STRAP,TIE DOWN,ELECTRICAL COMPON. Key specifications include usage_form: SINGULAR, end_item_identification: ENGINE, AIRCRAFT, F100-PW-200 (F-16A/B/C/D) A. This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 5999-00-754-7567, 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.
| usage_form | SINGULAR |
| end_item_identification | ENGINE, AIRCRAFT, F100-PW-200 (F-16A/B/C/D) A |
| NSN | 5999-00-754-7567 |
| OVERALL HEIGHT | 0.375 INCHES NOMINAL IN |
| CURRENT RATING FOR WHICH DESIGNED | 35.5 AMPERES MINIMUM AND 37.5 AMPERES MAXIMUM |
| OVERALL LENGTH | 1.906 INCHES NOMINAL IN |
| OVERALL WIDTH | 0.344 INCHES NOMINAL IN |
| MOUNTING FACILITY TYPE AND QUANTITY | 2 UNTHREADED HOLE(S) |
| MOUNTING HOLE DIAMETER | 0.145 INCHES NOMINAL IN |
| OVERALL HEIGHT | 0.375 INCHES NOMINAL IN |
| CURRENT RATING FOR WHICH DESIGNED | 35.5 AMPERES MINIMUM AND 37.5 AMPERES MAXIMUM |
| OVERALL LENGTH | 1.906 INCHES NOMINAL IN |
| OVERALL WIDTH | 0.344 INCHES NOMINAL IN |