The WASHER,FLAT is a the manufacturer industrial component. Key specifications include material: STEEL OVERALL, thickness: 0.080 INCHES MINIMUM AND 0.100 INCHES MAXIMUM IN, hole_diameter: 0.880 INCHES MINIMUM AND 0.900 INCHES MAXIMUM IN, overall_diameter: 1.495 INCHES MINIMUM AND 1.520 INCHES MAXIMUM IN, surface_treatment: CADMIUM OVERALL, peripheral_shape_style: ROUND. This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 5310-00-167-0827, 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 OVERALL |
| thickness | 0.080 INCHES MINIMUM AND 0.100 INCHES MAXIMUM IN |
| hole_diameter | 0.880 INCHES MINIMUM AND 0.900 INCHES MAXIMUM IN |
| overall_diameter | 1.495 INCHES MINIMUM AND 1.520 INCHES MAXIMUM IN |
| surface_treatment | CADMIUM OVERALL |
| peripheral_shape_style | ROUND |
| center_hole_shape_style | ROUND |
| cross-sectional_shape_style | RECTANGULAR |
| material_document_and_classification | MIL-S-7952 MIL SPEC SINGLE MATERIAL RESPONSE OR QQ-S-698 FED SPEC SINGLE MATERIAL RESPONSE OVERALL |
| surface_treatment_document_and_classification | QQ-P-416,TY 2,CL 3 FED SPEC SINGLE TREATMENT RESPONSE OVERALL |
| NSN | 5310-00-167-0827 |
| MATERIAL DOCUMENT AND CLASSIFICATION | MIL-S-7952 MIL SPEC SINGLE MATERIAL RESPONSE OR QQ-S-698 FED SPEC SINGLE MATERIAL RESPONSE OVERALL |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | QQ-P-416,TY 2,CL 3 FED SPEC SINGLE TREATMENT RESPONSE OVERALL |
| SURFACE TREATMENT | CADMIUM OVERALL |
| MATERIAL | STEEL OVERALL |
| CROSS-SECTIONAL SHAPE STYLE | RECTANGULAR |
| END ITEM IDENTIFICATION | W/S:DEEP SUBMERGENCE SYSTEMS PROGRAMS (DSSP); AVIATION ENGINE TEST SYSTEMS (AETS); HELICOPTER, MH-53E; ENGINE, AIRCRAFT, TF39-GE-1 (C-5A); AIRCRAFT, T-39; AIRCRAFT, C-2A (REPROCURED); SUPPORT EQUIPMENT, B-1 AIRCRAFT; ENGINE, AIRCRAFT, T56-A-7/15 (C-130B/E/H/N/P); AIRCRAFT, C-18A, EC-18B; AIRCRAFT, (AC-130H, MC-130H, EC-130E, HC-130) A |
| OVERALL DIAMETER | 1.495 INCHES MINIMUM AND 1.520 INCHES MAXIMUM IN |
| THICKNESS | 0.080 INCHES MINIMUM AND 0.100 INCHES MAXIMUM IN |
| HOLE DIAMETER | 0.880 INCHES MINIMUM AND 0.900 INCHES MAXIMUM IN |
| PERIPHERAL SHAPE STYLE | ROUND |