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SPRING, HELICAL, EXTENSION FOR LOADS BELOW 30 POUNDS
- Aerospace Standard
- AS24586C
- Revised
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Sector:
Issuing Committee:
Language:
English
Rationale
DIMENSION FOR GAP BETWEEN END HOOKS OF SPRING AND SPRING BODY CORRECTED.
Recommended Content
| Aerospace Standard | SPRING, HELICAL, EXTENSION FOR LOADS BELOW 30 LBF |
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| Aerospace Material Specification | Steel, Highly-Stressed Springs 0.95Cr - 0.20V (0.48 - 0.53C) (SAE 6150) Case Hardened |
Topic
2D/3D Drawings
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Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| TABLE 1 | CORRECTION FACTORS FOR STRESS RANGE, LIFE CYCLES AND SPRING MATERIAL | |
| Unnamed Dataset 2 | ||
| Unnamed Dataset 3 | ||
| TABLE 2 | DIMENSIONS AND CHARACTERISTICS | |
| Unnamed Dataset 5 | ||
| Unnamed Dataset 6 | ||
| Unnamed Dataset 7 | ||
| Unnamed Dataset 8 | ||
| Unnamed Dataset 9 | ||
| Unnamed Dataset 10 | ||
| Unnamed Dataset 11 |
Issuing Committee
E-25 General Standards for Aerospace and Propulsion Systems
The SAE E-25 General Standards for Aerospace & Propulsion Systems committee addresses aerospace propulsion systems and components. These systems and components include bolts, screws, nuts, washers, studs, rivets, pins, covers, O-rings, brackets, plugs and associated procurement requirements, as well as solid film lubricants and design specifications for screw threads and fastener assembly requirements.
Reference
| Number | Title |
|---|---|
| AMSQQP416 | Plating, Cadmium (Electrodeposited) |
| ASM2700 | This document is not part of the subscrption. |
| ASTMA228 | This document is not part of the subscrption. |
| ASTMB633 | This document is not part of the subscrption. |
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