817262: ROTOR,SYNCHRO.
The ROTOR,SYNCHRO is a the manufacturer industrial component. Key specifications include material: RUBBER SYNTHETIC, thickness: 0.054 INCHES MINIMUM AND 0.074 INCHES MAXIMUM IN, hole_diameter: 0.225 INCHES MINIMUM AND 0.275 INCHES MAXIMUM IN, overall_diameter: 0.495 INCHES MINIMUM AND 0.520 INCHES MAXIMUM IN, surface_treatment: TIN OVERALL, peripheral_shape_style: ROUND. This part is cataloged in the U.S.
Government catalog under NSN 5310-00-177-1156, 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 | RUBBER SYNTHETIC |
| thickness | 0.054 INCHES MINIMUM AND 0.074 INCHES MAXIMUM IN |
| hole_diameter | 0.225 INCHES MINIMUM AND 0.275 INCHES MAXIMUM IN |
| overall_diameter | 0.495 INCHES MINIMUM AND 0.520 INCHES MAXIMUM IN |
| surface_treatment | TIN OVERALL |
| peripheral_shape_style | ROUND |
| center_hole_shape_style | ROUND |
| end_item_identification | SELF-CONTAINED BREATHING APPARATUS P/N 10046572 ONBOARD 210 FT WMEC, 270 FT WMEC & 378 FT WHEC COAST GUARD VESSELS FT |
| cross-sectional_shape_style | RECTANGULAR |
| material_document_and_classification | QQ-W-321 1/2 HARD FED SPEC 1ST MATERIAL RESPONSE OR QQ-B-626 1/2 HARD FED SPEC 2ND MATERIAL RESPONSE OVERALL |
| general_characteristics_item_description | 0.6110 IN. DIA; 1.4844 IN. LG; W/TWO COILS OF 200 TURNS EACH OF AWG 39 IN |
| surface_treatment_document_and_classification | MIL-T-10727 TY 1 MIL SPEC SINGLE TREATMENT RESPONSE OVERALL |
| NSN | 5310-00-177-1156 |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-T-10727 TY 1 MIL SPEC SINGLE TREATMENT RESPONSE OVERALL |
| OVERALL DIAMETER | 0.495 INCHES MINIMUM AND 0.520 INCHES MAXIMUM IN |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-W-321 1/2 HARD FED SPEC 1ST MATERIAL RESPONSE OR QQ-B-626 1/2 HARD FED SPEC 2ND MATERIAL RESPONSE OVERALL |
| CROSS-SECTIONAL SHAPE STYLE | RECTANGULAR |
| SURFACE TREATMENT | TIN OVERALL |
| PERIPHERAL SHAPE STYLE | ROUND |
| END ITEM IDENTIFICATION | W/S: ENGINE, AIRCRAFT, F110-GE-100/129 (F-16C/D); AIRCRAFT, (AC-130H, MC-130H, EC-130E, HC-130); GUIDED MISSILE LAUNCHING SYSTEM, MK 26 (GMLS); SUPPORT EQUIPMENT, B-1 AIRCRAFT; AIRCRAFT, C-2A (REPROCURED); TRAINER, B-1B AIRCRAFT; CLOSE IN WEAPON SYSTEM (CIWS-PHALANX); TACTICAL AIR OPNS MODULE (AN/TYQ-(23)); DEEP SUBMERGENCE SYSTEMS PROGRAMS (DSSP) A |
| MATERIAL | COPPER ALLOY 270 OR COPPER ALLOY 268 OVERALL |
| CENTER HOLE SHAPE STYLE | ROUND |
| HOLE DIAMETER | 0.225 INCHES MINIMUM AND 0.275 INCHES MAXIMUM IN |