40 hp @ 8000rpm, quick start apu with tmd of t-62t-40lc-2, wimilar to 161331-135/-128, weight 169lbs.
A continuous combustion type engine. consists primarily of a compressor, nonaircraft gas turbine engine; chamber, combustion, nonaircraft gas turbine engine and a turbine assembly, nonaircraft gas turbine engine. it may have a fan section. air is compressed and heated by a combustible fuel and expanded through the turbine. it is designed to furnish a source of rotary shaft and/or pneumatic power. the pneumatic power is obtained by a bleedoff of the engine compressor. for a complete operating power unit, mounted on a base, see power unit, gas turbine engine.
Classification: Gas turbine engine, except aircraft nesoi, of a power not exceeding 5,000 kw
NSN 5905-00-271-3672
NSN 5835-01-561-2959
NSN 5925-01-101-7781
NSN 6240-01-497-3085
NSN 6130-00-901-5595
NSN 6220-01-052-3986
NSN 6645-01-063-8243
NSN 4140-01-113-2055
NSN 2925-00-887-2073
NSN 5935-00-657-1527
NSN 5905-00-771-0870
NSN 5930-01-344-0519