NSN 2835-01-343-4081
Part Details | NONAIRCRAFT GAS TURBINE ENGINE
2835-01-343-4081 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: 16600500, 16600-500, 2835-01-343-4081, 01-343-4081, 2835013434081, 013434081
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 13, 1991 | 01-343-4081 | 50489 ( ENGINE, GAS TURBINE, NONAIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2835-01-343-4081
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 16600-500 | 55820 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
Technical Data | NSN 2835-01-343-4081
| Characteristic | Specifications |
|---|---|
| FUEL TYPE | JET FUEL |
| POWER OUTPUT FOR WHICH DESIGNED | SHAFT |
| OVERALL LENGTH | 81.400 INCHES NOMINAL |
| OVERALL HEIGHT | 46.500 INCHES NOMINAL |
| OVERALL WIDTH | 45.600 INCHES NOMINAL |
| REFERENCE DATA AND LITERATURE | 2G-T41M-4 FIG.1 |
| DEPARTURE FROM CITED DOCUMENT | ACGENERATOR NOT INCLD |
| END ITEM IDENTIFICATION | KC-135A-E ACFT |