160001-1100: ENGINE,GAS TURBINE,NONAIRCRAFT.
The ENGINE,GAS TURBINE,NONAIRCRAFT is a the manufacturer industrial component. Key specifications include fuel_type: JET FUEL, mounting_type: AIRCRAFT, overall_width: 16.500 INCHES NOMINAL IN, overall_height: 16.500 INCHES NOMINAL IN, overall_length: 19.500 INCHES NOMINAL IN, end_item_identification: F-16 ACFT. This part is cataloged in the U.S.
Government catalog under NSN 2835-01-154-3533, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.
Verify compatibility with your specific system configuration before ordering.
| fuel_type | JET FUEL |
| mounting_type | AIRCRAFT |
| overall_width | 16.500 INCHES NOMINAL IN |
| overall_height | 16.500 INCHES NOMINAL IN |
| overall_length | 19.500 INCHES NOMINAL IN |
| end_item_identification | F-16 ACFT |
| reference_data_and_literature | AF TO. 2JA3-57-3 |
| power_output_for_which_designed | SHAFT |
| NSN | 2835-01-154-3533 |
| OVERALL HEIGHT | 16.500 INCHES NOMINAL IN |
| REFERENCE DATA AND LITERATURE | AF TO. 2JA3-57-3 |
| OVERALL LENGTH | 19.500 INCHES NOMINAL IN |
| OVERALL WIDTH | 16.500 INCHES NOMINAL IN |
| FUEL TYPE | JET FUEL |
| POWER OUTPUT FOR WHICH DESIGNED | SHAFT |
| 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 TURBINE; ANNULAR COMBUSTOR; CAPACITOR-DISCHARGE TY INGITION EXCITER; SURFACE-DISCHARGE TY SPARK PLUG DEGF |
| END ITEM IDENTIFICATION | F-16 ACFT |
| MOUNTING TYPE | AIRCRAFT |
No substitute or cross-reference records for this part.