NSN 2995-01-139-6642
Part Details | GAS TURBINE ENGINE STARTER
2995-01-139-6642 An item designed to accelerate a gas turbine engine from rest to starter cutoff speed by means of a combustion gas driven turbine and reduction gear assembly constructed to be mounted on the engine starter drive. The combustion gas is generated from ignited liquid fuel and air in the combustion chamber or from a solid propellant cartridge attached to the combustion chamber of the starter. May have provision for energizing the turbine by low pressure air from engine bleed or ground equipment air supply.
Alternate Parts: 3535419, 35-35419, 35051243, 3505124-3, 350512451, 3505124-5-1, 350512431, 3505124-3-1, 350512431, 3505124-3-1, 2995-01-139-6642, 01-139-6642, 2995011396642, 011396642
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 29 | OCT 05, 1982 | 01-139-6642 | 21907 ( STARTER, ENGINE, GAS TURBINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2995-01-139-6642
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 35-35419 | 82918 | BOEING COMPANY, THEDBA BOEING |
| 3505124-3 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 3505124-5-1 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 3505124-3-1 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 3505124-3-1 | 59364 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2995-01-139-6642
| Characteristic | Specifications |
|---|---|
| END ITEM IDENTIFICATION | TF33-PW-102/JT3D AIRCRAFT ENG |