411JE): [Aviation Trust Company LLC Trustee](https://openairdocs.org/faa-owner/AVIATION%20TRUST%20COMPANY%20LLC%20TRUSTEE), [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City), built 1987, S/N 5011
- [N444SE](https://openairdocs.org/aircraft/N444SE): [Encore Enterprises Inc](https://openairdocs.org/faa-owner/ENCORE%20ENTERPRISES%20INC), [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas), built 1987, S/N 5008
- [N480LA](https://openairdocs.org/aircraft/N480LA): [Luxury Aero Collection LLC](https://openairdocs.org/faa-owner/LUXURY%20AERO%20COLLECTION%20LLC), [Scottsdale, AZ](https://openairdocs.org/faa-place/AZ/Scottsdale), built 1983, S/N 3003
- [N54ES](https://openairdocs.org/aircraft/N54ES): [Bank Of Utah Owner Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20OWNER%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 1987, S/N 5010
- [N551SD](https://openairdocs.org/aircraft/N551SD): [Pollard Spares LLC](https://openairdocs.org/faa-owner/POLLARD%20SPARES%20LLC), [Fort Worth, TX](https://openairdocs.org/faa-place/TX/Fort%20Worth), built 1987, S/N 5016
- [N601RC](https://openairdocs.org/aircraft/N601RC): [Raytheon Co](https://openairdocs.org/faa-owner/RAYTHEON%20CO), [Tucson, AZ](https://openairdocs.org/faa-place/AZ/Tucson), built 1986, S/N 3055
- [N618RR](https://openairdocs.org/aircraft/N618RR): [Fat Boy Leasing LLC](https://openairdocs.org/faa-owner/FAT%20BOY%20LEASING%20LLC), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 1988, S/N 5022
- [N715AV](https://openairdocs.org/aircraft/N715AV): [Lead And Steel 3 LLC](https://openairdocs.org/faa-owner/LEAD%20AND%20STEEL%203%20LLC), [Fountain Valley, CA](https://openairdocs.org/faa-place/CA/Fountain%20Valley), built 1996, S/N 7158
- [N747NJ](https://openairdocs.org/aircraft/N747NJ): [Challenger 601 Msn 5123 LLC](https://openairdocs.org/faa-owner/CHALLENGER%20601%20MSN%205123%20LLC), [Kansas City, MO](https://openairdocs.org/faa-place/MO/Kansas%20City), S/N 5123
- [N807MM](https://openairdocs.org/aircraft/N807MM): [Pollard Spares LLC](https://openairdocs.org/faa-owner/POLLARD%20SPARES%20LLC), [Fort Worth, TX](https://openairdocs.org/faa-place/TX/Fort%20Worth), built 1983, S/N 3014
- [N824DH](https://openairdocs.org/aircraft/N824DH): [Pollard Spares LLC](https://openairdocs.org/faa-owner/POLLARD%20SPARES%20LLC), [Roanoke, TX](https://openairdocs.org/faa-place/TX/Roanoke), built 1985, S/N 3047
- [N881BG](https://openairdocs.org/aircraft/N881BG): [Etosha LLC](https://openairdocs.org/faa-owner/ETOSHA%20LLC), [Weston, FL](https://openairdocs.org/faa-place/FL/Weston), built 1991, S/N 5097
- [N951RM](https://openairdocs.org/aircraft/N951RM): [Siilats Keith](https://openairdocs.org/faa-owner/SIILATS%20KEITH), [New York, NY](https://openairdocs.org/faa-place/NY/New%20York), S/N 3042

## NTSB investigations

None matched to aircraft with this engine model.

## FAA accident and incident reports (1)

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 20260517004909I](https://openairdocs.org/incident/20260517004909I), May 17, 2026: Canadair CL-600-2B19 (N715AV), Richmond, VA, No damage. While enroute from erie international airport (eri) to lynden pindling international airport (nas) at flight level 310, the left engine N1 and N2 indications…

## Service difficulty reports (174, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR 2021FA0000132](https://openairdocs.org/sdr/2021FA0000132), Feb 19, 2021: FLAP TRACK. BINDING. FAILURE OF THE FLAPS AT 10 DEGREES. CORRECTIVE ACTION WAS LUBRICATION OF THE FLAP ACTUATORS IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUALS FOLLOWED BY AN OPE
- [SDR CA190416014](https://openairdocs.org/sdr/CA190416014), Apr 8, 2019: ACTUATOR. FAILED. (CAN) AOG DUE TO HSTA FAILURE PREVIOUSLY INSTALLED HSTA HAS BEEN A NFF. (TC# 20190416014)
- [SDR WWQA20180213001](https://openairdocs.org/sdr/WWQA20180213001), Jan 29, 2018: CARBON SEAL. LEAKING. WITH PACKS SELECTED OFF AND APU BLEED AIR SELECTED ON, STARTED THE RT ENGINE. NOTICED SMOKE COMING OUT OF FORWARD AIR CONDITIONING VENTS IN COCKPIT. STARTED THE
- [SDR MXIA2016051800001](https://openairdocs.org/sdr/MXIA2016051800001), May 18, 2016: HINGE. CRACKED. DURING A SCHEDULED NDI INSPECTION OF THE CABIN DOOR HINGE A CRACK WAS DETECTED ON 1 OF THE LOBES OF THE DOOR SIDE HINGE HALF. EDDY CURRENT METHOD OF NDI WAS USE
- [SDR 2016FA0000247](https://openairdocs.org/sdr/2016FA0000247), May 17, 2016: TIRE. FAILED. RIGHT MAIN INBD TIRE HAS A PORTION OF THE TREAD THAT SEPARATED ON LANDING. NEW TIRE WAS INSTALLED AT WHEEL ASSY O/H.
- [SDR CA160311002](https://openairdocs.org/sdr/CA160311002), Mar 10, 2016: LEVER. STUCK. (CAN) DURING OPERATIONAL CHECKS OF LANDING GEAR SYSTEM GEAR SWINGS, THE EMERGENCY SYSTEM HAS BEEN ACTIVATED. THE GEAR EXTENDED WITH OUT ANY ISSUES. FOLLOWING ST
- [SDR CA150327002](https://openairdocs.org/sdr/CA150327002), Mar 18, 2015: SCREW. BROKEN. (CAN) LT ACME SCREW ADJUSTING FOUND BROKEN FOLLOWING PILOT REPORT.
- [SDR CA150108002](https://openairdocs.org/sdr/CA150108002), Dec 27, 2014: ENGINE. SHUTDOWN. (CAN) CUSTOMER REPORTS THE LEFT ENGINE SHUT DOWN UN-COMMANDED. THE AIRCRAFT WAS ON DESCENT. THE PILOTS THINK THEY HAD A COMPRESSOR STALL. THE LEFT ENGINE SHUTDO
- [SDR LOMA2015F00009](https://openairdocs.org/sdr/LOMA2015F00009), Nov 18, 2014: SHUTOFF VALVE. LEAKING. RIGHT 10TH STAGE BLEED AIR WARNING ILLUMINATED. DIVERTED FOR REPAIR. REPLACED 10TH AND 14TH STAGE BLEED AIR SHUTOFF VALVES.
- [SDR CA141114001](https://openairdocs.org/sdr/CA141114001), Nov 11, 2014: LANDING GEAR. FAILED. (CAN) AT APPROX. 5 MILES FINAL RUNWAY 16, AN EXECAIRE CANADAIR CL600-2B16 REPORTED A POSSIBLE NOSE GEAR PROBLEM. DID A FLY BY AND NOSE GEAR WAS NOT OBSERVED TO 
- [SDR CA140606002](https://openairdocs.org/sdr/CA140606002), Jun 5, 2014: CONTROL CABLE. FAILED. (CAN) DURING AN 60 MONTH INSPECTION. THE TECH FOUND BY VISUAL CHECK UP, WHEN HE OPEN THE PANEL IN THE VERTICAL STABILIZER RT SIDE.
- [SDR CA140408007](https://openairdocs.org/sdr/CA140408007), Apr 8, 2014: SWITCH. MALFUNCTIONED. (CAN) DURING A MAINTENANCE INSPECTION OF THE AIR CONDITION OVERHEAT SWICHES ON BOTH ACU FAIL THE TEST, FOUND INOPERATIVE, DURING THE FUNCTIONAL TEST AS REQUIRED
- [SDR KW3R2014032617085](https://openairdocs.org/sdr/KW3R2014032617085), Mar 26, 2014: WINDSHIELD. CRACKED. DURING APPROACH, LT WINDSHIELD CRACKED, CREW PERFORMED ABNORMAL PROCEDURES AND LANDED WITH NO FUTHER PROBLEMS.
- [SDR CA130626005](https://openairdocs.org/sdr/CA130626005), Jun 25, 2013: WIRE. FAILED. (CAN) DURING A PREFLIGHT CHECK THE PILOT COULD NOT OPERATE THE PITCH TRIM AND FOUND THE BREAKER CHANNEL NR 2 POP OUT. AFTER THE INVESTIGATION BY THE AME HE FOUN
- [SDR CA130610014](https://openairdocs.org/sdr/CA130610014), Jun 6, 2013: SELECTOR VALVE. FAILED. (CAN) ON DEPARTURE WHEN THE LANDING GEAR WAS SELECTED TO THE UP POSITION THE NOSE GEAR WOULD NOT RETRACT, A FERRY FLIGHT PERMIT WAS ISSUED TO FACILITATE POSITIO
- [SDR CA130528010](https://openairdocs.org/sdr/CA130528010), May 18, 2013: CONTROL HANDLE. FAILED. (CAN) DURING TAKE-OFF THE GEAR HANDLE WAS SELECTED TO THE UP POSITION. THE MAIN LANDING GEAR RETRACTED AND INDICATED AS BEING RETRACTED HOWEVER, THE NOSE LANDIN
- [SDR CA120529001](https://openairdocs.org/sdr/CA120529001), May 23, 2012: DOOR. SEPARATED. (CAN) PASSAGER DOOR DEPARTED IN FLIGHT. INVESTIGATION TEAM HAS RETURNED FROM THE ACCIDENT SITE. THE ACFT DAMAGE AND GOLF COURSE, WHERE THE PASSENGER DOOR LANDED
- [SDR CA120405004](https://openairdocs.org/sdr/CA120405004), Apr 4, 2012: FUEL CONTROL. MALFUNCTIONED. (CAN) DURING DESCENT, BOTH THRUST LEVERS WERE RETARDED TO IDLE. THE RT ENGINE FLAMEDOUT. THE CREW ELECTED TO CONTINUE WITH THE APPROACH SINGLE ENGINE. THE CUSTO
- [SDR CA120321004](https://openairdocs.org/sdr/CA120321004), Mar 19, 2012: ACTUATOR. FAILED. (CAN) AFTER TAKE OFF THE FLAP FAIL AT 20 DEGREES DOWN, THE AIPLANE FLEW TO DESTINATION WITH THE FLAPS AT 20 DEGREES AND LANDED WITHOUT INCIDENT.
- [SDR CA120127001](https://openairdocs.org/sdr/CA120127001), Jan 23, 2012: WINDOW. CRACKED. (CAN) IN CRUISE THE PILIOT SUDDENLY SEE THAT THE LT SIDE WIDOW CRACKED, WENT FROM 24,000 TO 13,000 WITHOUT PANIC SLOWLY TO MAKE SURE THAT THE WINDOW DOESN`T BRE
- [SDR CA120104009](https://openairdocs.org/sdr/CA120104009), Jan 4, 2012: LINE. LEAKING. (CAN) HYDRAULIC NR 3 LOSS CAUSING AN EMERGENCY GEAR EXTENSION. THE HYDRAULIC LEAK WAS LOCATED ON ACMP 3 A HOSE PUMP PRESS LINE.
- [SDR CA110328003](https://openairdocs.org/sdr/CA110328003), Mar 27, 2011: STRUT. BINDING. (CAN) DURING AN APPROACH IN CYUY MARCH 27 2011 ,THE NLG REFUSE TO DESCENT .THEY DID THE EMERGENCY LANDING GEAR PROCEDURE AND IT DIDN`T WORK.THEY HAD IN THE COCK
- [SDR CA110112009](https://openairdocs.org/sdr/CA110112009), Dec 17, 2010: SUPPORT BEAM. CRACKED. THIS SDR SHOULD HAVE BEEN ISSUED IN JULY 2010 WHEN DISCOVERED. MISTAKENLY OMITTED. DURING EXCHANGE OF AN APU, THE TECHNICIAN NOTICE A CRACK ON THE UPPER WEB, AF
- [SDR 2010FA0000201](https://openairdocs.org/sdr/2010FA0000201), Feb 5, 2010: FRAME. CRACKED. FWD FUSELAGE FRAME AT FS235 ABOVE FLOOR, PILOTS AND COPILOTS SIDE, FOUND CRACKED. DURING 240 MONTH INSP.
- [SDR CA091216003](https://openairdocs.org/sdr/CA091216003), Nov 9, 2009: FUEL CONTROL. MALFUNCTIONED. (CAN) THE ENGINE WAS IN FLIGHT AT 9000 FT WHEN A REQUEST WAS MADE TO AIR TRAFFIC TO INCREASE TO NEXT ALTITUDE. AFTER THE REQUEST WAS GRANTED, THE PILOT ADVANCED
- [SDR CA090529001](https://openairdocs.org/sdr/CA090529001), May 24, 2009: CABLE. WORN. (CAN) DURING APPROACH THE CREW EXPERIENCED MULTIPLE COMPRESSOR STALLS ON THE LT ENG. THEY CARRIED OUT THE APPROACH WITH THAT ENGINE AT IDLE. AT ONE POINT, THE I
- [SDR CA090525006](https://openairdocs.org/sdr/CA090525006), Feb 26, 2009: COWLING. DEPARTED. (CAN) OPERATOR REPORTED THE FOLLOWING TO MFG: DURING A PASSENGER FLIGHT THE LT UPPER ENGINE COWL ACCESS PANEL (PN 228-50080-801) DEPARTED THE ACFT DURING FLIGHT
- [SDR 2008FA0000358](https://openairdocs.org/sdr/2008FA0000358), May 19, 2008: CONTROL BOX. FAILED. CREW REPORTED FLAP FAILURE DURING APPROACH APPROXIMATELY 8 HOURS AFTER INSTALLATION. RESET SYSTEM AND FLAPS WORKED FINE. FLEW AIRCRAFT HOME AND NO DISCREPANCIES
- [SDR CA070403005](https://openairdocs.org/sdr/CA070403005), Mar 31, 2007: WATER HEATER. ODOR. (CAN) WHILE EN ROUTE, A BURNING ODOR WAS NOTICED BY THE CREW AND PASSENGERS. NO SMOKE WAS APPARENT IN THE CABIN OR COCKPIT. THEN SEARCHED THE LAVATORY AND BAGGA
- [SDR 2007FA0000298](https://openairdocs.org/sdr/2007FA0000298), Mar 20, 2007: INVERTER. SHORTED. WHEN TURNING MAIN BATTERY SWITCHES ON, MECHANIC HEARD A LOUD POPPING SOUND, FOLLOWED BY THE AROMA OF SMOKE IN THE ENTRANCE AREA OF THE AIRCRAFT. THE FLOORBOARD 
- [SDR CA070125001](https://openairdocs.org/sdr/CA070125001), Jan 25, 2007: ACTUATOR. INOPERATIVE. (CAN) RT MAIN LANDING GEAR UNLOCK INDICATION APPROX. 15 - 20 MIN. AFTER ARRIVAL, NO PUMP, NO GEAR COMMAND, LOCK PARTIALLY MOVED TO UNLOCK POSITION. RETRACTING A
- [SDR CA061227006](https://openairdocs.org/sdr/CA061227006), Dec 27, 2006: WINDSHIELD. BROKEN. (CAN) RT WINDSHIELD FACE PLY BROKEN IN FLIGHT. APPROX. 7000 INCH ON APPROACH. FOD INSPECTION CARRIED OUT ON ENGINE INTAKE AND WINDSHIELD REPLACED. A/C HOURS; 68
- [SDR CA061218015](https://openairdocs.org/sdr/CA061218015), Dec 18, 2006: PUMP. DAMAGED. (CAN) LOST OF NR 3 SYSTEM HYDRAULIC FLUID IN FLIGHT. THE NR 3B PUMP HAS FAILED ON FLANGE GASKET. THE PUMP HAS BEEN REPLACED AND A\C RETURNED TO SERVICE. A/C HOU
- [SDR CA061208001](https://openairdocs.org/sdr/CA061208001), Dec 6, 2006: ACTUATOR. CRACKED. (CAN) DURING SCHEDULE LUBRICATION OF THE FLAP ACTUATORS, THE TECHNICIAN NOTICED GREASE WAS OOZING OUT OF A CRACKED WELD ON THE HOUSING OF THE LT OB FLAP ACTUATO
- [SDR CA061116003](https://openairdocs.org/sdr/CA061116003), Nov 16, 2006: BULKHEAD. CRACKED. (CAN) BULKHEAD STRUCTURE AT STATION 559.00 CRACKED ON TWO AILERON MIXER (P/N 600-91154-5) ATTACHMENTS BOLTS. A/C HOURS:25688 A/C CYCLES:30488
- [SDR CA061103011](https://openairdocs.org/sdr/CA061103011), Nov 2, 2006: CONTROL UNIT. FAILED. (CAN) DURING TAKE OFF FLAP FAIL DURING FLAP RETRACTION, A/C RETURN TO TERMINAL .BREAKER RESET AS PER OPERATING MANUAL NR 1 ABNORMAL PROCEDURE SECTION 10 P 3-4. 
- [SDR CA061010005](https://openairdocs.org/sdr/CA061010005), Oct 9, 2006: FLAP SYSTEM. MALFUNCTIONED. (CAN) FLAP FAIL BETWEEN 20 DEGREES TO 0 DEGREE DURING RETRACTION OF THE FLAPS AT TAKEOFF , FLAPS RESET ON GROUND IAW OPERATING MANUAL NR 1 ABNORMAL PROCEDURE SE
- [SDR CA060918001](https://openairdocs.org/sdr/CA060918001), Sep 18, 2006: FLAP SYSTEM. MALFUNCTIONED. (CAN) FLAP FAILED ON TAKEOFF, A/C RETURNED AND LANDED SAFELY AT QB MAIN BASE, BREAKER WAS RESET IAW OPERATING MANUAL, COULDN`T DUPLICATED THE SNAG. A/C DID ONE 
- [SDR CA060828001](https://openairdocs.org/sdr/CA060828001), Aug 28, 2006: PUMP. BROKEN. (CAN) LT MAIN AND SCAVENGE EJECTOR FAILURE (MOTIVE FLOW FAILURE). FUEL PUMP SHAFT FOUND BROKEN. FUEL PUMP REPLACED AND AIRCRAFT RETURNED TO SERVICE. A/C HOURS; 
- [SDR CA060712003](https://openairdocs.org/sdr/CA060712003), Jul 2, 2006: FEEDER CABLE. ARCED. (CAN) RT GEN TRIPPED OFFLINE DURING APPROACH. GEN OFF ANNUNCIATOR CAME ON, PWR AUTO TRANSFERED FROM GEN 1. NO LOSS OF PWR ON ANY AC BUSES. AC FERRIED WITH GENER
- [SDR CA060428002](https://openairdocs.org/sdr/CA060428002), Apr 28, 2006: TRANSFORMER. INOPERATIVE. (CAN) LOSS OF NR 1 MASI, NR 1 ALTIMETER, FDR, NR 1 ADI PITCH AND ROLL INFO, COMPASS INFO, NR 1 ESSENTIAL BUS AND LOSS 26 VAC. CAUSE OF FAULT FOUND TO BE BROKEN 
- [SDR DJFA2005143](https://openairdocs.org/sdr/DJFA2005143), Sep 26, 2005: ENGINE. OVERSERVICED. KAPA - KSMO - WHILE CLIMBING THROUGH 15,000 FEET, THE NR 2 ENGINE OIL TEMPERATURE BEGAN TO RISE INTO THE AMBER BAND. WHEN POWER WAS REDUCED THE OIL TEMPERATURE 
- [SDR CA050920004](https://openairdocs.org/sdr/CA050920004), Sep 13, 2005: WIRE. OVERHEATED. (CAN) POST FLIGHT INSPECTION REVEALED EVIDENCE OF OVERHEAT CONDITION FOUND AT 6 O'CLOCK POSITION AT THE COMBUSTOR SECTION FWD FRAME WHEN COWLINGS OPENED TO INVE
- [SDR UG82005F00006](https://openairdocs.org/sdr/UG82005F00006), Aug 15, 2005: WARNING LIGHT. ILLUMINATED. (REF CNTRL NR PA05003) THERE WAS NOT GREEN (DOWN AND LOCKED) INDICATION ON THE NOSE GEAR. THERE WAS ALSO NO RED (UNSAFE) INDICATION. THE CREW WENT THROUGH THE R
- [SDR UG82005F00010](https://openairdocs.org/sdr/UG82005F00010), Aug 15, 2005: INDICATOR. DEFECTIVE. ( REF: PA 05-003) THERE WAS NO GREEN DOWN AND LOCKED INDICATION ON THE NOSE GEAR. THERE WAS ALSO NO RED UNSAFE INDICATION. THE CREW WENT THROUGH THE REQUIRED CH
- [SDR 2005FA0001071](https://openairdocs.org/sdr/2005FA0001071), Jun 19, 2005: TIRE. SEPARATED. (REF: PA05002) VIBRATION NOTED AT ROTATION SPEED. FLIGHT CREW RETURNED TO POINT OF ORIGIN AND LANDED UNEVENTFULLY. NR 4 TIRE TREAD SEPARATED. THE NR 4 MAIN WHEE
- [SDR CA050324002](https://openairdocs.org/sdr/CA050324002), Jan 2, 2005: SENSOR. INOPERATIVE. (CAN) ON JANUARY 02, 2005, AFTER TAKE OFF THE LANDING GEAR WERE SELECTED UP (RETRACT). LANDING GEAR REMAINED ON EXTENDED POSITION. AIRCRAFT RETURNED TO DEPARTUR
- [SDR CA041223003](https://openairdocs.org/sdr/CA041223003), Dec 23, 2004: ENGINE. MALFUNCTIONED. (CAN) UNCOMMANDDED ACCELERATION ON THE LT ENGINE ON TAKE OFF AROUND + 7 PERCENT ABOVE RETURN TO NORMAL 40 SECONDS LATER.
- [SDR DJFA2004032](https://openairdocs.org/sdr/DJFA2004032), Nov 12, 2004: ENGINE. MALFUNCTIONED. CREW REPORTED, THAT DURING CLIMB WHILE EN ROUTE FROM KBRO TO KATL CLIMB POWER WAS NOT ACHIEVED. THE NR 1 ENGINE POWER WAS 2 PERCENT LOWER THAN REQUIRED. AIRCRAF
- [SDR ASOA04576](https://openairdocs.org/sdr/ASOA04576), Aug 8, 2004: SCAVENGE PUMP. CLOGGED. DURING CRUISE FROM AEX-DFW, AT APPROXIMATELY 22,000 FT WHILE FERRYING THE AIRCRAFT TO DFW THE CREW RECEIVED A RT ENGINE OIL PRESSURE WARNING. THE QRH WAS COMPLI

All 174: https://openairdocs.org/engine/ge-cf34-3a/reports.md

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