LTS101

Initial Operational Capability (IOC) : 1975
Total Production : 2,000

Model Status Year Produced
LTS101 Active 1975 2,000



LTS101

Group : Turboshaft Engines
Status : Active
Also Known As : LTS101-850 (version developing 850-shp)
Origin : United States of America
Contractor : Honeywell
Initial Operational Capability (IOC) : 1975
Total Production : 2,000

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.

Operators
Country Status State Notes
United States of AmericaActive ?
Specifications
Notes
Power
Max Output Power 850 shp

Notes

* Prime Contractor
State Latest Known holdings/Original Procurement
Com - Date of Commissioning
Decom - Date of Decommissioning

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