|
|
|
National Stock Number:
5340-01-368-4770
Federal Supply Class:
5340
National Item Identification Number:
013684770
Description:
SEAT,HELICAL COMPRESSION SPRING
Detail:
A circular item, usually having a flat or grooved flange, boss(es), and/or counterbore designed to accommodate the end of the spring. It is used to position the spring, but does not encase the spring or restrain lateral motion. It may be used in conjunction with a RETAINER, HELICAL COMPRESSION SPRING. Excludes WASHER (1), (as modified); SEAT, BALL SOCKET and HOLDER, SPRING. See also ROTOR, ENGINE POPPET VALVE.
|
Manufacturer Information:
| 17P1C7264-1 | 88277 | THE BOEING COMPANY |
|
Techincal Specification:
| DESIGN TYPE | SOLID | | END DIAMETER | 0.3080 INCHES MINIMUM AND 0.3100 INCHES MAXIMUM | | BORE DIAMETER | 0.2500 INCHES MINIMUM AND 0.2520 INCHES MAXIMUM | | FIRST STEP DIAMETER | 0.4560 INCHES MINIMUM AND 0.4600 INCHES MAXIMUM | | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-225/6, ALLOY 2024 FED SPEC SINGLE MATERIAL RESPONSE | | MATERIAL | ALUMINUM ALLOY 2024 | | PROPRIETARY CHARACTERISTICS | PACS | | OVERALL HEIGHT | 0.2150 INCHES MINIMUM AND 0.2350 INCHES MAXIMUM | | STYLE DESIGNATOR | SEAT | | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-A-8625 MIL SPEC SINGLE TREATMENT RESPONSE | | SURFACE TREATMENT | ANODIZE |
|
|