Lycoming LTS101 explained
| LTS101 / LTP101 |
| National Origin: | United States |
| First Run: | 1960 |
The Lycoming (now Honeywell) LTS101 is a turboshaft engine family ranging from 650 to 850 shaft horsepower, used in a number of popular helicopters,[1] and, as the LTP101 turboprop, light aircraft. Both models carry the US military designation T702. The engine was originally designed at the Lycoming Turbine Engine Division in Stratford, Connecticut, but is now produced by Honeywell Aerospace.
Variants
- LTP101-600[2]
LTP101-700[3]
LTS101-600A-2
LTS101-600A-3
LTS101-600A-3A
LTS101-650B-1
LTS101-650B-1A
LTS101-650C-2
LTS101-650C-3
LTS101-650C-3A
LTS101-700D-2
LTS101-750A-1
LTS101-750B-2
LTS101-750C-1
LTS101-850B-2
T702
Applications
References
- Book: Gunston, Bill . World Encyclopedia of Aero Engines . 1986 . Patrick Stephens . Wellingborough . 96 .
External links
Notes and References
- Web site: Honeywell LTS101 . 2015-11-24 . https://web.archive.org/web/20160304095420/https://aerospace.honeywell.com/products/engines/lts101 . 2016-03-04 . dead .
- Web site: Textron Lycoming Turbine Engine Encyclopedia.com . 2026-02-28 . www.encyclopedia.com.
- Web site: Honeywell Achieves Longer Inspection Interval And Cost Reductions For Lts101 Operators . 2026-02-28 . aerospace.honeywell.com . en-US.