Part Details | NONAIRCRAFT GAS TURBINE ENGINE
2835-01-346-1115 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: 161331128, 161331-128, 2835-01-346-1115, 01-346-1115, 2835013461115, 013461115
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 27, 1991 | 01-346-1115 | 50489 ( ENGINE, GAS TURBINE, NONAIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2835-01-346-1115
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 161331-128 | 55820 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
Technical Data | NSN 2835-01-346-1115
| Characteristic | Specifications |
|---|---|
| FUEL TYPE | JET FUEL |
| POWER OUTPUT FOR WHICH DESIGNED | SHAFT |
| MOUNTING TYPE | AIRCRAFT |
| OVERALL LENGTH | 38.800 INCHES NOMINAL |
| OVERALL HEIGHT | 24.500 INCHES NOMINAL |
| OVERALL WIDTH | 23.000 INCHES NOMINAL |
| REFERENCE DATA AND LITERATURE | AF TO. 2G-T62T-44 |
| SPECIAL FEATURES | 40HP @ 8000RPM, QUICK START APU WITH A TMD OF T-62T-40LC-2, SIMILAR TO 161331-121/135, WEIGHT 169LBS. |
| END ITEM IDENTIFICATION | KC-135R ACFT |