NSN 2995-01-320-1315
Part Details | GAS TURBINE ENGINE STARTER
2995-01-320-1315 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: 350530061, 3505300-6-1, 36E14412A, 36E144-12A, 7030610000106, 70306-10000-106, 7030610000AV1, 70306-10000-AV1, 7030610000, 70306-10000, 2995-01-320-1315, 01-320-1315, 2995013201315, 013201315
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 29 | MAY 19, 1990 | 01-320-1315 | 21907 ( STARTER, ENGINE, GAS TURBINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2995-01-320-1315
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 3505300-6-1 | 59364 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 36E144-12A | 92003 | PARKER HANNIFIN CORPORATIONDIV AEROSPACE GROUP HEADQUARTERS |
| 70306-10000-106 | 81996 | U S ARMY AVIATION AND MISSILECOMMAND |
| 70306-10000-AV1 | 81996 | U S ARMY AVIATION AND MISSILECOMMAND |
| 70306-10000 | 81996 | U S ARMY AVIATION AND MISSILECOMMAND |
Technical Data | NSN 2995-01-320-1315
| Characteristic | Specifications |
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