Thank you for taking an interest in the various military and defense parts, aerospace parts, and other items that we offer. You have reached the RFQ page for part number 5914011, a Hamilton Sundstrand Corporation item with the NSN 2835013083769 that is listed alongside the description “Engine Gas Turbine Nonaircraft.” If you are interested in part number 5914011 and wish to learn more about your purchasing options, be sure to submit the form below at your earliest convenience while supplying us with important information concerning your needs and restrictions alike. Once we have a chance to receive and review your completed form, a member of our staff will reach out to you in 15 minutes or less to present a tailored solution for your comparisons.
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To ensure that shopping with us is as simple as possible, we make it easy to identify and procure exact items by listing parts alongside all applicable designations and information. For example, part number 5914011 is specifically listed with the NSN 2835-01-308-3769, and this code can be used to determine that it falls under FSC 2835 Gas Turbines and Jet Engines Non Aircraft Prime Mover Aircraft Non Prime Mover and Components. Additionally, while tracing back to Hamilton Sundstrand Corporation, this NSN part was specifically produced under CAGE Code 99167. With our services and dedication to simple procurement in mind, get started with us today!
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2835-01-308-3769 Item PartTypeName: 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 |
| 4504554 | 5 | 2 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AAXX | MOUNTING TYPE | AIRCRAFT |
| 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 |
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