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Rings, Retaining – Spiral Wound, Uniform Section Corrosion and Heat Resistant, UNS S66286
- Aerospace Standard
- AS4299B
- Revised
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This procurement specification covers retaining rings of the spiral wound type with uniform rectangular cross-section, made of a corrosion and heat resistant age hardenable iron base alloy of the type identified under the Unified Numbering System as UNS S66286, work strengthened and heat treated to a tensile strength of 185 to 240 ksi at room temperature.
Rationale
Revise QQ-P-35 TO AMS2700, add minimum to FPI Sensitivity Level, error corrected in Table 5 for ØC (nom. bore 5.905), update references and titles throughout (NASM, ASTM, ANSI/ASME), general editorial update.
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Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Table 1 | ||
Unnamed Dataset 2 | ||
Unnamed Dataset 3 | ||
Unnamed Dataset 4 | ||
Table 2 | ||
Table 3 | Groove runout tolerance (inches) | |
Table 4 | Groove dimensions, external rings (inches) | |
Table 4 | Groove dimensions, external rings (inches) (continued) | |
Table 5 | Groove dimensions, internal rings (inches) | |
Table 6A | Nondestructive tests | |
Table 6B | Destructive tests | |
Table 7 | Sampling data | |
Table 8 | Classification of visual and dimensional characteristics | |
Table 9 | Sampling data |
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
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