NSN 2835-01-345-3402

Part Details | NONAIRCRAFT GAS TURBINE ENGINE

2835-01-345-3402 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.

Alternate Parts: 161331135, 161331-135, 2835-01-345-3402, 01-345-3402, 2835013453402, 013453402

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
28SEP 17, 199101-345-340250489 ( ENGINE, GAS TURBINE, NONAIRCRAFT )
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2835-01-345-3402
Part Number Cage Code Manufacturer
161331-13555820UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY
Technical Data | NSN 2835-01-345-3402
Characteristic Specifications
FUEL TYPE JET FUEL
POWER OUTPUT FOR WHICH DESIGNED SHAFT
MOUNTING TYPE AIRCRAFT
OVERALL LENGTH38.800 INCHES NOMINAL
OVERALL HEIGHT24.400 INCHES NOMINAL
OVERALL WIDTH17.600 INCHES NOMINAL
REFERENCE DATA AND LITERATUREAIR FORCE TO. 2G-T62T-44
SPECIAL FEATURES110 SHAFT HP @ 64643RPM. APU IS SIMILAR TO P/N 161331-121/-128 EXCEPT UPDGRADED BY ECP-007R1C1. TMD IS T-62T-40LC-2. WEIGHT 186LBS.
TEST DATA DOCUMENT55820-ECPT-62T-40LC-2-007R1C1 SPECIFICATION (INCLUDES ENGINEERING TYPE BULLETINS, BROCHURES,ETC., THAT REFLECT SPECIFICATION TYPE DATA IN SPECIFICATION FORMAT; EXCLUDES COMMERCIAL CATALOGS, INDUSTRY DIRECTORIES, AND SIMILAR TRADE PUBLICATIONS, REFLECTING GENERAL TYPE DATA ON CERTAIN ENVIRONMENTAL AND PERFORMANCE REQUIREMENTS AND TEST CONDITIONS THAT ARE SHOWN AS "TYPICAL", "AVERAGE", "NOMINAL", ETC.).
END ITEM IDENTIFICATIONKC135R ACFT