Monday, September 08, 2008

LTS101

IOC: 1975
Total Production: 2,000

Also Known As: LTS101-850 (version developing 850-shp)

Origin:United States of America

Contractor/s: Honeywell

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.

Specifications
Power: Max Output Power 850 shp

Applications
AS350 Ecureuil, AS365 Internet Resources
honeywell.com

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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