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 |
---|---|---|---|
![]() | Active | ? |
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
State Latest Known holdings/Original Procurement
Com - Date of Commissioning
Decom - Date of Decommissioning
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