- Manufacturer (registry)
- GE
- Model
- CT58
- Registry code
- 30001
- Installed in
- 1 registered aircraft
- Type
- Turbo-shaft
- Power
- 1,350 hp
Model codes come from the FAA registry’s reference file.
On this page
Airworthiness directives that may apply · 0
ADs whose products match this engine model. Each AD’s applicability may narrow it by serial number, part number or configuration.
No ADs matched this model
Registered aircraft · 1
Query with SQL
duckdb -csv -c "SELECT n_number, serial_number, year_manufactured, status, registrant_name, registrant_city, registrant_state
FROM 'https://openairdocs.org/data/latest/faa_aircraft_registration.parquet'
WHERE engine_model_code IN ('30001')
ORDER BY n_number"Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT n_number, serial_number, year_manufactured, status, registrant_name, registrant_city, registrant_state
FROM 'https://openairdocs.org/data/latest/faa_aircraft_registration.parquet'
WHERE engine_model_code IN ('30001')
ORDER BY n_numberRun it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
NTSB investigations
No NTSB investigations matched to aircraft with this engine modelMatched through the registry by N-number, so foreign aircraft and some older cases aren’t counted.
FAA incident reports
No reports matched to aircraft with this engine modelMatched through the registry by N-number, so foreign aircraft and some older reports aren’t counted.
Service difficulty reports · 14
SDR CHIRNC#24635Bearing · wornFCU UNIT RECEIVED FOR WARRANTY INSP/ TEST. CUSTOMER FAULT: N1/NG OVERSPEED “107%” OF THE #1 ENGINE. ENGINE ASSY INSTALLED ON TEST BED TO DIAGNOSE CAUSE OF THE OVERSPEED AND FOUND THE VARIABLE VANE SCHEDULE N1/NG 4201 RPM TOO FAST AT THE .75 DEGREE VANE ANGLSDR CA140221024Sleeve · worn(CAN) ON GEAR BOX INSTALLATION, THE FEMALE THREADS GAVE WAY AS LUBE FITTING WAS TIGHTENED. ACFT HAS DEVELOPED AN OPTIONAL REPLACEMENT PART WITH A STEEL INSERT TO PREVENT SUCH OCCURRENCE FROM HAPPENING, REF SB 61B35-50.SDR CA130516005Fcu · contaminated(CAN) METAL WAS FOUND IN THE FCU FILTER. UPON INSPECTION OF THE CFP EXTENSIVE RUBBING WAS FOUND. THIS CFP HAD ONLY BEEN INSTALLED FOR 26.7 HRS.SDR 3PRA2011092400001Fire Loop · false activationNR 2 ENGINE FIRE LIGHT ILLUMINATED DURING FLIGHT. MX FOUND THE AFT FIRE LOOP WIRE TO BE DEFECTIVE. REPLACED WITH NEW ELEMENT.SDR U0GA111150Uplock · obstructedAIRCRAFT DEPARTED OFFSHORE RIG BOUND TO A SHORE BASE, THE LANDING GEAR FAILED TO RETRACT. LOWERED THE LANDING GEAR HANDLE, GEAR HAD AN UNSAFE INDICATION. USED EMERGENCY BLOWDOWN HANDLE, GEAR SHOWED SAFE INDICATION. AIRCRAFT LANDED AT DESTINATION WITH NO FUSDR ERAA094067Blower · wornFAN RUBBING, WORN BEARINGS. SLIGHT FREE FLOAT OF BEARINGS OBSERVED, SIGNS OF RUBBING INDICATED IN A 1INCH PORTION OF OUTER HOUSING. PULLEY TO BE VERIFIED FOR ALIGNMENT UPON INSTALLATION ON AIRCRAFT. BEARINGS REPLACED WITH NEW. L GAP ADDRESSED WITH APPROPRSDR ERAA093690Actuator · leakingSTATOR VANE ACTUATOR IS LEAKING. OLD STYLE PISTON RINGS WERE BROKEN, U CUP SEAL DAMAGED. COMPLIED WITH SB-75-0025. DISASSEMBLED, CLEANED, INSPECTED, REASSEMBLED, AND TESTED UNIT.SDR 2003FA0000918Hose · crackedAIRCRAFT WAS ENROUTE FOR REDEPLOYMENT OF FIREFIGHTING CREWS. AIRCRAFT DEVELOPED A LARGE OIL LEAK AND MADE A PRECAUTIONARY LANDING. AIRCRAFT SUSTAINED NO DAMAGE AND OCCUPANTS WERE NOT INJURED. INVESTIGATION FOUND A MAIN TRANSMISSION OIL LINE HAD RUPTURED AT SDR ERAA087092Drive System · damagedUNIT MAKING GROWLING NOISE AND STICKING. WATER DAMAGE. REPLACED WATER DAMAGED MOTOR, REMOVED CORROSION, ALIGNED AND TESTED. COMPLIED WITH SERVICE LETTER SL-T-03-001.SDR ERAA087088Cable · inoperativeSCREEN IN INOPERATIVE (NOT COMING ON). FOUND DEFECTIVE CABLE ON DATA PROCESSING BOARD. REPLACED CABLE AND TESTED.SDR ERAA087090Receiver · failedRADAR DOES NOT PAINT RAIN. ONCE YOU'RE WITHIN 10 MILES OF VERY HEAVY RAIN, IT STARTS TO PAINT LIGHT RAIN.SDR CA011126002Nozzle · cracked(CAN) THE BAFFLE OF THE 3RD STAGE NOZZLE WAS REMOVED TO INVESTIGATE THE CAUSE OF AIR LEAKAGE. VISUAL AND NDT INSPECTION REVEALED CRACKS IN THE SHEET METAL OF THE SUMP ABOVE THE AIR TUBE LOCATION.TELCON WITH GE ON NOV. 21 REGARDING THE CRACKS AND THE LACK OF RSDR JYE2001F00000Cable · frayedTAIL ROTOR CABLE (PN S6140-65612-11) WAS FOUND BADLY FRAYED AND BROKEN AFTER PILOT MADE AN UNEVENTFUL LANDING, AT AN AIRPORT. THE PROBABLE CAUSE IS THE CABLE HAD BEEN ROUTED OVER THE CABLE GUARD PIN INSTEAD OF THE PULLEY. THE CABLE IS BEING SENT OUT FOR MESDR JYD2001F00005Hub · crackedFRONT HUB, PN 712701, SN 3V4170 FOUND CRACKED DURING OVERHAUL. COMPRESSOR WAS REMOVED FROM SERVICE DUE TO REACHING ITS OVERHAUL INTERVAL. DURING THE OVERHAUL INSPECTION, TWO CRACKS WERE DETECTED BY FLUORESCENT PENETRANT INSPECTION(FPI). 1ST CRACK LOCATION D
Query with SQL
duckdb -csv -c "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 = 'CT58' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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 = 'CT58' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.