T58
IOC: 1960
Total Production: 9,000
T58-GE-16
IOC: 1977
Also Known As:
CT58 (commercial derivative), T58-GE-10, T58-GE-8
Origin:United States of America
Contractor/s:
General Electric Aviation
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.
Specifications
Weights: Max Weight 113 kg (249 lb)
Power: Power 1,870 shp
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Notes
(*) lead contractor
IOC: Initial Operating Capability
FOC: Full Operating Capability
CEP: Circular Error Probable
Comm: Commissioning Date
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)
Last Updated: Sunday, August 24, 2008
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