The FUSE,CARTRIDGE is a the manufacturer industrial component. Key specifications include material: STEEL COMP 410 OVERALL, body_style: TUBE TYPE, corner_shape: SQUARE LEFT FLANGE OUTSIDE RIGHT CORNER, flange_width: 0.0650 INCHES MINIMUM AND 0.0750 INCHES MAXIMUM IN, overall_length: 0.4500 INCHES MINIMUM AND 0.5450 INCHES MAXIMUM IN, hardness_rating: 25.0 ROCKWELL C MINIMUM AND 33.0 ROCKWELL C MAXIMUM OVERALL. This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 5920-00-142-7375, 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.
| material | STEEL COMP 410 OVERALL |
| body_style | TUBE TYPE |
| corner_shape | SQUARE LEFT FLANGE OUTSIDE RIGHT CORNER |
| flange_width | 0.0650 INCHES MINIMUM AND 0.0750 INCHES MAXIMUM IN |
| overall_length | 0.4500 INCHES MINIMUM AND 0.5450 INCHES MAXIMUM IN |
| hardness_rating | 25.0 ROCKWELL C MINIMUM AND 33.0 ROCKWELL C MAXIMUM OVERALL |
| overall_diameter | 0.250 INCHES NOMINAL IN |
| special_features | WEAPON SYSTEM ESSENTIAL |
| style_designator | SOLID, EXTERNAL FLANGE ONE END |
| features_provided | NONRENEWABLE FUSIBLE ELEMENT |
| body_inside_diameter | 1.1095 INCHES MINIMUM AND 1.1100 INCHES MAXIMUM IN |
| body_outside_diameter | 1.2501 INCHES MINIMUM AND 1.2504 INCHES MAXIMUM IN |
| NSN | 5920-00-142-7375 |
| SPECIAL FEATURES | WEAPON SYSTEM ESSENTIAL |
| END ITEM IDENTIFICATION | F-4 PHANTOM,C-135 STRATOLIFTER,C-130 HERCULES,F-15 EAGLE,T-37 AIRCRAFT. H-3 GREEN GIANT,HH/UH-1 IROQUOIS HELICOPTER. AIM SIDEWINDER MISSLE SYSTEMS (9P/L/M/X). 485L TACS. ADVANCED AIR TRAFFIC CONTROL & LAND SYSTEM (ATCALS) 404L. JOINT SURVEILLANCE SYSTEM(JSS)/REGION OPS CONTROL CENTER (ROCC). A-10, F-4, F-111 (FMS ONLY) SIMULATOR. TARGET SYSTEM AERIAL GUNNERY (AGTS). T-37, T-38 B-1 AIRCRAFT SUPPORT EQUIPMENT. DEFENSE COMMUNICATIONS RADIO (9 SYSTEMS). J69-T-25 (T-37B) AIRCRAFT ENGINE. |
| OVERALL DIAMETER | 0.250 INCHES NOMINAL IN |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| CIRCUIT OVER-CURRENT INTERRUPTION DELAY TIME IN SECONDS | 25.0 200 PCT OF CURRENT RATING AND 8.0 300 PCT OF CURRENT RATING |
| MAXIMUM VOLTAGE RATING IN VOLTS | 32.0 AC AND 32.0 DC |
| CONTINUOUS CURRENT RATING IN AMPS | 8.000 |
| FEATURES PROVIDED | NONRENEWABLE FUSIBLE ELEMENT |
| CIRCUIT OVER-CURRENT INTERRUPTION TYPE | TIME DELAY |
| INTERRUPTION INDICATOR METHOD | VISIBLE ELEMENT |