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National Stock Number:
5340-01-033-9997
Federal Supply Class:
5340
National Item Identification Number:
010339997
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.
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Manufacturer Information:
| 29361 | 99643 | EATON AEROSPACE LLC |
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Techincal Specification:
| DISTANCE FROM END TO FIRST STEP | 0.6750 INCHES NOMINAL | | END DIAMETER | 0.4500 INCHES NOMINAL | | BORE DIAMETER | 0.3130 INCHES NOMINAL | | DESIGN TYPE | SOLID | | FIRST STEP LENGTH | 0.1750 INCHES NOMINAL | | FIRST STEP DIAMETER | 1.0850 INCHES NOMINAL | | FSC APPLICATION DATA | AIRCRAFT HYDRAULIC SYSTEMS | | OVERALL HEIGHT | 0.9250 INCHES NOMINAL | | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-225/6, ALLOY 2024 FED SPEC SINGLE MATERIAL RESPONSE | | MATERIAL | ALUMINUM ALLOY 2024 | | SECOND END DIAMETER | 0.4650 INCHES NOMINAL | | SECOND STEP DIAMETER | 1.3570 INCHES NOMINAL | | SECOND STEP LENGTH | 0.0550 INCHES NOMINAL | | SPECIAL FEATURES | SEAT HAS 0.125 DIAMETER HOLE THRU LOCATED 0.380 FROM HORIZONIAL CENTERLINE | | STYLE DESIGNATOR | SEAT | | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-A-8625, TYPE 1, CLASS 1 MIL SPEC SINGLE TREATMENT RESPONSE | | SURFACE TREATMENT | ANODIZE |
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