Initial Operational Capability (IOC):
Total Production: 19,000
Also Known As: T53-L-138, T53-L-17 and T53-L-703
Origin: United States of America
Corporations: Honeywell
Parent System: T53
Initial Operational Capability (IOC):
Total Production: 19,000
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Description: The Honeywell T53 is a turboshaft engine designed to power rotary-wing aircraft applications. To date, more than 19,000 engines have been produced to power Bell UH-1H Huey, Huey II , AH-1F Cobra, Kaman K-Max and Fuji Bell 205B helicopters.

T53 Applications

Combat Aircraft AH-1W Super Cobra Private Aircraft K-MAX Support Aircraft UH-1N Huey

T53 Specifications

Max Power at TakeOff: 1,500 shp (1,119 kW)
Time Between Overhaul: 5,000 hour
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)

T53 News

There are 2 news between
8 Jan 2008 and 5 Jun 2008
Thursday, June 5, 2008Lockheed Martin and Kaman Aerospace Demonstrate Unmanned Supply Helicopter to US Army
Tuesday, January 8, 2008McTurbine Becomes Part of Bell Helicopter

Operators & Related Equipment


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