| Part Number: 5914011 | Manufacturer: Hamilton Sundstrand Corporation |
| NSN : 2835-01-308-3769 (2835013083769) | Item Name : engine gas turbine nonaircraft |
| CAGE Code: 99167 | FSC : 2835 Gas Turbines and Jet Engines Non Aircraft Prime Mover Aircraft Non Prime Mover and Components |
| NIIN : 01-308-3769 (013083769) | FSG : 28 Engines Turbines and Components |
| Country: USA | NCB Code: 01 |
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| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2835-01-308-3769 Item Description: Engine Gas Turbine Nonaircraft | 2835 | 013083769 | 0 | Y | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 5914011 | 5 | 2 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 19.500 INCHES NOMINAL |
| ABKW | OVERALL HEIGHT | 16.500 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 16.500 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | F-16 ACFT |
| AXKD | POWER OUTPUT FOR WHICH DESIGNED | SHAFT |
| FEAT | SPECIAL FEATURES | MAX ALLOWABLE ENG SPEED 67722.0 RPM; CCW ROTATION; MAX RATED EXHAUST GAS TEMP 1200 DEG F; MAX EXHAUST GAS TEMP DURING START 1385 DEG F; FUEL STD MIL-T-5624, TY JP4/5; SINGLE-STAGE CENTRIFUGAL-FLOW COMPRESSOR; SINGLE-STAGE RADIAL-INFLOW TURB |
| FUEL | FUEL TYPE | JET FUEL |
| RDAL | REFERENCE DATA AND LITERATURE | AF TO. 2JA3-57-3 |
| AAXX | MOUNTING TYPE | AIRCRAFT |
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