424053: STEM,FLUID VALVE.
The STEM,FLUID VALVE is a the manufacturer industrial component. Key specifications include diameter: 0.056 INCHES MINIMUM AND 0.060 INCHES MAXIMUM IN, point_type: EXTENDED PRONG SQUARE CUT OR HAMMER LOCK, style_designator: STANDARD, underloop_length: 0.938 INCHES MINIMUM AND 1.125 INCHES MAXIMUM IN, surface_treatment: CADMIUM OVERALL, material_document_and_classification: 66 FED STD ALL MATERIAL RESPONSES OVERALL. This part is cataloged in the U.S.
Government catalog 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 |
| point_type | EXTENDED PRONG SQUARE CUT OR HAMMER LOCK |
| style_designator | STANDARD |
| underloop_length | 0.938 INCHES MINIMUM AND 1.125 INCHES MAXIMUM IN |
| surface_treatment | CADMIUM OVERALL |
| material_document_and_classification | 66 FED STD ALL MATERIAL RESPONSES OVERALL |
| surface_treatment_document_and_classification | QQ-P-416,TY 2,CL 3 FED SPEC SINGLE TREATMENT RESPONSE OVERALL |
| NSN | 5315-00-017-9252 |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | QQ-P-416,TY 2,CL 3 FED SPEC SINGLE TREATMENT RESPONSE OVERALL |
| STYLE DESIGNATOR | STANDARD |
| MATERIAL DOCUMENT AND CLASSIFICATION | 66 FED STD ALL MATERIAL RESPONSES OVERALL |
| DIAMETER | 0.056 INCHES MINIMUM AND 0.060 INCHES MAXIMUM IN |
| SURFACE TREATMENT | CADMIUM OVERALL |
| 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 |
| UNDERLOOP LENGTH | 0.938 INCHES MINIMUM AND 1.125 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 |
| POINT TYPE | EXTENDED PRONG SQUARE CUT OR HAMMER LOCK |