# GE CT7-5A2

- Type: Engine model (FAA registry)
- Registry code: 30144
- Manufacturer (registry): GE
- Model: CT7-5A2
- Engine type: Turbo-prop
- Power: 1,735 hp
- Data sheet: [TCDS E8NE](https://openairdocs.org/tcds/E8NE) (OpenAirDocs)
- Holder: General Electric Company GE Aviation
- Installed in: 7 registered aircraft
- Page: https://openairdocs.org/engine/ge-ct7-5a2

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 2025-05-02](https://openairdocs.org/ad/2025-05-02): Engine (Turbine/Turboprop) · General Electric CT7-5A2, CT7-5A3, CT7-7A and 8 more. Effective Apr 8, 2025
- [AD 2023-21-07](https://openairdocs.org/ad/2023-21-07): Turbine Engine Reduction Gear · General Electric CT7-5A2, CT7-5A3, CT7-7A and 6 more. Effective Dec 11, 2023
- [AD 2007-08-01](https://openairdocs.org/ad/2007-08-01): Eddy current inspection (ECI) of boltholes · General Electric CT7-5A2, CT7-5A3, CT7-7A and 8 more. Effective May 14, 2007
- [AD 2004-07-09](https://openairdocs.org/ad/2004-07-09): PGB oil filter impending bypass button (IBB) · General Electric CT7-2A, CT7-2D, CT7-2D1 and 14 more. Effective May 11, 2004
- [AD 2002-01-03](https://openairdocs.org/ad/2002-01-03): Stage 2 Turbine Aft Cooling Plates · General Electric CT7-5A2, CT7-5A3, CT7-7A and 1 more. Effective Feb 12, 2002
- [AD 97-25-07](https://openairdocs.org/ad/97-25-07): Stage 1 or 2 Gas Generator Turbine (GGT) Disk · General Electric CT7-5A2, CT7-7A, CT7-9B and 1 more. Effective Jan 28, 1998
- [AD 96-26-01](https://openairdocs.org/ad/96-26-01): GGT Stage 2 Forward Cooling Plate · General Electric CT7-5A2, CT7-7A, CT7-9B and 1 more. Effective Mar 10, 1997
- [AD 94-17-16](https://openairdocs.org/ad/94-17-16): Propeller Gearboxes · General Electric CT7-5A2, CT7-5A3, CT7-7A and 6 more. Effective Sep 15, 1994
- [AD 93-25-17](https://openairdocs.org/ad/93-25-17): Gas Generator Turbine (GGT) Disks and Cooling Plates · General Electric CT7-2A, CT7-5A2, CT7-6 and 2 more. Effective Feb 2, 1994
- [AD 93-23-05](https://openairdocs.org/ad/93-23-05): Gas Generator Turbine (GGT) Rotor Assembly Parts and Power Turbine (PT) Disks · General Electric CT7-5A2 and CT7-7A. Effective Jan 10, 1994
- [AD 88-07-08](https://openairdocs.org/ad/88-07-08): Power Turbine Overspeed · General Electric CT7-5A2. Effective May 9, 1988

Historical (superseded or no longer in force):

- [AD 2018-03-13](https://openairdocs.org/ad/2018-03-13) (historical): Turbine Engine Reduction Gear · General Electric CT7-5A2, CT7-5A3, CT7-7A and 6 more. Effective Feb 28, 2018
- [AD 2005-18-01](https://openairdocs.org/ad/2005-18-01) (historical): Turbine aft cooling plate boltholes · General Electric Aircraft Engines CT7-5A2, CT7-5A3, CT7-7A and 4 more. Effective Oct 24, 2005
- [AD 2003-06-03](https://openairdocs.org/ad/2003-06-03) (historical): Propeller gearbox (PGB) oil filter · General Electric Aircraft Engines CT7-2A, CT7-2D, CT7-2D1 and 14 more. Effective Apr 24, 2003

## Registered aircraft (7)

- [N118PA](https://openairdocs.org/aircraft/N118PA): [Phoenix Air Group Inc](https://openairdocs.org/faa-owner/PHOENIX%20AIR%20GROUP%20INC), [Cartersville, GA](https://openairdocs.org/faa-place/GA/Cartersville), built 1989, S/N 151
- [N189PA](https://openairdocs.org/aircraft/N189PA): [Phoenix Air Group Inc](https://openairdocs.org/faa-owner/PHOENIX%20AIR%20GROUP%20INC), [Cartersville, GA](https://openairdocs.org/faa-place/GA/Cartersville), built 1985, S/N 038
- [N44KS](https://openairdocs.org/aircraft/N44KS): [Go Vector One LLC](https://openairdocs.org/faa-owner/GO%20VECTOR%20ONE%20LLC), [Pls Vrds Est, CA](https://openairdocs.org/faa-place/CA/Pls%20Vrds%20Est), built 1986, S/N 340A-050
- [N671BC](https://openairdocs.org/aircraft/N671BC): [Ibc Airways Inc](https://openairdocs.org/faa-owner/IBC%20AIRWAYS%20INC), [Fort Lauderdale, FL](https://openairdocs.org/faa-place/FL/Fort%20Lauderdale), built 1987, S/N 340A-084
- [N681BC](https://openairdocs.org/aircraft/N681BC): [Aviation Inventory Resources Inc](https://openairdocs.org/faa-owner/AVIATION%20INVENTORY%20RESOURCES%20INC), [Alvarado, TX](https://openairdocs.org/faa-place/TX/Alvarado), built 1987, S/N 340A-108
- [N901BC](https://openairdocs.org/aircraft/N901BC): [Aviation Inventory Resources Inc](https://openairdocs.org/faa-owner/AVIATION%20INVENTORY%20RESOURCES%20INC), [Alvarado, TX](https://openairdocs.org/faa-place/TX/Alvarado), built 1987, S/N 340A-088
- [N907RA](https://openairdocs.org/aircraft/N907RA): [Ryan Air Inc](https://openairdocs.org/faa-owner/RYAN%20AIR%20INC), [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage), built 1987, S/N 340A-111

## NTSB investigations

None matched to aircraft with this engine model.

## FAA accident and incident reports (4)

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 20210121002349I](https://openairdocs.org/incident/20210121002349I), Jan 21, 2021: Saab-Fairchild 340A (N907RA), Anchorage, AK, Minor damage. The crew was cleared for a visual approach to runway 7R. The aircraft was descending into Anchorage international airport on right base. The SIC noticed sparks…
- [Incident 20040525008769I](https://openairdocs.org/incident/20040525008769I), May 25, 2004: Saab SF340A (N95CQ), Pittsburgh, PA. (-23) At 1750E, shuttle america flight 4556, a, SF34, aborted takeoff on runway 28R for unknown reasons. No assistance was required and the aircraft returned…
- [Incident 20010406005969I](https://openairdocs.org/incident/20010406005969I), Apr 6, 2001: Cessna 340A (N95CQ), Pittsburgh, PA. (-23) On 4/6/01 at 8:45 am at Pittsburgh international airport chautauqua flight #4215 a saab-fairchild 340-A N95CQ aborted a takeoff on runway 28R. ATC…
- [Incident 19970319010639I](https://openairdocs.org/incident/19970319010639I), Mar 19, 1997: Saab SF340A (N95CQ), Pittsburgh, PA, Minor damage. Narrative: the pilot stated: when taxiing in to gate E-9 at Pittsburgh, he was taxiing the aircraft between parked DO-328 and a truck. He thought he was clear…

## Service difficulty reports (450, newest 50)

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

- [SDR OZCA2025002641](https://openairdocs.org/sdr/OZCA2025002641), May 31, 2025: DOWNLOCK SWITCH. LOOSE. ON APPROACH INTO SNU, THE CREW SELECTED THE LANDING GEAR DOWN AND FAILED TO GET A DOWN AND LOCKED INDICATION ON THE LH MLG. THE CREW NOTIFIED THE TOWER AND ABOR
- [SDR OZCA2024091706641](https://openairdocs.org/sdr/OZCA2024091706641), Sep 16, 2024: ENGINE. ERRATIC. TAKING OFF FROM RUNWAY 06 IN FREEPORT, CLIMB OUT TO 1000 FT, CREW STARTED THE CLIMB CHECKLIST. UPON TURNING OFF CTOT AND SETTING CONDITION LEVERS TO CLIMB, THE 
- [SDR OZCA2024004641](https://openairdocs.org/sdr/OZCA2024004641), Aug 12, 2024: ENGINE. OVERTEMP. DURING DESCENT, SEVERAL LOUD BANGS WERE HEARD FROM THE RH ENGINE WITH VIBRATIONS. MAJOR FLUCTUATIONS ON THE TORQUE AND ITT. OVERTEMP LIGHT CAME ON FOR APPROX. 5
- [SDR OZCA20240219001](https://openairdocs.org/sdr/OZCA20240219001), Feb 16, 2024: BLEED AIR SYS. LOOSE. AT FL240 RIGHT TQ AND RIGHT PROP RPM GAUGES AT ZERO. UNABLE TO MAINTAIN AIRSPEED. RIGHT ENGINE BECAME ROUGH, FUEL FLOW DECREASED. GAUGES THEN RETURNED TO NORMAL
- [SDR OZCA340076221212](https://openairdocs.org/sdr/OZCA340076221212), Dec 12, 2022: TRIMMER. FAULTY. CROSSING 11,000 FT, RIGHT ENGINE ITT INCREASE UNCOMMANDED TO 872C (802C BEFORE INCREASE). PROCEEDED WITH QRH - REDUCING POWER POWER LEVERS BROUGHT TEMPERATURES 
- [SDR OZCA340084221207](https://openairdocs.org/sdr/OZCA340084221207), Dec 7, 2022: PERISEAL. UNSERVICEABLE. #2 ENGINE IN CRUISE, ITT OUT OF LIMITS. C/W QRH. - REMOVED AND REPLACED R/H SIDE UNDER WING FLAP PERI-SEAL IAW SF340A AMM 36-11-40-04. RUN CHECKS SATISFACTORILY
- [SDR OZCA340076221103](https://openairdocs.org/sdr/OZCA340076221103), Nov 3, 2022: CHIP DETECTOR. ACTIVATED. DURING CRUISE FLIGHT AT 17000 FT LEFT ENGINE CHIP DETECT LIGHT ILLUMINATED A8-15 QRH. NO OTHER ABNORMALITIES. -- REMOVED AND REPLACED LT HAND ENGINE CHIP DETECT
- [SDR OZCA06102DEC2021](https://openairdocs.org/sdr/OZCA06102DEC2021), Dec 2, 2021: HMU. FAULTED. SUPPLEMENTAL - ON GO AROUND RWY 26R AT MIA ENG 1 OIL PRESS LT CAME ON, LOST POWER, MEMORY ITEMS, DECLARED EMERGENCY AND QRH COMPLY. - DURING T/S FOUND AT BOTTOM
- [SDR OZCA340088211109](https://openairdocs.org/sdr/OZCA340088211109), Nov 9, 2021: CLAMP. CRACKED. DURING TO/O ROLL @ V1, PLANE DISPLAYED HIGH TEMP + LOW PROP OIL PRESSURE IN #2 ENG PROP RPM DROPPED, ENGINE SHUTDOWN. COMPLIED W/QRH, RETURNED TO LAND AT MYNN. 
- [SDR OZCA90130MAR21](https://openairdocs.org/sdr/OZCA90130MAR21), Mar 30, 2021: PROPELLER. LOW PRESSURE. DURING CRUISE FLIGHT AT 13000, WE HAD PROP OIL PRESSURE LOW ON #1 ENGINE. PROCEEDED ACCORDING TO QRH PG E3-6
- [SDR OZCA202011190001](https://openairdocs.org/sdr/OZCA202011190001), Nov 16, 2020: UNKNOWN. HAZE. CREW REPORTED, ATOMIZED OIL HAZE IN COCKPIT UNABLE TO SEE OUTSIDE OF INSTRUMENTS, AFTER HP'S WERE TURNED ON AND RECIRCLE SWITCH. MAINTENANCE PERFORMED, INSPECTE
- [SDR OZCA202011060001](https://openairdocs.org/sdr/OZCA202011060001), Nov 2, 2020: SHAFT. SHEARED. 2020 NOV 2ND, N631BC (AS CSQ 726) FLYING FROM GRAND CAYMAN (MWCR) TO MIAMI (KMIA) EXPERIENCED AN UNSCHEDULED PROP FEATHERING AT ALTITUDE. CREW COMPLIED WITH QUI
- [SDR OZCA20200811001](https://openairdocs.org/sdr/OZCA20200811001), Aug 7, 2020: OIL SYSTEM. LOW PRESSURE. OIL LOW PRESSURE ON CWP AND FLIGHT CREW SHUT DOWN ENGINE IN CRUISE. SERVICED ENGINE OIL AND FILL QUANTITY EXCEEDED LIMITS IN CMM. ENGINE BEING REMOVED FOR EVALU
- [SDR OZCA202006290001](https://openairdocs.org/sdr/OZCA202006290001), Jun 26, 2020: ENGINE. SHUTDOWN. WHILE CONDUCTING FLIGHT CSQ702,ON 26JUN2020, UTILIZING AIRCRAFT N611BC THE LEFT HAND ENGINE DURING CLIMB AT 9000FT HAD AN UNCOMMANDED INFLIGHT SHUTDOWN. CREW RA
- [SDR OZCA2020033100000](https://openairdocs.org/sdr/OZCA2020033100000), Mar 24, 2020: PRESSURE SWITCH. FAULTY. FLIGHT CREW WRITE UP - AUTOCOARSEN FAILURE IN FLIGHT. LEFT ENG FEATHERED. "AUTOCOARSEN" CWP ILLUMINATED. LATER AFTER SPEAKING WITH CAPTAIN HE STATED THAT THE PR
- [SDR 2018FA0000501](https://openairdocs.org/sdr/2018FA0000501), Nov 30, 2018: SEAL. CRUSHED. STRONG ENGINE FUMES SMELL IN FLIGHT DECK. CORRECTIVE ACTION: INSPECTED AND FOUND LH ENGINE CONICAL SEALS CRUSHED AND AC GENERATOR DRIVE SHAFT BENT. R/R AC AC GE
- [SDR S9BA201707070003](https://openairdocs.org/sdr/S9BA201707070003), Jul 6, 2017: LINK. SEPARATED. DURING TAKE OFF, THE PROPELLER DID NOT FOLLOW CONDITION LEVER POSITION. THE LINK AT THE PROPELLER CONTROL UNIT WAS FOUND SEPARATED DUE TO A LOCK WASHER THAT FAI
- [SDR TSAA2016042519](https://openairdocs.org/sdr/TSAA2016042519), Apr 25, 2016: HMU. DAMAGED. ABORTED TAKEOFF DUE TO NR 2 ENG ISSUE NG, NP, TEMP HIGH ON NR 2 ENG WITH LITTLE TORQUE. NR 2 ENG DAMAGED DUCT GASKET REPLACED AT LOW PRESS BLEED CHECK VLV & PRS
- [SDR TSAA2016042018](https://openairdocs.org/sdr/TSAA2016042018), Apr 20, 2016: COUPLING. OUT OF POSITION. ABORTED TAKEOFF DUE TONR 2 ENG ISSUE. NG, NP, TEMP HIGH ON NR 2 ENG WITH VERY LITTLE TORQUE. FOUND BLEED LEAK AT LOW PRESS BLEED AIR CHECK VLV. RE-POSITION & RE
- [SDR 29GA2016041100001](https://openairdocs.org/sdr/29GA2016041100001), Apr 10, 2016: LIGHT. UNKNOWN. EMERGENCY LIGHT ARMED LIGHT ON F/A PANEL FLICKERED WHEN EMERGENCY LIGHTS WERE ARMED. PERFORMED OPS CHECK NO DEFECT NOTED IAW 33-50-60.
- [SDR 29GA2016041000001](https://openairdocs.org/sdr/29GA2016041000001), Apr 9, 2016: POWER SUPPLY. FAULTY. FORWARD DOOR EMERGENCY EXIT LIGHT DOSEN'T REMAIN ILLUMINATED ONCE EMERGENCY SWITCH ACTIVATED. T/S AND FOUND FWD EMERGENCY POWER SUPPLY AT FAULT, R & R FWD EMERG
- [SDR TSAA20151208006](https://openairdocs.org/sdr/TSAA20151208006), Dec 8, 2015: ENGINE. SHUTDOWN. ON LANDING ROLLOUT, NR 2 ENG SHUTDOWN AUTOMATICALLY. POWER LEVERS WERE INTO SLIGHT REVERSE WHEN NR 2 ENG FAILED. FOLLOWED FAULT ISOLATION MANUAL 71-00-00, VISUA
- [SDR TSAA20150929005](https://openairdocs.org/sdr/TSAA20150929005), Sep 29, 2015: ENGINE. FLAMED OUT. NUMBER 2 ENG FLAMED OUT AFTER POWER LEVER WAS BROUGHT TO FLIGHT IDLE UPON LANDING. CREW TAXIED CLEAR OF RNWY & COMPLETED ALL APPLICABLE CHECKLISTS & TAXIED TO P
- [SDR OZCA20150831018](https://openairdocs.org/sdr/OZCA20150831018), Aug 31, 2015: RELIEF VALVE. FAULTY. ABOUT 10 MINUTES AFTER TAKEOFF, RT ENG OIL TEMP WENT ABOVE RED LINE. REDUCED POWER & FOLLOWED QRH. TEMP SLOWLY STARTED TO REDUCE, OIL PRESS WAS 48 PSI. TROUBLE 
- [SDR OZCA20150710016](https://openairdocs.org/sdr/OZCA20150710016), Jul 10, 2015: WIRE. BROKEN. RIGHT SIDE PROPELLER OIL PRESSURE LIGHT CAME ON BETWEEN 0-25 PSI. TROUBLE SHOT PROBLEM & FOUND BROKEN WIRE AT RT SIDE PROPELLER GEAR BOX OIL PRESS TRANSDUCER. R
- [SDR S9BA201505280003](https://openairdocs.org/sdr/S9BA201505280003), May 27, 2015: SCOOP. MISSING. NR 1 ENGINE AC GENERATOR SCOOP MISSING, RAM AIR SCOOP.
- [SDR CA060609001](https://openairdocs.org/sdr/CA060609001), Mar 12, 2015: AXLE. LOOSE. (CAN) NR 4 MAIN WHEEL ASSEMBLY OBSERVED TO BE HOT TO THE TOUCH DURING ROUTINE MAINTENANCE. WHEN THE AIRCRAFT WAS JACKED TO INVESTIGATE THE CAUSE, THE WHEEL APPE
- [SDR TSAA20150206001](https://openairdocs.org/sdr/TSAA20150206001), Feb 6, 2015: TUBE. CRACKED. FLIGHT 5503, NR 1 ENG FAILED AT 8,000 FEET AFTER DEPARTING. NO INDICATIONS OF PROBLEMS BEFORE THE ENG FAILED. REPLACED CRACKED HMU P3 TUBE.
- [SDR OZCA201501160013](https://openairdocs.org/sdr/OZCA201501160013), Jan 16, 2015: HMU. MALFUNCTIONED. LEFT ENG FAILED ON LANDING ROLL AFTER USING MODERATE REVERSE THRUST. R & R LT ENG HMU IAW APPLICABLE MM. OPERATIONAL CHECKS SATISFACTORY.
- [SDR OZCA20140102012](https://openairdocs.org/sdr/OZCA20140102012), Jan 2, 2015: LATCH. OPEN. AFTER TAKEOFF RT COWLING LATCH POPPED OPEN. COWLING STAYED ATTACHED, LANDED WITHOUT INCIDENT. INSPECTED RT ENG COWLING & FOUND COWLING OTBD FWD LATCH OPEN. R & 
- [SDR OZCA20141211007](https://openairdocs.org/sdr/OZCA20141211007), Dec 11, 2014: GEARBOX. FAILED. ON APPROACH, RT ENG SURGED. RIGHT ENG OIL PRESS INDICATOR AT RED LINE. TROUBLE SHOT & FOUND RT ENG PROPELLER GEAR BOX CASE CRACKED DUE TO INTERNAL FAILURE. R & 
- [SDR OZCA20141029003](https://openairdocs.org/sdr/OZCA20141029003), Oct 29, 2014: CLAMP. LOOSE. TAKEOFF ABORTED AT 105 KT DUE TO RT ENG OVER TEMP INDICATION. INSPECTED RT ENG FOR BLEED LEAKS. FOUND RT PRIMARY BLEED TUBE & LOW PRESS BLEED TUBE CLAMPS LOOSE.
- [SDR OZCA20140922001](https://openairdocs.org/sdr/OZCA20140922001), Sep 19, 2014: CONTROL CABLE. DAMAGED. DURING FLIGHT CREW EXPERIENCED A LOSS OF THE NR 2 PROPELLER RPM. ACFT RETURNED BACK TO AIRPORT & LANDED SAFELY. INSPECTED THE ACFT & FOUND THE RT WING TO NACELL
- [SDR OZCA20140327001](https://openairdocs.org/sdr/OZCA20140327001), Mar 27, 2014: CONTROL BOX. FAULTY. RIGHT ENGINE FIRE WARNING, RETURNED TO AIRPORT. REPLACED RT FIRE DETECTOR CONTROL BOX WITH AN INSPECTED PART & ACFT WAS RELEASED TO SERVICE.
- [SDR OZCA20130905001](https://openairdocs.org/sdr/OZCA20130905001), Aug 30, 2013: SMOKE DETECTOR. DEFECTIVE. DURING A TURNBACK FOR AN OIL TEMP PROBLEM ON THE LT ENGINE, THE CARGO SMOKE LIGHT ILLUMINATED INTERMITTENTLY. NO SMOKE WAS DETECTED OR NOTICED. AN EMERGENCY WAS
- [SDR CA130816007](https://openairdocs.org/sdr/CA130816007), Aug 14, 2013: CABLE. FAILED. (CAN) CREW WENT TO PULL THE HANDLE TO SET THE PARKING BRAKE AND THE HANDLE SHEARED OFF THE CABLE.
- [SDR CA130409014](https://openairdocs.org/sdr/CA130409014), Mar 19, 2013: TUBE. LEAKING. (CAN) DURING CRUISE FLIGHT THE FLIGHT CREW NOTICED A LOW OIL PRESSURE INDICATION ON THE NR 2 ENGINE. THE CHECKLIST WAS FOLLOWED AND THE NR 2 ENGINE WAS SHUTDOWN
- [SDR CA130222008](https://openairdocs.org/sdr/CA130222008), Feb 20, 2013: TERMINAL BLOCK. OVERHEATED. (CAN) UPON SWITCHING ON THE AVIONICS MASTER PRIOR TO TAXIING OUT FOR TAKEOFF, A BURNING ODOR WAS NOTICED IN THE COCKPIT. THE AVIONICS SWITCH WAS TURNED OFF AND 
- [SDR CA130114004](https://openairdocs.org/sdr/CA130114004), Dec 19, 2012: SENSOR. MALFUNCTIONED. (CAN) DURING THE CLIMBOUT, THE CREW NOTED THAT THE NR 2 ENGINE OIL TEMPERATURE BEGAN TO INCREASE AND WAS READING HIGHER THAN NORMAL. IT CONTINUED TO INCREASE IN
- [SDR CA121130011](https://openairdocs.org/sdr/CA121130011), Nov 22, 2012: RECORDER. FAILED. (CAN) THE FDR WAS SENT OUT TO OBTAIN THE RECORDING FOR AN UNRELATED SYS FAILURE. WHEN THE AVIONICS SHOP ATTEMPTED TO READ THE FDR THEY FOUND THE FDR WAS NOT WOR
- [SDR CA121019008](https://openairdocs.org/sdr/CA121019008), Oct 19, 2012: SUPPORT BRACKET. CRACKED. (CAN) RIGHT ENGINE CONTROL CABLE SUPPORT BRACKET CRACKED AT FWD ATTACHMENT INBD.
- [SDR TSAA20121003006](https://openairdocs.org/sdr/TSAA20121003006), Oct 3, 2012: ENGINE. SURGES. ACFT HAD A LOW SPEED TAKEOFF ABORT (LESS THAN 80 KNOTS) DUE TO ENGINE SURGE.
- [SDR CA120419001](https://openairdocs.org/sdr/CA120419001), Apr 18, 2012: BEARING. FAILED. (CAN) DURING HEAVY INSPECTION, WITH THE AILERON CABLE TENSION SLACKED OFF, IT WAS NOTICED THAT THE RT AILERON BELLCRANK, IN THE WING, MOVEMENT WAS ROUGH AND NOI
- [SDR 2012F00061](https://openairdocs.org/sdr/2012F00061), Feb 24, 2012: LINE. CRACKED. ON APPROACH THE NR 2 ENGINE EXPERIENCED AN AUTOCOARSON PROBLEM AND A PERCAUTIONARY SHUTDOWN WAS PERFORMED. 
- [SDR TSAA2011112372012](https://openairdocs.org/sdr/TSAA2011112372012), Nov 23, 2011: OIL SYSTEM. LOW. ON TAKEOFF ROLL, THE LT ENGINE OIL WARNING LIGHT ILLUMINATED AT APPROX 90 KTS, ABORTED TAKEOFF ROLL AND RETURNED TO GATE WITHOUT FURTHER INCIDENCE. SERVICED NR1
- [SDR TSAA2011112372013](https://openairdocs.org/sdr/TSAA2011112372013), Nov 23, 2011: OIL SYSTEM. LOW. ON TAKEOFF ROLL, THE RT ENGINE OIL WARNING LIGHT ILLUMINATED AT APPROX 90 KTS. ABORTED TAKEOFF ROLL AND RETURNED TO GATE WITHOUT FURTHER INCIDENT. SERVICED NR2 
- [SDR CA111116004](https://openairdocs.org/sdr/CA111116004), Nov 15, 2011: ACM. SEIZED. (CAN) APPROXIMATELY 10 MINUTES AFTER DEPARTURE THE CREW NOTED AN ABNORMAL SMELL IN THE COCKPIT. THE RECIRC FANS WERE SUSPECT & WERE SELECTED TO OFF IAW THE CHEC
- [SDR CA111116005](https://openairdocs.org/sdr/CA111116005), Nov 10, 2011: PUMP. INTERMITTENT. (CAN) ON APPROACH THE CREW RECEIVED A HYD PRESS INDICATION ADVISORY WHEN THE LG WAS SELECTED. IAW CHECKLIST, THE LG WAS EXTENDED USING THE ALTERNATE SYS & ALL 3
- [SDR CA111116007](https://openairdocs.org/sdr/CA111116007), Oct 31, 2011: ICE SHIELD. LOOSE. (CAN) ON APPROACH THE FLIGHT CREW COULD HEAR AN ABNORMAL NOISE FROM THE EXTERIOR OF THE ACFT. ALL PARAMETERS & OPERATION OF THE ACFT WAS NORMAL & THE ACFT COMPL
- [SDR CA110602004](https://openairdocs.org/sdr/CA110602004), May 31, 2011: SWIVEL FITTING. CRACKED. ON CLIMB-OUT, DURING GEAR RETRACTION THE CREW NOTICED DECREASING HYDRAULIC PRESSURE, WHILE THE PUMP WAS RUNNING- INDICATING FLUID LOSS. THE ACFT RETURNED AND LA

All 450: https://openairdocs.org/engine/ge-ct7-5a2/reports.md

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