# GE CF-34-1A

- Type: Engine model (FAA registry)
- Registry code: 30033
- Manufacturer (registry): GE
- Model: CF-34-1A
- Engine type: Turbo-fan
- Power: 9,140 lb thrust
- Data sheet: [TCDS E15NE](https://openairdocs.org/tcds/E15NE) (OpenAirDocs)
- Holder: General Electric Company GE Aerospace
- Installed in: 13 registered aircraft
- Page: https://openairdocs.org/engine/ge-cf-34-1a

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 (13)

- [N113SR](https://openairdocs.org/aircraft/N113SR): [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 1994, S/N 5164
- [N275MT](https://openairdocs.org/aircraft/N275MT): [Aerotrust Services Corp Trustee](https://openairdocs.org/faa-owner/AEROTRUST%20SERVICES%20CORP%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 1983, S/N 3007
- [N3726](https://openairdocs.org/aircraft/N3726): [Canyons Aviation Group LLC](https://openairdocs.org/faa-owner/CANYONS%20AVIATION%20GROUP%20LLC), [Orlando, FL](https://openairdocs.org/faa-place/FL/Orlando), built 1997, S/N 5351
- [N654CM](https://openairdocs.org/aircraft/N654CM): [Pacific States Industries Inc](https://openairdocs.org/faa-owner/PACIFIC%20STATES%20INDUSTRIES%20INC), [Morgan Hill, CA](https://openairdocs.org/faa-place/CA/Morgan%20Hill), built 1987, S/N 5009
- [N657GF](https://openairdocs.org/aircraft/N657GF): [Challenger 601 - 3045 Inc](https://openairdocs.org/faa-owner/CHALLENGER%20601%20-%203045%20INC), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), S/N 3045
- [N773CL](https://openairdocs.org/aircraft/N773CL): [Pollard Spares LLC](https://openairdocs.org/faa-owner/POLLARD%20SPARES%20LLC), [Roanoke, TX](https://openairdocs.org/faa-place/TX/Roanoke), built 1984, S/N 3032
- [N800LB](https://openairdocs.org/aircraft/N800LB): [Rj Logistics II LLC](https://openairdocs.org/faa-owner/RJ%20LOGISTICS%20II%20LLC), [Meridian, ID](https://openairdocs.org/faa-place/ID/Meridian), built 1997, S/N 5361
- [N8432A](https://openairdocs.org/aircraft/N8432A): [Logos Aviation Inc](https://openairdocs.org/faa-owner/LOGOS%20AVIATION%20INC), [Fort Lauderdale, FL](https://openairdocs.org/faa-place/FL/Fort%20Lauderdale), built 2000, S/N 7432
- [N8444F](https://openairdocs.org/aircraft/N8444F): [Logos Aviation Inc](https://openairdocs.org/faa-owner/LOGOS%20AVIATION%20INC), [Fort Lauderdale, FL](https://openairdocs.org/faa-place/FL/Fort%20Lauderdale), built 2000, S/N 7444
- [N883CA](https://openairdocs.org/aircraft/N883CA): [Adlakha Aviation LLC](https://openairdocs.org/faa-owner/ADLAKHA%20AVIATION%20LLC), [Pflugerville, TX](https://openairdocs.org/faa-place/TX/Pflugerville), built 1999, S/N 5406
- [N893TA](https://openairdocs.org/aircraft/N893TA): [Sta Aviation Management](https://openairdocs.org/faa-owner/STA%20AVIATION%20MANAGEMENT), [New York City, NY](https://openairdocs.org/faa-place/NY/New%20York%20City), built 1983, S/N 3016
- [N9191](https://openairdocs.org/aircraft/N9191): built 1996, S/N 5312
- [N999YG](https://openairdocs.org/aircraft/N999YG): [Slate 999 LLC](https://openairdocs.org/faa-owner/SLATE%20999%20LLC), [Johnstown, PA](https://openairdocs.org/faa-place/PA/Johnstown), built 1995, S/N 7075

## NTSB investigations (5)

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 CEN12IA662](https://openairdocs.org/ntsb/CEN12IA662), Sep 21, 2012: Canadair CL-600 Challenger (N125PS), Denver, CO, incident, no damage. Probable cause: The internal failure of the galley heater mat’s thermostat, which resulted in an overheat condition.
- [NTSB SEA08IA080](https://openairdocs.org/ntsb/SEA08IA080), Feb 13, 2008: Bombardier CL-600 (N651BR), Hilo, HI, incident, no damage. Probable cause: The captain and first officer inadvertently falling asleep during the cruise phase of flight. Contributing to the incident were the captain's undiagnosed obstructive sleep apnea and the flight crew’s…
- [NTSB NYC07RA064](https://openairdocs.org/ntsb/NYC07RA064), Feb 13, 2007: Bombardier CL-600-2B19 (N168CK), Moscow, Russia, destroyed
- [NTSB NYC01LA023](https://openairdocs.org/ntsb/NYC01LA023), Oct 24, 2000: Bombardier CL-600 (N804CA), New York, NY, substantial damage. Probable cause: The Boeing captain's misjudgment of the distance between his airplane and the CRJ. A factor was the nighttime conditions.
- [NTSB SEA88IA028](https://openairdocs.org/ntsb/SEA88IA028), Dec 6, 1987: Canadair CL600-2A12 (N125PS), Twentynine Plms, CA, incident, no damage

## FAA accident and incident reports (15)

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 20120921024269I](https://openairdocs.org/incident/20120921024269I), Sep 21, 2012: Canadair Ltd CL-600-2A12 (N125PS), Denver, CO, No damage. On 9/21/2012 at approximately 1430 hrs. MDT, N125PS, a Canadair Ltd. Model CL-600-2A12 challenger aircraft sustained no damage after making an emergency…
- [Incident 20100204036169I](https://openairdocs.org/incident/20100204036169I), Feb 4, 2010: Bombardier CL-600-2B19 (N861AS), Atlanta, GA, No damage. On February 2, 2010, atlantic southeast airlines flight 5432, operating from daytona beach, Florida to Atlanta, Georgia with CRJ-200 aircraft N861AS,…
- [Incident 20080213012359I](https://openairdocs.org/incident/20080213012359I), Feb 13, 2008: Cndair CL6002B19 (N651BR), Hilo, HI, No damage. (-23) Hilo, HI: air shuttle 1002, CRJ-2, N651BR, flight from honolulu to Hilo, HI, on 2/13 at 1130PST, both pilots fell asleep and overflew the airport by 15…
- [Incident 20051007031199I](https://openairdocs.org/incident/20051007031199I), Oct 7, 2005: Cndair CL6002B19 (N641BR), Cleveland, OH. (-23) Vtza flt 1132 iad-cle landed without incident after declaring an emergency due to no flaps. Vtza maintenance ferried the acft to iad where vtza…
- [Incident 20040918022829I](https://openairdocs.org/incident/20040918022829I), Sep 18, 2004: Cndair CL6002B19 (N87353), Boise, ID, Minor damage. (-23) Right nose landing gear tire tread separated during takeoff roll at kalispell Mt. Nose landing gear would not indicate up and locked. Pilot declared…
- [Incident 20030501008759I](https://openairdocs.org/incident/20030501008759I), May 1, 2003: Cndair CL6002B19 (N651BR), Wichita, KS. (-23) Flight 7225 enroute ord-ict, on approach to ict, experienced a flap fail message when flap handle was put in down position. Crew aborted landing. No…
- [Incident 20030111006459I](https://openairdocs.org/incident/20030111006459I), Jan 11, 2003: Cndair CL6002B19 (N8432A), Dayton, OH. (-23) On 01/11/2003, designator rexa express airlines I, inc. dba northwest airlink - pinnacle- call sign FLG5683, E145, at 0203Z enroute to Dayton, Ohio,…
- [Incident 20021108035539I](https://openairdocs.org/incident/20021108035539I), Nov 8, 2002: Cndair CL6002B19 (N8432A), Minneapolis, MN. (-23) During flight from Minneapolis, MN to omaha, NE, the flight crew experienced a "passenger door outer handle" caution light, followed by the "passenger…
- [Accident 20001023040649A](https://openairdocs.org/incident/20001023040649A), Oct 23, 2000: Cndair CL6002B19 (N804CA), New York, NY, No damage. (-23) On October 23, 2000, at 2123 EST, American trans air (ata) flight 596, a Boeing 727-200 (N786AT), was being taxied for take-off at laguardia airport…
- [Incident 20001012024519I](https://openairdocs.org/incident/20001012024519I), Oct 12, 2000: Cndair CL6002B19 (N17175), Milwaukee, WI, Minor damage. (-23)See attached form FAA 8020-23
- [Incident 20000731035049I](https://openairdocs.org/incident/20000731035049I), Jul 31, 2000: Cndair CL6002B19 (N17175), Philadelphia, PA. (-23)Usair express (mesa airlines), flight 5805, N17175, a crj, phl-mke, was involved in a ground stop that resulted in an almost 2 hour taxi from the usair…
- [Incident 19981102034019I](https://openairdocs.org/incident/19981102034019I), Nov 2, 1998: Cndair CL6002B19 (N17175), Indianapolis, IN. Left engine oil pressure loss. Crew performed emergency shutdown. A/c was in a ferry flight when seals allowed oil pressure drop on left engine. A/c landed…
- [Incident 19981030041689I](https://openairdocs.org/incident/19981030041689I), Oct 30, 1998: Cndair CL6002B19 (N632BR), Indianapolis, IN. The crew declared an emergency due to an overheated anti-ice duct. The aircraft landed without further incident. A service difficulty report (SDR) was…
- [Incident 19891022056259I](https://openairdocs.org/incident/19891022056259I), Oct 22, 1989: Cndair CL6002A12 (N125PS), Santa Ana, CA, Minor damage. During engine start a jet blast caused minor damage to a parked aircraft. Pilot taxied away and departed.
- [Incident 19871206075519I](https://openairdocs.org/incident/19871206075519I), Dec 6, 1987: Cndair CL6002A12 (N125PS), Twenty Nine Pal, CA. Dutch roll at FL330 due to yaw damper problem caused by leaky galley water filter. Turned off autopilot. Landed ok.

## Service difficulty reports (115, newest 50)

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

- [SDR ASOA201001969](https://openairdocs.org/sdr/ASOA201001969), Dec 15, 2010: SMOKE DETECTOR. FALSE INDICATION. SMOKE TOILET CAUTION MSG ILLUMATED MOMENTARLY IN FLIGHT. R & R LAV SMOKE DETECTOR, OPS CK GOOD REF AMM 26-16-01.
- [SDR ASOA201001532](https://openairdocs.org/sdr/ASOA201001532), Oct 10, 2010: LAMP. BURNED OUT. NR 4 POSITION EXTERIOR EMERGENCY LIGHT INOP. RELAMPED NR4 POSITION EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21.
- [SDR ASOA201001020](https://openairdocs.org/sdr/ASOA201001020), Jul 18, 2010: ATTACH FITTING. CRACKED. FOUND ENGINE SUPPORT BEAM FWD CLIP AT LBL 9.5 HAS A CRACK APPROX .5" IN LENGTH NEAR LOWER FASTENER. R & R CLIP AT ESB AT LBL 9.5 FWD WEB IAW SRM 51-42-06 AND 51
- [SDR ASOA201000332](https://openairdocs.org/sdr/ASOA201000332), Feb 27, 2010: BULKHEAD. CRACKED. COMPLIED WITH A SPECIAL DETAILED INSP OF FS559.0 PRESSURE BULKHEAD WEB AND CAP ANGLE LOCAL TO BL9.0 AND BL18.0 LT AND RT IAW NDT MANUAL, PART 6, 53-41-201. (3) 
- [SDR CA090831001](https://openairdocs.org/sdr/CA090831001), Aug 18, 2009: SIGNAL COND UNIT. FAULTY. RT LOW OIL PRESSURE ON CLIMB-OUT, AFTER LANDING, RT ENGINE WAS DOWN 5 LITRES. OIL LEVEL RETURNED TO NORMAL (5 LITRES ADDED) AND NO FURTHER INCIDENTS. OIL LEVEL 
- [SDR DJFA2007133](https://openairdocs.org/sdr/DJFA2007133), Nov 2, 2007: ADG. BURNED. DURING POST MAINTENANCE CHECK FLIGHT, CREW TESTED THE AIR DRIVEN GENERATOR SYSTEM (ADG). DURING THE TEST THE ADG FAILED LEAVING THE CREW IN COMPLETE ELECTRICAL 
- [SDR WWQ2007F00001](https://openairdocs.org/sdr/WWQ2007F00001), Aug 5, 2007: WIRE HARNESS. SHORTED. DURING APPROACH, THE CREW EXTENDED THE LANDING GEAR (NORMAL PROCEDURE). SEVERAL SECONDS AFTER THE GEAR EXTENSION THE NOSE LANDING GEAR DOWN AND LOCKED GREEN LIG
- [SDR 2007FA0000000](https://openairdocs.org/sdr/2007FA0000000), Dec 1, 2006: ENGINE. FAILED. RT ENGINE FAILURE AT T/O. ALL INDICATIONS WERE NORMAL ON ENGINE START AND TAXI. UPON THRUST ADVANCEMENT FOR TAKEOFF, AT APPROXIMATELY 60 PERCENT N1 WE HEARD AND
- [SDR 2006FA0000835](https://openairdocs.org/sdr/2006FA0000835), Aug 11, 2006: INVERTER. MISINSTALLED. THIS STATIC FREQUENCY INVERTER WAS INSTALLED IN THE STATED AIRCRAFT ON JUNE 2, 2006. AT THE TIME OF INSTALLATION, THE PART HAD BEEN OVERHAULED BY CONSOLIDATED A
- [SDR CA060515002](https://openairdocs.org/sdr/CA060515002), May 3, 2006: VENT LINE. CORRODED. (CAN) MASTER REFUEL PANEL CHECK TO CHECK VALVE FOR OP, FUEL CAME OUT OF LT NACA SCOOP APPROX 2 GALLON, THEN STOP. MAINT WAS ADVISE THIS WAS ONLY HAPPEN WHEN AC 
- [SDR CA060515003](https://openairdocs.org/sdr/CA060515003), May 3, 2006: VENT LINE. CORRODED. (CAN) REFUELLING WAS C/O, MASTER REFUEL PANEL CHECK C/O TO CHECK VALVE FOR OPERATION, WHAT WAS NOTICED, FUEL CAME OUT OUT OF THE LT NACA SCOOP APPROXIMATE 2 GAL
- [SDR CA051121001](https://openairdocs.org/sdr/CA051121001), Nov 21, 2005: FUEL HEATER. CRACKED. (CAN) FUEL LEAK AS BEEN FOUND ON SEVEN DAYS INSPECTION, TECHNICIAN HAS FOUND A CRACK IN A SOLDERED JOINT ON FUEL HEATER. THE FUEL HEATER HAS BEEN REPLACED AND T
- [SDR DJFA2005159](https://openairdocs.org/sdr/DJFA2005159), Oct 19, 2005: BULKHEAD. CRACKED. DURING A ROUTINE MAINTENANCE VISIT, A CRACK WAS DISCOVERED IN THE PRESSURE BULKHEAD WEB AT FUSELAGE STATION 409.00 WHILE PERFORMING AD 97-24-02. THE CRACK WAS R
- [SDR COMA0560558](https://openairdocs.org/sdr/COMA0560558), Oct 17, 2005: ACTUATOR. MALFUNCTIONED. FLIGHT 5814 - FLAPS FAIL. REPLACED THE RT OB FLAP ACTUATOR.
- [SDR MASA200500354](https://openairdocs.org/sdr/MASA200500354), May 14, 2005: OIL SYSTEM. LOW. CREW RETURNED TO FIELD FOR RT ENGINE OIL LOW PRESSURE. CREW DID NOT SHUT DOWN ENGINE. MX SERVICED ENGINE OIL.
- [SDR CA050413003](https://openairdocs.org/sdr/CA050413003), Apr 13, 2005: ELEMENT. BROKEN. (CAN) DURING A SCHEDULED 1200-HOUR CHECK, A FUNCTIONAL TEST OF THE RIGHT THRUST REVERSER AUTO THROTTLE RETARDER WAS CARRIED OUT. THE RIGHT THROTTLE FAILED TO RE
- [SDR CA050406005](https://openairdocs.org/sdr/CA050406005), Apr 6, 2005: ACTUATOR. LEAKING. (CAN) NOSE LANDING GEAR ACTUATOR LEAKING AT ROD END PISTON. LIFE LIMITED PART AT 19480 CYCLES. A/C RETURN TO BASE ON SPECIAL FLIGHT PERMIT WITH GEAR DOWN.
- [SDR CA050215012](https://openairdocs.org/sdr/CA050215012), Feb 10, 2005: CONNECTOR. LOOSE. (CAN) ON APPROACH, NLG WOULD NOT DEPLOY UPON NORMAL SELECTION OF LANDING GEAR DOWN. EMER EXTENSION WAS COMPLETED, AC LANDED WITHOUT FURTHER INCIDENT, FOUND THAT
- [SDR CA050125008](https://openairdocs.org/sdr/CA050125008), Jan 19, 2005: ACCESS DOOR. DISTORTED. (CAN) THIS AIRCRAFT WAS INSPECTED AND TESTED AND FOUND TO EXHIBIT UNACCEPTABLE NOSE AVIONICS ACCESS DOOR DEFORMATION IN EXTREME COLD CONDITIONS. THE DEGREE OF D
- [SDR COMA0460445](https://openairdocs.org/sdr/COMA0460445), Aug 3, 2004: OUTFLOW VALVE. OBSTRUCTED. FLIGHT 4952 AIRCRAFT WILL NOT PRESSURIZE. FOUND SAFETY WIRE IN OUTFLOW VALVE. REMOVED WIRE AND PRESSURE CHECK WAS NORMAL.
- [SDR CA040729002](https://openairdocs.org/sdr/CA040729002), Jul 27, 2004: GENERATOR. FAILED. DURING A ROUTINE POST MAJOR MAINTENANCE FLIGHT CHECK OF THE AIR DRIVEN TURBINE GENERATOR SYSTEM, THE SYSTEM FAILED TO TAKE THE ELECTRICAL LOAD, AS INDICATED BY 
- [SDR CA040603004](https://openairdocs.org/sdr/CA040603004), Jun 3, 2004: AILERON. MISMANUFACTURED. (CAN) WHILE INVESTIGATING A SNAG, DISCOVERED AN AILERON A/P QUADRANT ASSEMBLY P/N 40E22-84-1069-1 WHICH DID NOT MEET THE MANUFACTURER'S DRAWING IN THE INSTALLAT
- [SDR REX2004F00001](https://openairdocs.org/sdr/REX2004F00001), Jun 1, 2004: APU. ODOR. ELECTRICAL/AC SMOKE IN CABIN. EVACUATED AIRCRAFT-MECHANIC NOTIFIED. PERFORMED ENG RUNS/BLEED AIR CHECKS IAW. NO SMOKE NOTED. OK FOR SERVICE. SMOKE IN CABIN ON A
- [SDR CA040423007](https://openairdocs.org/sdr/CA040423007), Apr 16, 2004: POTENTIOMETER. INTERMITTENT. (CAN) DURING TAKEOFF ROTATION, THE STICK SHAKER ACTIVATED ON THE LOW LEVEL, THE STALL PROTECT SYSTEM (SPS) WARBLER SOUNDED, THE SPS FAIL LIGHTS WENT TO A FLASH 
- [SDR REXA04003](https://openairdocs.org/sdr/REXA04003), Jan 31, 2004: OIL SYSTEM. LOW. FLIGHT CREW RECEIVED AN AURAL OIL PRESSURE WARNING FOR THE LEFT ENGINE. OIL PRESSURE WAS OBSERVED TO BE FLUCTUATING BETWEEN 25-30 PSI. FLIGHT CREW PERFORMED AN 
- [SDR CA040321003](https://openairdocs.org/sdr/CA040321003), Jan 13, 2004: WINDOW. FAILED. (CAN) THE LEFT SIDE WINDOW HAD SHATTERED. AN EMERGENCY DESCENT WAS TAKEN.THE REMAINDER OF THE FLIGHT, APPROACH AND LANDING WERE UNEVENTFUL. THE WINDOW WAS REPLA
- [SDR MASA200300509](https://openairdocs.org/sdr/MASA200300509), Dec 23, 2003: LIGHT. INOPERATIVE. CAPTAIN REPORTED A CABIN CEILING EMERGENCY LIGHT INOPERATIVE. MECHANIC RELAMPED. OP CHECKS GOOD
- [SDR CA031205003](https://openairdocs.org/sdr/CA031205003), Dec 1, 2003: SKIN. DAMAGED. (CAN) DURING FTP STALLS, BUFFET WAS EXPERIENCED JUST PRIOR TO PUSHER ACTIVATION FOR BOTH THE CLEAN AND F20 STALLS. ADDITIONALLY A MILD LT WING DROP WAS EXPERIEN
- [SDR CA031113001](https://openairdocs.org/sdr/CA031113001), Oct 14, 2003: ENGINE. SHUTDOWN. (CAN) DURING CRUISE AT FL 390, THE RT ENGINE SHUTDOWN. THE CREW REPORTED ALL ENGINE PARAMETERS WERE NORMAL AT THE TIME AND NO MESSAGES OR CAUTIONS WERE POSTED. 
- [SDR JBXA03017](https://openairdocs.org/sdr/JBXA03017), Sep 23, 2003: AILERON. FROZEN. FLIGHT 5119 FROM PWM TO DCA PILOT REPORTED LT AILERON WAS FROZEN. PERFORMED DISCONNECT. ON DESCENT PILOTS RECONNECTED AND NO FURTHER PROBLEMS WERE REPORTED. PRO
- [SDR CA030903006](https://openairdocs.org/sdr/CA030903006), Aug 27, 2003: ACTUATOR. FAILED. (CAN) ATTEMPT TO TRIM AIRCRAFT NOSE UP OR NOSE DOWN CAUSED BOTH PITCH TRIM CHANNELS TO INDICATE (OFF). THUS HORIZONTAL PITCH TRIM SYSTEM DE-ACTIVATED.
- [SDR CA030122001](https://openairdocs.org/sdr/CA030122001), Jan 19, 2003: FITTING. BROKEN. (CAN) DOOR TENSION FITTING (UPPER FORWARD) BROKEN IN FLIGHT.
- [SDR CA021125002](https://openairdocs.org/sdr/CA021125002), Nov 11, 2002: BEARING. BROKEN. (CAN) DURING 300-600 HOURS INSPECTION AILERON PCU OPERATION TEST, FOUND AILERON QUADRANT IN RT WHEEL WELL IS NOISY (SNAPPING).AFTER REMOVING RT/ AILERON QUADRAN
- [SDR CA021217006](https://openairdocs.org/sdr/CA021217006), Nov 11, 2002: BEARING. BROKEN. (CAN) DURING 300-600 HOUR INSPECTION AILERON PCU OPERATION TEST. FOUND AILERON QUADRANT IN RT WHEEL WELL IS NOISY (SNAPPING). AFTER REMOVING RT AILERON QUADRANT
- [SDR CA020925003](https://openairdocs.org/sdr/CA020925003), Sep 18, 2002: WIRE HARNESS. EXPOSED. (CAN) WIRING HARNESS FOR THE ENGINE FIRE BOTTLE SQUIBS LOCATED IN THE APU AREA HAD EXPOSED WIRES WHERE THEHARNESS ENTERS THE CONNECTOR PLUG FOR THE SQUIB.
- [SDR SWIA200211107](https://openairdocs.org/sdr/SWIA200211107), Aug 1, 2002: ENGINE. OVERTEMP. DURING TAKEOFF, LEFT ENGINE ITT WENT TO 907 DEGREES, FLASHING RED. ABORTED TAKEOFF. REMOVED AND REPLACED LEFT ENGINE IAW MM 71-00-00.
- [SDR CA020806002](https://openairdocs.org/sdr/CA020806002), Jul 19, 2002: CONNECTOR. FAILED. (CAN) AS A RESULT OF REPORTED "PUMP INOP" LIGHT AND ADAPTER OIL "HI TEMP" LIGHT, REPLACED THE APU BOOST PUMP. OPERATED NORMALLY FOR THE FIRST FEW TESTS BUT QUIT
- [SDR CA020220012](https://openairdocs.org/sdr/CA020220012), Feb 15, 2002: OUTFLOW VALVE. FAILED. (CAN) OVERHAULED SECONDARY OUTFLOW VALVE FOR PRESSURIZATION SYSTEM WAS INSTALLED TO RECTIFY A POPPED CIRCUIT BREAKER. SYSTEM GROUND RUN CARRIED OUT AND AIRCRAFT
- [SDR M02023](https://openairdocs.org/sdr/M02023), Feb 11, 2002: BULB. BURNED OUT. DURING OVERNIGHT MAINTENANCE, IT WAS DISCOVERED THAT THE RIGHT FORWARD EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MECHANIC REMOVED AND REPLACED THE LIGHTS. OPS CHE
- [SDR CA020207004](https://openairdocs.org/sdr/CA020207004), Feb 6, 2002: BELLCRANK. (CAN) DOOR HARD TO OPEN: INSPECTION FOUND CRANK ASSY CRACKED (P/N 600-31890-21) - PART CRACKED DUE TO IMPROPER INSTALLATION OF SB 601-0192 - DOGS OF LOST MOTION
- [SDR CA020308012](https://openairdocs.org/sdr/CA020308012), Jan 30, 2002: ENGINE. FAILED. (CAN) DURING FLIGHT INSPECTION OF ILS CLEARANCE ORBIT OF AIRFIELD IN SLIGHT BANK & 10-20 KTS TAILWIND NR 2 ENGINE SUDDENLY SHUTDOWN. A/C RETURNED & LANDED. ENGI
- [SDR CA020207003](https://openairdocs.org/sdr/CA020207003), Jan 18, 2002: BRAKE. MALFUNCTIONED. (CAN) DURING TAXI- ANTI-SKID TEST FAILURE - WIRES BG15B20BLU & GB30B20WHT - SUSPECT CYCLIC FAILURE.
- [SDR CA011217020](https://openairdocs.org/sdr/CA011217020), Dec 17, 2001: CONTROLLER. BURNED. (CAN) AS AIRCRAFT WAS SITTING IN THE HANGER WITH POWER ON ADS HEATER CONTROL TURNED OFF SMOKE STARTED COMING OUT FROM CONTROLLER POWER WAS SHUT DOWN. C/B DID NO
- [SDR CA011113013](https://openairdocs.org/sdr/CA011113013), Nov 6, 2001: CONTACTOR. BURNED. (CAN) AFTER STARTING ENGINES WENT AND TRANSFERED GENRATORS. TURNED ON NR 3A HYD PUMP LARGE POWER SURGE ABOUT 34KVA NR 3A HYD BREAKER POPPED. TURNED ON NR 1 HYD 
- [SDR CA011101018](https://openairdocs.org/sdr/CA011101018), Sep 29, 2001: INDICATOR. FAILED. (CAN) SMOKE IN CABIN WHEN AIRCRAFT IS PARKED AT BAGOTVILLE AIRPORT. A FAIL RESISTANCE HAS BEEN FOUND ON THE CABIN DISPLAY ALTITUDE REPORTER WHICH IS USED BY MED
- [SDR M01091](https://openairdocs.org/sdr/M01091), Aug 15, 2001: LIGHT. INOPERATIVE. DURING A PREFLIGHT INSPECTION, THE CREW FOUND THE FIRST THREE SECTIONS OF THE FLOOR TRACK LIGHTING INOPERATIVE. MAINTENANCE CLEANED THE CONNECTIONS. OPS CHECKED
- [SDR 2001FA0000174](https://openairdocs.org/sdr/2001FA0000174), Jun 1, 2001: CHECK VALVE. DAMAGED. DURING REPLACEMENT OF THE CHECK VALVE, FOUND PIECES OF CHECK VALVE FLAPPERS, REPLACED WITH PN 320-2832-1-1 SN 635 OPERATIONAL CHECKED SATISFACTORY. NOTE: ALL PI
- [SDR CA010403003](https://openairdocs.org/sdr/CA010403003), Mar 13, 2001: BEAM. CRACKED. (CAN) DURING C-CHECK A CRACK WAS FOUND IN THE ENGINE SUPPORT BEAM LOWER WEB BETWEEN FS 625.30 AND FS 640.00 NEAR LBL 36.20. THE CRACK WAS LOCATED IN THE CORNER 
- [SDR COMA0160234](https://openairdocs.org/sdr/COMA0160234), Feb 10, 2001: WARNING SYSTEM. ILLUMINATED. RT ENGINE FAN VIB ICON ON EICAS. INSPECTED ENGINE AND FOUND NO DEFECTS. COULD NOT DUPLICATE.
- [SDR CA010213019](https://openairdocs.org/sdr/CA010213019), Jan 24, 2001: SMOKE DETECTOR. FAULTY. (CAN) ON SHORT FINAL, SMOKE TOILET CAUTION MESSAGE CAME ON. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT ANY FURTHER EVENT.LAV SMOKE DETECTOR FOUND FAULTY & RE

All 115: https://openairdocs.org/engine/ge-cf-34-1a/reports.md

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