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MS29513-127
Military Standard Ring O
Description
O-Ring
Specifications
| Center Hole Diameter | Between 1.418 inches and 1.430 inches |
|---|---|
| Compound Specification Number | MIL-P-5315 |
| Cross-Sectional Height | Between 0.100 inches and 0.106 inches |
| End Application | Tf-33-p-7 (c-141a/b) aircraft f100-pw-100 (f-15a/b/c/d); engine aircraft f100-pw-200 (f-16a/b/c/d); engine aircraft ec-18b; engine c-18a hh-53h pave low; aircraft tf33-100 (e3a/b/c); helicopter aircraft b-52h); engine aircraft tf33-p-3/5/9 (c/ec-135 ec-135h/k/p); engine aircraft tf33-pwpp-102 (c-135e hc-130); engine ec-130e mc-130h w/s: aircraft (ac-130h |
| Industry Standards/Certification | MS29513 |
| Inside Diameter | 1.424 in |
| Inside Diameter Tolerance | ±0.003 to ±0.005 in |
| Material | Rubber |
| NIIN | 00-265-1078 |
| NSN | 5331-00-265-1078 |
| Outside Diameter | Between 1.612 inches and 1.648 inches |
| Temperature Range | -65 to 200 ºF |
| Thickness | 0.103 in |
| Thickness Tolerance | ±0.003 to ±0.005 in |
| Weight | 0.0055 lb |
Cross-reference
Similar parts
Parts with matching key dimensions — often from a different standards family. Candidates for comparison only; verify the full specification before substituting.
- MS28775-127 MS 1-5/8 in · 1.42 in · Rubber
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Catalog data updated 2026-07-05. Report a data error