|
|
|
National Stock Number:
5340-01-398-1743
Federal Supply Class:
5340
National Item Identification Number:
013981743
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:
| 3180436-1 | 59364 | HONEYWELL INTERNATIONAL INC. |
|
Techincal Specification:
| DESIGN TYPE | SOLID | | DISTANCE FROM END TO FIRST STEP | 0.0300 INCHES MINIMUM AND 0.0500 INCHES MAXIMUM | | END DIAMETER | 0.2500 INCHES MINIMUM AND 0.2700 INCHES MAXIMUM | | FIRST STEP DIAMETER | 0.4200 INCHES MINIMUM AND 0.4400 INCHES MAXIMUM | | FIRST STEP LENGTH | 0.0300 INCHES MINIMUM AND 0.0400 INCHES MAXIMUM | | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-225/8, ALLOY 6061, T6 FED SPEC SINGLE MATERIAL RESPONSE | | MATERIAL | ALUMINUM ALLOY 6061 | | PROPRIETARY CHARACTERISTICS | PACS | | OVERALL HEIGHT | 0.0900 INCHES NOMINAL | | SECOND END DIAMETER | 0.3300 INCHES MINIMUM AND 0.3400 INCHES MAXIMUM | | SPHERICAL SEAT TOP RADIUS | 0.0300 INCHES MINIMUM AND 0.0500 INCHES MAXIMUM | | STYLE DESIGNATOR | SEAT | | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-A-8625 MIL SPEC SINGLE TREATMENT RESPONSE | | SURFACE TREATMENT | ANODIZE |
|
|