# Service difficulty reports: GE CT7-8A

A list on [GE CT7-8A](https://openairdocs.org/engine/ge-ct7-8a.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 117 reports

- [SDR HEEA20261526001](https://openairdocs.org/sdr/HEEA20261526001.md): Sensor · unserviceable · Oct 13, 2026 · N935PH · Skrsky S92A · Turbine Engine Oil System
  > #1 ENG OIL BYPASS ILLUMINATED APPROX. 75 MINUTES INTO FLIGHT.
- [SDR U0GA2025120418345](https://openairdocs.org/sdr/U0GA2025120418345.md): Unknown · odor · Dec 3, 2025 · N524PB · Skrsky S92A · Air Distribution System
  > AFTER LEVELING OFF FROM TAKEOFF WE STARTED NOTICING THE SMELL OF FUEL WHICH SEEMED TO BE COMING FROM THE CABIN AREA OF THE AIRCRAFT. INITIALLY WE TURNED OFF THE HEAT AND SELECTED OUTSIDE AIR FOR THE CABIN AND COCKPIT. WE TRIED DIFFERENT COMBINATIONS OF BLEED A
- [SDR HEEA202501310001](https://openairdocs.org/sdr/HEEA202501310001.md): Plate · cracked · Jan 27, 2025 · N949PH · Skrsky S92A · Engine (Turbine/Turboprop)
  > DURING DEPARTURE FROM MC782/DEEPWATER POSEIDON THE AIRCRAFT EXPERIENCED AN UN-COMMANDED, INFLIGHT SHUTDOWN OF THE #1 ENGINE. THE AIRCREW FOLLOWED THE CHECKLIST EMERGENCY PROCEDURE AND LANDED AT HOUMA WITHOUT FURTHER INCIDENT.
- [SDR U0GA2024091314429](https://openairdocs.org/sdr/U0GA2024091314429.md): Wire Harness · damaged · Sep 13, 2024 · N145JW · Skrsky S92A · Fire Protection System Wiring
  > FIRE LIGHT FLASHES INTERMITTENTLY WITH NO AUDIO OR CAPTION LIGHT.: REMOVED AND REPLACED #2 ENGINE OUTBOARD FLAME DETECTOR HARNESS. OPERATIONAL CHECK GOOD.
- [SDR U0GA2024091314412](https://openairdocs.org/sdr/U0GA2024091314412.md): Fire Detector · contaminated · Sep 10, 2024 · N145JW · Skrsky S92A · Fire Detection
  > FIRE #2 ENG CAUTION AND AUDIO ACTIVATED DURING HEAVY RAIN AND STAYED "ON". FOUND WATER ON JUNCTION OF #2 INBOARD FIRE DETECTOR CONNECTOR HARNESS. CLEANED AND DRIED OUT CONNECTOR. OPS CHECK GOOD ON GROUND AT THIS TIME. ALL WORK PERFORMED IAW REF. S92 WIRING S
- [SDR U0GA2024090914391](https://openairdocs.org/sdr/U0GA2024090914391.md): Connector · contaminated · Sep 8, 2024 · N145JW · Skrsky S92A · Fire Protection System Wiring
  > FIRE #2 ENGINE CAUTION LIGHT AND AUDIO WARNING ON FOR ONE MINUTE IN RAIN. INSPECTED #2 FIRE DETECTOR WIRE HARNESS AND DRIED CONNECTORS. TESTED SATISFACTORY. TL-265449-2024
- [SDR U0GA 202409014384](https://openairdocs.org/sdr/U0GA%20202409014384.md): Connector · dirty · Sep 7, 2024 · N145JW · Skrsky S92A · Fire Protection System Wiring
  > NO #2 ENGINE FIRE LIGHT ILLUMINATED IN FLIGHT 10 MINUTES AFTER TAKE-OFF. CLEANED ALL ELECTRICAL CONNECTORS ON FLAME DETECTOR AND UPPER DECK. FIRE LIGHT WENT OFF, TESTED SATISFACTORY. TL-265393-2024
- [SDR U0GA2024090914385](https://openairdocs.org/sdr/U0GA2024090914385.md): Connector · dirty · Sep 7, 2024 · N524PB · Skrsky S92A · Fire Protection System Wiring
  > NO 2 ENGINE FIRE LIGHT ILLUMINATED IN HEAVY RAIN FOR 3 SECONDS WITH NO AUDIO WARNING. CLEANED #2 ENGINE FIRE DETECTOR CANNON PLUGS. OPS CHECK GOOD. REF. S92A AMM CHAPTER 26. TL-265397-2024
- [SDR HEEA202407260001](https://openairdocs.org/sdr/HEEA202407260001.md): Engine · making metal · Jul 25, 2024 · N945PH · Skrsky S92A · Engine (Turbine/Turboprop)
  > #2 ENGINE CHIP CAUTION LIGHT ON.
- [SDR U0GA2024030612717](https://openairdocs.org/sdr/U0GA2024030612717.md): Fire Detector · faulted · Mar 5, 2024 · N524PB · Skrsky S92A · Fire Detection
  > OUTBOUND LEVEL AT 3000' THE AIRCRAFT BEGAN TO GIVE INTERMITTENT APU FIRE WARNINGS. THE AIRCRAFT WAS TURNED BACK TO RETURN TO BASE AND THE FIRE WARNINGS STOPPED APPROXIMATELY 5 MINUTES AFTER IT HAD BEGUN. WHILE ON APPROACH WHEN THE AIRCRAFT ENTERED CLOUDS THE W
- [SDR U0GA202402020001](https://openairdocs.org/sdr/U0GA202402020001.md): Unknown · odor · Feb 2, 2024 · N920VH · Skrsky S92A · Air Distribution System
  > WHILE ENROUTE TO GC468 ON HAA TASKING CREW STATED THAT THEY HAD A STRONG INDICATION OF FUEL SMELL. THE ODOR INCREASED AND CREW STATED THAT THEY WERE HAVING NEGATIVE EFFECTS ON VISION, NAUSEA AND HEADACHES. VISUAL OBSERVATION OF LEAKING FUEL UNDER MEDIC SEAT AF
- [SDR 2023F00288](https://openairdocs.org/sdr/2023F00288.md): Detector · inoperative · Sep 25, 2023 · N592PH · Skrsky S92A · Engine Oil System (Airframe Furnished)
  > DURING CRUISE, #1 ENGINE OIL TEMPERATURE WENT INTO THE YELLOW. RTB VIA OEI PROFILE TERMINATING AT HBP
- [SDR 2022F00507](https://openairdocs.org/sdr/2022F00507.md): Seal · failed · Dec 19, 2022 · N936PH · Skrsky S92A · Engine (Turbine/Turboprop)
  > #1 ENGINE OIL PRESSURE LOW NOTED DURING CRUISE CHECK. CANCELLED IFR AND RETURNED TO LAND RW18 AT KHUM. #1 ENGINE WAS BROUGHT BACK TO IDLE AS PER CHECKLIST AND RETURNED TO FLY ON FINAL FOR LANDING. #1 ENGINE B-AXIS SEAL BLOWN OUT.
- [SDR 2022F00236](https://openairdocs.org/sdr/2022F00236.md): Fire Detector · inoperative · May 20, 2022 · N950PH · Skrsky S92A · Fire Protection System
  > #2 FIRE LIGHT ILLUMINATED ON CLIMB OUT. DECLARED AN EMERGENCY AND RETURNED TO KHUM. SHUT DOWN ENGINE #2 AFTER LANDING AND TAXIED TO PARKING.
- [SDR HEEA202209190370](https://openairdocs.org/sdr/HEEA202209190370.md): Fire Detector · false indication · May 20, 2022 · N950PH · Skrsky S92A · Fire Detection
  > ENGINE #2 FIRE LIGHT ILLUMINATED ON CLIMB OUT. DECLARED AN EMERGENCY AND RETURNED TO KHUM. SHUT DOWN ENGINE #2 AFTER LANDING AND TAXIED TO PARKING.
- [SDR HEEA202209190368](https://openairdocs.org/sdr/HEEA202209190368.md): Fire Detector · false indication · Feb 19, 2022 · N945PH · Skrsky S92A · Fire Detection
  > SHORTLY AFTER DEPARTING DGTK AT CRUISE FLIGHT, A "FIRE ENGINE 1" AUDIO OCCURRED WITH NO FIRE LIGHT. REDUCED AIRSPEED AND REDUCED ENG 1 THROTTLE TO IDLE. IN THAT TIME FRAME SYMPTOMS DISAPPEARED AND NO INDICATIONS OF ABNORMAL OPERATION. CONCURRENTLY BEGAN TURN B
- [SDR HEER201911071414](https://openairdocs.org/sdr/HEER201911071414.md): Switch · inoperative · Nov 1, 2019 · N937PH · Skrsky S92A · Main Rotor Drive System
  > IN CRUISE FLIGHT AT 3000 FEET MGB BYPASS AND MGB PRESSURE LIGHTS ILLUMINATED. REPLACED MGB BYPASS TOGGLE SWITCH, REPAIRED WIRE TO MAIN TRANSMISSION LOW OIL PRESSURE SWITCH CANNON PLUG @ P417.
- [SDR HEER201910217365](https://openairdocs.org/sdr/HEER201910217365.md): Oil System · low · Oct 17, 2019 · N943PH · Skrsky S92A · Turbine Engine Oil System
  > #1 ENGINE OIL PRESSURE LOW CAUTION ILLUMINATED IN FLIGHT. CHECKED THE ENGINE OIL LEVEL AND FOUND TO BE 2.5 QUARTS LOW. THE HUMS DOWNLOAD SHOWED THAT THE OIL PRESSURE DROPPED TO 20 PSI WHILE THE THROTTLE WAS ABOVE IDLE.
- [SDR CA190517007](https://openairdocs.org/sdr/CA190517007.md): Strut · malfunctioned · May 9, 2019 · Skrsky S92A · Main Landing Gear Strut/Axle/Truck
  > (CAN) THE LANDING GEAR OLEOS IN THE S92A UTILIZE A FLOATING PISTON DESIGN AND IT IS VERY SUSCEPTIBLE TO IMBALANCE OF NITROGEN AND HYDRAULIC FLUID. THE INCORRECT GEAR INDICATION WAS DRIVEN BY A LOW LEFT HAND (L/H) SHOCK STRUT SERVICING, CAUSING A LACK OF WOW SI
- [SDR CA190312014](https://openairdocs.org/sdr/CA190312014.md): Gearbox · making metal · Mar 8, 2019 · Skrsky S92A · Main Rotor Gearbox
  > (CAN) FLIGHT CREW RECEIVED A MASTER CAUTION LIGHT WARNING ADVISING THEM OF METAL CHIP DETECTION ON #2 INPUT MODULE GEAR BOX. AIRCRAFT RETURNED TO BASE. CHIP DETECTORS, STRAINERS, AND FILTERS VERIFIED. FOUND METAL PARTICLES ON #2 INPUT MODULE GEAR BOX AND MAIN
- [SDR CA190307015](https://openairdocs.org/sdr/CA190307015.md): Hanger Assy · damaged · Mar 4, 2019 · Skrsky S92A · Tail Rotor Drive Shaft
  > (CAN) DURING THE REVIEW OF THE HUMS DATA DIRECTLY FOLLOWING THE AIRCRAFT`S RETURN FROM AN OFFSHORE FLIGHT, A HANGER BEARING 2 TEMPERATURE EXCEEDANCE WAS DISPLAYED. UPON FURTHER INTERROGATION, IT WAS FOUND THAT THE BEARING HAD EXPERIENCED A LEVEL 1 EXCEEDANCE,
- [SDR HEER201812143469](https://openairdocs.org/sdr/HEER201812143469.md): Connector · contaminated · Dec 13, 2018 · N951PH · Skrsky S92A · Fire Protection System Wiring
  > #1 ENGINE FIRE LIGHT ILLUMINATED IN FLIGHT. FOUND EXCESSIVE WATER IN #1 ENGINE AFT FIRE DETECTOR CONNECTORS.
- [SDR HEER201811165403](https://openairdocs.org/sdr/HEER201811165403.md): Compressor · stalled · Nov 15, 2018 · N940PH · Skrsky S92A · Turbine Engine Compressor Section
  > #2 ENGINE FAILED FOLLOWING A COMPRESSOR STALL. REPLACED #2 ENGINE DUE TO COMPRESSOR BLADES DAMAGED.
- [SDR HEER20180228864](https://openairdocs.org/sdr/HEER20180228864.md): Arm · broken · Feb 28, 2018 · N948PH · Skrsky S92A · Turbine Engine Compressor Section
  > ENGINE REMOVED 2-28-18 DUE TO BROKEN LEVER ARM. REPLACED LEVER ARM AND RETURNED TO SERVICE.
- [SDR HEER20180228865](https://openairdocs.org/sdr/HEER20180228865.md): Arm · broken · Feb 28, 2018 · N946PH · Skrsky S92A · Turbine Engine Compressor Section
  > ENGINE REMOVED 9-27-17 DUE TO BROKEN LEVER ARM. REPLACED LEVER ARM AND RETURNED TO SERVICE.
- [SDR HEER20180228866](https://openairdocs.org/sdr/HEER20180228866.md): Arm · broken · Feb 28, 2018 · N948PH · Skrsky S92A · Turbine Engine Compressor Section
  > ENGINE REMOVED 6-27-16 DUE TO BROKEN LEVER ARM. REPLACED LEVER ARM AND RETURNED TO SERVICE.
- [SDR HEER20180228867](https://openairdocs.org/sdr/HEER20180228867.md): Arm · broken · Feb 28, 2018 · N928PH · Skrsky S92A · Turbine Engine Compressor Section
  > ENGINE REMOVED 9-4-15 DUE TO BROKEN LEVER ARM. REPLACED LEVER ARM AND RETURNED TO SERVICE.
- [SDR HEER20180228868](https://openairdocs.org/sdr/HEER20180228868.md): Arm · broken · Feb 28, 2018 · N943PH · Skrsky S92A · Turbine Engine Compressor Section
  > ENGINE REMOVED 6-24-17 DUE TO BROKEN LEVER ARM. REPLACED LEVER ARM AND RETURNED TO SERVICE.
- [SDR HEER20180228869](https://openairdocs.org/sdr/HEER20180228869.md): Arm · broken · Feb 28, 2018 · N924PH · Skrsky S92A · Turbine Engine Compressor Section
  > ENGINE REMOVED 9-5-14 DUE TO BROKEN LEVER ARM. REPLACED LEVER ARM AND RETURNED TO SERVICE.
- [SDR HEER20180228870](https://openairdocs.org/sdr/HEER20180228870.md): Arm · broken · Feb 28, 2018 · N892PH · Skrsky S92A · Turbine Engine Compressor Section
  > ENGINE REMOVED 6-2-12 DUE TO BROKEN LEVER ARM. REPLACED LEVER ARM AND RETURNED TO SERVICE.
- [SDR CA180104001](https://openairdocs.org/sdr/CA180104001.md): Damper · delaminated · Jan 3, 2018 · Skrsky S92A · Main Rotor Head
  > (CAN) REPLACEMENT MAIN ROTOR DAMPER RECEIVED FROM A SUPPLIER. FORM 8130 INDICATED STATUS: `OVERHAULED` (COPY OF 8130 ATTACHED). UPON CLOSER INSPECTION, BEARING WAS FOUND TO BE DE-LAMINATED (SEE ATTACHED PHOTOS SHOWING CENTER BUSING DE-LAMINATED FROM ELASTOME
- [SDR HEER20170915622](https://openairdocs.org/sdr/HEER20170915622.md): Engine · making metal · Sep 15, 2017 · N936PH · Skrsky S92A · Engine (Turbine/Turboprop)
  > NR 2 ENGINE CHIP LIGHT ILLUMINATED. FOUND METAL ON CHIP PLUGS. REPLACED THE NR 2 ENGINE.
- [SDR HEER20170502216](https://openairdocs.org/sdr/HEER20170502216.md): Transducer · fluctuates · May 2, 2017 · N944PH · Skrsky S92A · Engine Oil Pressure
  > NR 2 ENGINE OIL PRESSURE CLIMBED INTO THE RED RANGE, THEN FLUCTUATED. BROUGHT ENGINE TO IDLE IN CRUISE AND RETURNED TO FLY POSITION FOR LANDING. HUMS DATA REVIEWED AND PRESSURE TRANSDUCER VERY ERRATIC. REPLACED TRANSDUCER.
- [SDR HEER20160918235](https://openairdocs.org/sdr/HEER20160918235.md): Fire Detector · false indication · Sep 18, 2016 · N941PH · Skrsky S92A · Fire Detection
  > INTERMITTENT FIRE LIGHT AND AURAL ON NR 1 ENGINE. TESTED THE NR 1 ENGINE FIRE DETECTION SYSTEM IAW S92A-AMM-000 TASK 26-11-00710-001 REV. 33. CHECKED GOOD. INSPECTED INBOARD AND OUTBOARD DETECTORS WIRING AND CONNECTORS, NO DEFECTS NOTED. FAULT COULD NOT BE
- [SDR HEER20160813057](https://openairdocs.org/sdr/HEER20160813057.md): Fire Detector · malfunctioned · Aug 13, 2016 · N939PH · Skrsky S92A · Fire Detection
  > INTERMITTENT FIRE LIGHT AND WOULD NOT TEST. REPLACED FLAME DETECTOR NR 1 ENGINE OUTBOARD. FUNCTIONAL TESTED GOOD.
- [SDR JTAA2016FA0000026](https://openairdocs.org/sdr/JTAA2016FA0000026.md): Bearing · corroded · Jan 21, 2016 · N901CH · Skrsky S92A · Standard Practices/Structures
  > WHEN REMOVING BEAM, LT AND RT SIDES, IT WAS FOUND THAT BOTH OTBD BEARINGS WERE SEVERELY CORRODED. RT BEARING WAS SEIZED WITH NO VISIBLE INDICATIONS OF SEIZURE AND LT 1 WAS STIFF WITH RUST COMING OUT OF BEARING SEALS.
- [SDR JTAA2016FA0000021](https://openairdocs.org/sdr/JTAA2016FA0000021.md): Bushing · broken · Jan 15, 2016 · N901CH · Skrsky S92A · Main Rotor Gearbox
  > DURING REMOVAL OF MAIN ROTOR GEARBOX, THE FWD AND REAR MGB MOUNT BOLTS AND SLEEVE BUSHINGS WERE REMOVED. 3 OF THE 4 SLEEVE BUSHINGS WERE FOUND TO BE COMPLETELY BROKEN, WITH THE 4TH CRACKED APPROXIMATELY 75 PERCENT OF THE CIRCUMFERENCE OF THE BUSHING IN THE SA
- [SDR CA160115008](https://openairdocs.org/sdr/CA160115008.md): Sleeve · broken · Jan 15, 2016 · Skrsky S92A · Main Rotor Transmission Mount
  > (CAN) DURING REMOVAL OF MAIN ROTOR GEARBOX, THE FORWARD AND REAR MGB MOUNT BOLTS AND SLEEVE BUSHINGS WERE REMOVED, 3 OF THE 4 SLEEVE BUSHINGS WERE FOUND TO BE COMPLETELY BROKEN, WITH THE 4TH CRACKED APPROXIMATELY 75 PERCENT OF THE CIRCUMFERENCE OF THE BUSHING
- [SDR CA160115009](https://openairdocs.org/sdr/CA160115009.md): Bearing · corroded · Jan 15, 2016 · Skrsky S92A · Rotorcraft Flight Control
  > (CAN) WHEN REMOVING BEAM, PN 92400-02212-101, LT AND RT SIDES, IT WAS FOUND THAT BOTH OTBD BEARINGS WERE SEVERELY CORRODED. RT BEARING WAS SEIZED WITH NO VISIBLE INDICATIONS OF SEIZURE AND LT 1 WAS STIFF WITH RUST COMING OUT OF BEARING SEALS.
- [SDR CA160118008](https://openairdocs.org/sdr/CA160118008.md): Bearing · failed · Dec 28, 2015 · Skrsky S92A · AC Generator-Alternator
  > (CAN) UNCOMMANDED APU SHUTDOWN. DURING START, THE ENGINEER COMMENTED THE APU DID NOT SOUND NORMAL. CHECKING THE PARAMETERS PAGE AND HEALTH PAGE CONFIRMED APU PARAMETERS TO BE NOMINAL AND HEALTH INDICATORS TO BE GREEN. APU THEN SHUTDOWN. NO SIGHS OF SMOKE OR
- [SDR CA151027004](https://openairdocs.org/sdr/CA151027004.md): Float · ruptured · Oct 19, 2015 · Skrsky S92A · Wheel/Ski/Float
  > (CAN) THIS IS THE 6TH INSTANCE OF AFT FLOAT BAG RUPTURE DURING ANNUAL INSPECTION AND INFLATION TEST. THIS IS THE SECOND SDR SUBMISSION FOR THIS ISSUE. I DID NOT MENTION ON THE ORIGINAL SDR THAT THE AFT FLOAT INFLATION TEST AS DESCRIBED IN THE CMM WAS ORIGINAL
- [SDR CA151013004](https://openairdocs.org/sdr/CA151013004.md): Fuel Sys · contaminated · Oct 6, 2015 · Skrsky S92A · Aircraft Fuel System
  > (CAN) ON ARRIVAL AT THE PLATFORM, WHILE DESCENDING FROM THE HOVER ONTO THE DECK, THE NR 2 FUEL BYPASS CAUTION CAME ON. ONCE ON THE DECK, APPROXIMATELY 7 SECONDS LATER, NR 1 FUEL BYPASS CAUTION ALSO CAME ON. FOLLOWING SHUTDOWN AND DISCUSSION WITH MAINTENANCE
- [SDR CA150811011](https://openairdocs.org/sdr/CA150811011.md): Bypass Switch · failed · Aug 8, 2015 · Skrsky S92A · Turbine Engine Oil System
  > (CAN) WHILE IN CRUISE FLIGHT, ENROUTE TO AN OFFSHORE PLATFORM, THE NR 2 ENGINE OIL BYPASS CAUTION LIGHT CAME ON. EMERGENCY CHECKLIST ACTIONS WERE CARRIED OUT AND THE ACFT RETURNED TO DEPARTURE WITHOUT FURTHER ISSUE. TROUBLESHOOTING DETERMINED THE BYPASS SWITC
- [SDR CA150817013](https://openairdocs.org/sdr/CA150817013.md): Frame · cracked · Aug 3, 2015 · Skrsky S92A · Fuselage Main, Frame
  > (CAN) DURING THE INCORPORATION OF SSI-92-074 A CRACK WAS DISCOVERED IN HOLE 48 USING EDDY CURRENT INSPECTION. ACFT MFG WAS CONTACTED AND NOW THE FRAMES 328 AND 361 WILL REQUIRE REPLACEMENT.
- [SDR CA150811012](https://openairdocs.org/sdr/CA150811012.md): Float · ruptured · Jul 15, 2015 · Skrsky S92A · Wheel/Ski/Float
  > (CAN) WE HAVE HAD 5 INSTANCES OF AFT FLOTATION BAGS RUPTURING DURING ANNUAL FUNCTIONAL TESTING. DURING THE TEST THE FLOAT IS INFLATED TO 3.5 PSI AND IT IS DURING THIS TEST STAGE THAT THE FLOATS ARE RUPTURING. THIS RENDERS THE FLOAT BAGS AS SCRAP AND ARE NOT R
- [SDR CA150714009](https://openairdocs.org/sdr/CA150714009.md): Spline Adapter · mismanufactured · Jul 9, 2015 · Skrsky S92A · Main Rotor Gearbox
  > (CAN) THE VESPEL SPLINE ADAPTERS SHOULD SLIDE OVER THE LUBE/SCAVENGE PUMP SPLINE SMOOTHLY BUT SNUGLY. ON REPLACING BOTH SPLINE ADAPTERS ON 1 OF OUR AIRCRAFT, IT WAS DISCOVERED THAT 5 SPLINE ADAPTERS NEW, FROM STORES WOULD FETCH UP AND NOT SMOOTHLY SLIDE OVER
- [SDR CA150714010](https://openairdocs.org/sdr/CA150714010.md): Actuator · interference · Jun 5, 2015 · Skrsky S92A · Landing Gear Actuator
  > (CAN) THE ACFT HAD FINISHED ITS FLIGHT SCHEDULE AND MAINTENANCE WAS PREPARING TO TOW IT INTO THE HANGAR, THE GEAR PIN COULD NOT BE INSERTED INTO THE NLG RETRACTION ACTUATOR. IT IS NOT SAFE TO BE UNDER THE HELICOPTER OR TO TOW IT WITHOUT GEAR PIN INSERTION, SO
- [SDR HEER20150322879](https://openairdocs.org/sdr/HEER20150322879.md): Fire Detector · false activation · Mar 22, 2015 · N792PH · Skrsky S92A · Fire Detection
  > NR 2 ENGINE LIGHT CAME ON IN HOVERING PRIOR TO TAKE OFF. REPLACED THE NR 2 ENGINE AFT FLAME DETECTOR AND HARNESS ASSEMBLY.
- [SDR CA150305006](https://openairdocs.org/sdr/CA150305006.md): Module · unserviceable · Feb 22, 2015 · Skrsky S92A · Main Rotor Gearbox
  > (CAN) UPON LANDING AT THE PLATFORM, THE NR 1 INPUT MODULE CHIP CAUTION ILLUMINATED. THE ACFT WAS THEN SHUTDOWN & SECURED. MX TEAM ARRIVED LATER THAT DAY & UPON INSPECTION OF THE NR 1 MODULE CHIP DETECTOR FOUND 4 SMALL RIVET HEADS. AMM DICTATES NO FURTHER FL
- [SDR CA150203002](https://openairdocs.org/sdr/CA150203002.md): Fmu · failed · Jan 27, 2015 · Skrsky S92A · Fuel Control/Turbine Engines
  > (CAN) ON THE GROUND FOLLOWING FLIGHT, THE THROTTLES WERE MOVED FROM THE "FLIGHT" POSITION BACK TO "IDLE". DIRECTLY FOLLOWING, A NR 2 ENGINE OUT AUDIO WAS HEARD AND A RED ENGINE OUT LIGHT WAS OBSERVERED ON THE INSTRUMENT PANEL, MOMENTARILY. TROUBLESHOOTING LED

Next page: https://openairdocs.org/engine/ge-ct7-8a/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 = 'CT78A'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/ge-ct7-8a/reports

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