LTS101  
Initial Operational Capability (IOC): 1975
Total Production: 2,000
Also Known As: LTS101-850
Origin: United States of America
Corporations: Honeywell
Parent System: LTS101
Initial Operational Capability (IOC): 1975
Total Production: 2,000
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Description: The Honeywell LTS101 is a turboshaft engine designed to power light helicopters such as Bell 222, HH-65A, BK117, and AS350D. It develops between 650 and 850 shaft-horsepower (shp). Over 2,000 engines have been produced by Honeywell logging more than 3 million flight hourse since the LTS101 was certified in 1975.

LTS101 Applications


Private Aircraft AS350 Ecureuil AS365 Dauphin H410

LTS101 Specifications

Power
Max Output Power: 850 shp
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)

Operators & Related Equipment


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