CONNECTOR BODY,RECEPTACLE,ELECTR. Key specifications include diameter: 0.056 INCHES MINIMUM AND 0.060 INCHES MAXIMUM IN, body_style: RECTANGULAR SHAPE, body_width: 0.750 INCHES NOMINAL IN, point_type: EXTENDED PRONG SQUARE CUT OR HAMMER LOCK, overall_height: 0.300 INCHES NOMINAL IN, insert_material: PLASTIC POLYAMIDE NYLON SINGLE MATING END. This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 5315-00-017-9252, 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.
| diameter | 0.056 INCHES MINIMUM AND 0.060 INCHES MAXIMUM IN |
| material | STEEL COMP 1008 OR STEEL COMP 1010 OR STEEL COMP 1012 OR STEEL COMP 1015 OR STEEL COMP 1017 OR STEEL COMP 1018 OR STEEL COMP 1020 OR STEEL COMP 1021 OVERALL |
| body_style | RECTANGULAR SHAPE |
| body_width | 0.750 INCHES NOMINAL IN |
| point_type | EXTENDED PRONG SQUARE CUT OR HAMMER LOCK |
| overall_height | 0.300 INCHES NOMINAL IN |
| insert_material | PLASTIC POLYAMIDE NYLON SINGLE MATING END |
| special_features | MOUNTING EARS |
| style_designator | STANDARD |
| underloop_length | 0.938 INCHES MINIMUM AND 1.125 INCHES MAXIMUM IN |
| surface_treatment | CADMIUM OVERALL |
| mating_end_quantity | 1 |
| NSN | 5315-00-017-9252 |
| DIAMETER | 0.056 INCHES MINIMUM AND 0.060 INCHES MAXIMUM IN |
| MATERIAL | STEEL COMP 1008 OR STEEL COMP 1010 OR STEEL COMP 1012 OR STEEL COMP 1015 OR STEEL COMP 1017 OR STEEL COMP 1018 OR STEEL COMP 1020 OR STEEL COMP 1021 OVERALL |
| UNDERLOOP LENGTH | 0.938 INCHES MINIMUM AND 1.125 INCHES MAXIMUM IN |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | QQ-P-416,TY 2,CL 3 FED SPEC SINGLE TREATMENT RESPONSE OVERALL |
| STYLE DESIGNATOR | STANDARD |
| END ITEM IDENTIFICATION | W/S: AIRCRAFT, T-2; BRIDGE ADAPTER PALLET; AIRCRAFT, EAGLE F-15; ENGINE, AIRCRAFT, TF39-GE-1 (C-5A); AIR COMPRESSORS, HIGH PRESSURE; AIRCRAFT, C-2A (REPROCURED); MISSILE, ALL-WEATHER ANTI-SHIP, HARPOON (AGM-84); AIRCRAFT, HX UNIQUE; SUPPORT EQUIPMENT, B-1 AIRCRAFT; ENGINE, AIRCRAFT, T56-A-7/15 (C-130B/E/H/N/P) A |
| SURFACE TREATMENT | CADMIUM OVERALL |
| MATERIAL DOCUMENT AND CLASSIFICATION | 66 FED STD ALL MATERIAL RESPONSES OVERALL |
| POINT TYPE | EXTENDED PRONG SQUARE CUT OR HAMMER LOCK |