Initial Operational Capability (IOC): 1977
Total Production: 9,000
Also Known As: CT58, T58-GE-10 and T58-GE-8
Origin: United States of America
Corporations: General Electric Aviation
Parent System: T58
Initial Operational Capability (IOC): 1960
Total Production: 9,000
Family Members: TF58-GE-16A
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Description: The T58 engine was designed to power jet helicopters in the 50s. It has powered a full range of jet helicopters produced in the United States and overseas such as H-3 and H-46.

The T58-GE-16 engine was introduced in the late 70s powering the USMC's CH-46E helicopter.

T58-GE-16 Applications

Propulsion Systems TF58-GE-16A Support Aircraft CH-46D Sea Knight CH-46E Sea Knight SH-2G Super Seasprite SH-3 Sea King

T58-GE-16 Specifications

Max Power at TakeOff: 1,870 shp (1,395 kW)
Dry Weight: 113 kilogram (249 pound)
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)

T58-GE-16 News

There is 1 news
on 4 Apr 2007
Wednesday, April 4, 2007T58 Engine Family Celebrates 50 Years

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