# Service difficulty reports: GE CT7-5A2

A list on [GE CT7-5A2](https://openairdocs.org/engine/ge-ct7-5a2.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 9 · 450 reports

- [SDR OZCA2025002641](https://openairdocs.org/sdr/OZCA2025002641.md): Downlock Switch · loose · May 31, 2025 · N641BC · Saab SF340A · Landing Gear Position and Warning
  > 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 ABORTED THE LANDING. A FLYBY PAST THE TOWER CONFORMED ALL 3 GEAR DOWN AND LOCKED. THE AIRCRAFT RETURNED
- [SDR OZCA2024091706641](https://openairdocs.org/sdr/OZCA2024091706641.md): Engine · erratic · Sep 16, 2024 · N641BC · Saab SF340A · Engine (Turbine/Turboprop)
  > 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 RIGHT ENGINE LOST POWER AND THE OVER TEMPERATURE LIGHT ILLUMINATED. CREW PERFORMED MEMORY ITEMS,AND
- [SDR OZCA2024004641](https://openairdocs.org/sdr/OZCA2024004641.md): Engine · overtemp · Aug 12, 2024 · N641BC · Saab SF340A · Engine (Turbine/Turboprop)
  > 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 SECONDS. TORQUE SET AT 40% THEN REDUCED TO 20%. ENGINE STABILIZED AROUND 30% TORQUE. AIRCRAFT DECLA
- [SDR OZCA20240219001](https://openairdocs.org/sdr/OZCA20240219001.md): Bleed Air Sys · loose · Feb 16, 2024 · N641BC · Saab SF340A · Engine Bleed Air System
  > 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 WITH HIGH RIGHT ITT. TURNED R HP OFF, ENGINE STABILIZED. MAINTENANCE INSPECTED BLEED SYSTEM AND FOU
- [SDR OZCA340076221212](https://openairdocs.org/sdr/OZCA340076221212.md): Trimmer · faulty · Dec 12, 2022 · N671BC · Saab SF340A · Engine EGT/TIT Indicating System
  > CROSSING 11,000 FT, RIGHT ENGINE ITT INCREASE UNCOMMANDED TO 872C (802C BEFORE INCREASE). PROCEEDED WITH QRH - REDUCING POWER POWER LEVERS BROUGHT TEMPERATURES BACK DOWN TO NORMAL LEVELS. BLEED VALVES HAD NO INFLUENCE ON ENGINE ITT. WHILE DESCENDING, ITT ON R
- [SDR OZCA340084221207](https://openairdocs.org/sdr/OZCA340084221207.md): Periseal · unserviceable · Dec 7, 2022 · N671BC · Saab SF340A · Cylinder Head Temperature (CHT) Indicating System
  > #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.md): Chip Detector · activated · Nov 3, 2022 · N651BC · Saab SF340A · Engine Oil Indicating System
  > 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 DETECTOR I/AW GE-CT-5 AMM 79-30-35-04. RUN AND LEAKS CHECK SATISFACTORY
- [SDR OZCA06102DEC2021](https://openairdocs.org/sdr/OZCA06102DEC2021.md): Hmu · faulted · Dec 2, 2021 · N631BC · Saab SF340A · Engine (Turbine/Turboprop)
  > 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 BOTTOMING GOVERNOR CONNECTED NP OVER SHOOTS 140 RPM NEED TO 1500 RPM AND RETURNED TO NORMAL READINGS. PRO
- [SDR OZCA340088211109](https://openairdocs.org/sdr/OZCA340088211109.md): Clamp · cracked · Nov 9, 2021 · N901BC · Saab SF340A · Engine Bleed Air System
  > 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. ON INVESTIGATION FOUND THAT THE HP BLEED LINE V-BAND CLAMP FAILED P/N 12J63-125 AT THE RETAINER SEGM
- [SDR OZCA90130MAR21](https://openairdocs.org/sdr/OZCA90130MAR21.md): Propeller · low pressure · Mar 30, 2021 · N901BC · Saab SF340A · Propeller Indication System
  > 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.md): Unknown · haze · Nov 16, 2020 · N651BC · Saab SF340A · Air Distribution System
  > CREW REPORTED, ATOMIZED OIL HAZE IN COCKPIT UNABLE TO SEE OUTSIDE OF INSTRUMENTS, AFTER HP'S WERE TURNED ON AND RECIRCLE SWITCH. MAINTENANCE PERFORMED, INSPECTED LT AND RT ACM'S FOR LEAKS AND OPERATIONS CHECK. INSPECTED LT AND RT ENGINE FOR INTERNAL OIL LEA
- [SDR OZCA202011060001](https://openairdocs.org/sdr/OZCA202011060001.md): Shaft · sheared · Nov 2, 2020 · N631BC · Saab SF340A · Propeller Feathering/Reversing
  > 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 QUICK REFERENCE HANDBOOK (QRH) AND EXECUTED AN ENGINE SHUTDOWN. CREW PRUDENTLY CONDUCTED AN EMERGENCY
- [SDR OZCA20200811001](https://openairdocs.org/sdr/OZCA20200811001.md): Oil System · low pressure · Aug 7, 2020 · N611BC · Saab SF340A · Engine Oil 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 EVALUATION.
- [SDR OZCA202006290001](https://openairdocs.org/sdr/OZCA202006290001.md): Engine · shutdown · Jun 26, 2020 · N611B · Saab SF340A · Engine (Turbine/Turboprop)
  > WHILE CONDUCTING FLIGHT CSQ702,ON 26JUN2020, UTILIZING AIRCRAFT N611BC THE LEFT HAND ENGINE DURING CLIMB AT 9000FT HAD AN UNCOMMANDED INFLIGHT SHUTDOWN. CREW RAN THE QRH AND ATTEMPTED A RESTART THAT WAS UNSUCCESSFUL. AIRCRAFT PERFORMED AN AIR RETURN TO PAP.
- [SDR OZCA2020033100000](https://openairdocs.org/sdr/OZCA2020033100000.md): Pressure Switch · faulty · Mar 24, 2020 · N681BC · Saab SF340A · Propeller Feathering/Reversing
  > FLIGHT CREW WRITE UP - AUTOCOARSEN FAILURE IN FLIGHT. LEFT ENG FEATHERED. "AUTOCOARSEN" CWP ILLUMINATED. LATER AFTER SPEAKING WITH CAPTAIN HE STATED THAT THE PROP DID NOT FEATHER IT WAS INDICATION ONLY.
- [SDR 2018FA0000501](https://openairdocs.org/sdr/2018FA0000501.md): Seal · crushed · Nov 30, 2018 · N631BC · Saab SF340A · Engine (Turbine/Turboprop)
  > 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 GENERATOR, FOUR CONICAL SEALS ON PGB, AND FUEL OIL HEATER IAW SAAB 340 AMM LEAK AND OPS CHECK OK.
- [SDR S9BA201707070003](https://openairdocs.org/sdr/S9BA201707070003.md): Link · separated · Jul 6, 2017 · N350CJ · Saab 340B · Propeller Controlling System
  > 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 FAILED.
- [SDR TSAA2016042519](https://openairdocs.org/sdr/TSAA2016042519.md): Hmu · damaged · Apr 25, 2016 · N845KH · Saab SF340A · Fuel Control/Turbine Engines
  > 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 & PRSOV IAW AMM 36-11-15-04 & 71-00-00-05, BUT OPERATION CHECK NG. R & R NR ENG HMU & ADJUSTED NR 2 ENG
- [SDR TSAA2016042018](https://openairdocs.org/sdr/TSAA2016042018.md): Coupling · out of position · Apr 20, 2016 · N845KH · Saab 340B · Pneumatic Distribution System
  > 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-TORQUED COUPLING IAW AMM 36-11-15. GND OPERATION CHECKED GOOD IAW AMM 71-00-00.
- [SDR 29GA2016041100001](https://openairdocs.org/sdr/29GA2016041100001.md): Light · unknown · Apr 10, 2016 · N347AG · Saab 340B · Emergency Lighting
  > 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.md): Power Supply · faulty · Apr 9, 2016 · N334AG · Saab 340B · Emergency Lighting
  > 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 EMERGENGY POWER SUPPLY ASSY IAW AMM 33-50-10-04. OPS CHK NORMAL.
- [SDR TSAA20151208006](https://openairdocs.org/sdr/TSAA20151208006.md): Engine · shutdown · Dec 8, 2015 · N845KH · Saab SF340A · Engine (Turbine/Turboprop)
  > 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, VISUALLY INSPECTED NR 2 ENG INLET FOR OBSTRUCTION & IGV RING & ACTUATING LINKAGE ASSEMBLY FOR DAMAGE.
- [SDR TSAA20150929005](https://openairdocs.org/sdr/TSAA20150929005.md): Engine · flamed out · Sep 29, 2015 · N845KH · Saab 340B · Engine (Turbine/Turboprop)
  > 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 PARKING WITHOUT INCIDENT. INSPECTED NR 2 ENG FOR FUEL LEAK, BUT NO FUEL LEAK NOTED. OPERATED NR 2
- [SDR OZCA20150831018](https://openairdocs.org/sdr/OZCA20150831018.md): Relief Valve · faulty · Aug 31, 2015 · N651BC · Saab SF340A · Engine Oil Temperature Regulator
  > 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 SHOT SYS & FOUND COLD OIL RELIEF VLV INOPERATIVE. R & R RT COLD OIL RELIEF VLV. GND OPERATIONAL
- [SDR OZCA20150710016](https://openairdocs.org/sdr/OZCA20150710016.md): Wire · broken · Jul 10, 2015 · N631BC · Saab SF340A · Engine Oil System Wiring
  > 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. REPAIRED WIRE IAW APPLICABLE MM. OPERATIONAL CHECKED SATISFACTORY.
- [SDR S9BA201505280003](https://openairdocs.org/sdr/S9BA201505280003.md): Scoop · missing · May 27, 2015 · N336S · Saab 340B · Nacelle/Pylon Miscellaneous Structure
  > NR 1 ENGINE AC GENERATOR SCOOP MISSING, RAM AIR SCOOP.
- [SDR CA060609001](https://openairdocs.org/sdr/CA060609001.md): Axle · loose · Mar 12, 2015 · Cessna 340A · Main Landing Gear Strut/Axle/Truck
  > (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 APPEARED TO BE LOOSE ON THE AXLE. THE WHEEL WAS REMOVED AND THE INNER WHEEL BEARING WAS FOUND TO HAVE BE
- [SDR TSAA20150206001](https://openairdocs.org/sdr/TSAA20150206001.md): Tube · cracked · Feb 6, 2015 · N843KH · Saab SF340A · Engine Fuel and Control
  > 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.md): Hmu · malfunctioned · Jan 16, 2015 · N671BC · Saab SF340A · Fuel Control/Turbine Engines
  > 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.md): Latch · open · Jan 2, 2015 · N691BC · Saab SF340A · Engine Cowling System
  > AFTER TAKEOFF RT COWLING LATCH POPPED OPEN. COWLING STAYED ATTACHED, LANDED WITHOUT INCIDENT. INSPECTED RT ENG COWLING & FOUND COWLING OTBD FWD LATCH OPEN. R & R RT ENG COWLING ASSEMBLY IAW MM.
- [SDR OZCA20141211007](https://openairdocs.org/sdr/OZCA20141211007.md): Gearbox · failed · Dec 11, 2014 · N691BC · Saab SF340A · Turbine Engine Reduction Gear
  > 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 & R PROPELLER GEAR BOX & POWER UNIT ASSEMBLY IAW MM. PERFORMED GND RUNS & LEAK CHECKS.
- [SDR OZCA20141029003](https://openairdocs.org/sdr/OZCA20141029003.md): Clamp · loose · Oct 29, 2014 · N691BC · Saab SF340A · Compressor Bleed Control
  > 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. SECURED CLAMPS AT BLEED TUBES IAW MAINTENANCE MANUALS. PERFORMED GND POWER RUNS. ALL POWER RUNS
- [SDR OZCA20140922001](https://openairdocs.org/sdr/OZCA20140922001.md): Control Cable · damaged · Sep 19, 2014 · N651BC · Saab SF340A · Engine Controls
  > 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 NACELLE CONTROL CABLE AT FAULT. AFFECTED CABLE WAS REPLACED. RIGGING CHECKS WERE SATISFACTORY & ENG RU
- [SDR OZCA20140327001](https://openairdocs.org/sdr/OZCA20140327001.md): Control Box · faulty · Mar 27, 2014 · N651BC · Saab SF340A · Fire Detection
  > 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.md): Smoke Detector · defective · Aug 30, 2013 · N661BC · Saab SF340A · Smoke Detection
  > 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 DECLARED. MX REPLACED CARGO ZONE B1 AND C2 SMOKE DETECTORS AND RELEASED. AFCF PERFORMED AND SE
- [SDR CA130816007](https://openairdocs.org/sdr/CA130816007.md): Cable · failed · Aug 14, 2013 · Saab SF340A · Landing Gear Brake System
  > (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.md): Tube · leaking · Mar 19, 2013 · Saab SF340A · Engine Oil Indicating System
  > (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. THE FLIGHT CREW ADVISED MAINTENANCE AND FLIGHT OPERATIONS AND RETURNED. AN INSPECTION WAS COMPL
- [SDR CA130222008](https://openairdocs.org/sdr/CA130222008.md): Terminal Block · overheated · Feb 20, 2013 · Saab SF340A · Light System Wiring
  > (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 THE PASSENGER DISSEMBARKED. MAINTENANCE INSPECTED THE ACFT AND FOUND THE ODOR TO BE COMING FROM T
- [SDR CA130114004](https://openairdocs.org/sdr/CA130114004.md): Sensor · malfunctioned · Dec 19, 2012 · Saab SF340A · Engine Oil Temperature
  > (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 INTO THE YELLOW ARC AND SHORTLY THEREAFTER TO THE REDLINE. ALL OTHER ENGINE PARAMETERS INCLUDING THE
- [SDR CA121130011](https://openairdocs.org/sdr/CA121130011.md): Recorder · failed · Nov 22, 2012 · Saab SF340A · Data Recorders (Flight/Maintenance)
  > (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 WORKING FOR ABOUT THE LAST 10HRS OF FLIGHT. THE LAST SCHEDULED MAINTENANCE THERE WAS A CORRELATION CHE
- [SDR CA121019008](https://openairdocs.org/sdr/CA121019008.md): Support Bracket · cracked · Oct 19, 2012 · Saab 340B · Power Lever
  > (CAN) RIGHT ENGINE CONTROL CABLE SUPPORT BRACKET CRACKED AT FWD ATTACHMENT INBD.
- [SDR TSAA20121003006](https://openairdocs.org/sdr/TSAA20121003006.md): Engine · surges · Oct 3, 2012 · N844KH · Saab SF340A · Engine (Turbine/Turboprop)
  > ACFT HAD A LOW SPEED TAKEOFF ABORT (LESS THAN 80 KNOTS) DUE TO ENGINE SURGE.
- [SDR CA120419001](https://openairdocs.org/sdr/CA120419001.md): Bearing · failed · Apr 18, 2012 · Saab SF340A · Aileron Control System
  > (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 NOISY. UPON REMOVAL FOR FURTHER INSPECTION, IT WAS DISCOVERED THAT THE 2 BEARINGS, PN MS27641-5 THAT SU
- [SDR 2012F00061](https://openairdocs.org/sdr/2012F00061.md): Line · cracked · Feb 24, 2012 · N651B · Saab SF340A · Engine Bleed Air System
  > ON APPROACH THE NR 2 ENGINE EXPERIENCED AN AUTOCOARSON PROBLEM AND A PERCAUTIONARY SHUTDOWN WAS PERFORMED.
- [SDR TSAA2011112372012](https://openairdocs.org/sdr/TSAA2011112372012.md): Oil System · low · Nov 23, 2011 · N843KH · Saab SF340A · Turbine Engine Oil System
  > 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 ENGINE OIL QUANTITY. ACFT RETURNED TO SERVICE.
- [SDR TSAA2011112372013](https://openairdocs.org/sdr/TSAA2011112372013.md): Oil System · low · Nov 23, 2011 · N843KH · Saab SF340A · Turbine Engine Oil System
  > 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 ENGINE OIL QUANTITY. ACFT RETURNED TO SERVICE.
- [SDR CA111116004](https://openairdocs.org/sdr/CA111116004.md): Acm · seized · Nov 15, 2011 · Saab SF340A · Cabin Cooling System
  > (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 CHECKLIST. THE SMELL DISSIPATED & THE FLIGHT CONTINUED. WITHIN 10 TO 15 MINUTES THE SMELL RETURNED IN
- [SDR CA111116005](https://openairdocs.org/sdr/CA111116005.md): Pump · intermittent · Nov 10, 2011 · Saab SF340A · Hydraulic Pump (Electric/Engine), Main
  > (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 GEAR INDICATED DOWN & LOCKED. THE ACFT HYD PRESS & QTY WAS VERIFIED & THE ACFT LANDED WITHOUT INC
- [SDR CA111116007](https://openairdocs.org/sdr/CA111116007.md): Ice Shield · loose · Oct 31, 2011 · Saab SF340A · Fuselage Main, Plate/Skin
  > (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 COMPLETED A NORMAL LANDING. A VISUAL INSPECTION BY THE CREW AFTER LANDING REVEALED A LIFTED SECTION OF
- [SDR CA110602004](https://openairdocs.org/sdr/CA110602004.md): Swivel Fitting · cracked · May 31, 2011 · Saab SF340A · Hydraulic System, Main
  > ON CLIMB-OUT, DURING GEAR RETRACTION THE CREW NOTICED DECREASING HYDRAULIC PRESSURE, WHILE THE PUMP WAS RUNNING- INDICATING FLUID LOSS. THE ACFT RETURNED AND LANDED UNEVENTFULLY. CAUSE OF THE PROBLEM WAS A FAILED DOWNLOCK ACTUATOR HYD SWIVEL FITTING. THE FI

Next page: https://openairdocs.org/engine/ge-ct7-5a2/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE engine_model_key = 'CT75A2'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/ge-ct7-5a2/reports

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