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MS29513-215
Military Standard Ring O
Description
O-Ring
Specifications
| Center Hole Diameter | Between 1.040 inches and 1.052 inches |
|---|---|
| Compound Specification Number | MIL-P-5315 |
| Cross-Sectional Height | Between 0.135 inches and 0.143 inches |
| End Application | Ec-135h/k/p) m aircraft tf33-pw-102 (c-135e t-2; engine ah-1w; aircraft advance attack b-1 aircraft; helicopter c-2a (reprocured); support equipment tf-33-p-7 (c-141a/b); aircraft aircraft mh-53e; engine hc-130); helicopter ec-130e mc-130h (ac-130h b-52h); aircraft aircraft tf33-p-3/5/9 (c/ec-135 w/s: engine |
| Industry Standards/Certification | MS29513 |
| Inside Diameter | 1.046 in |
| Inside Diameter Tolerance | ±0.003 to ±0.005 in |
| Material | Rubber |
| NIIN | 00-250-0235 |
| NSN | 5331-00-250-0235 |
| Outside Diameter | Between 1.306 inches and 1.342 inches |
| Temperature Range | -65 to 200 ºF |
| Thickness | 0.103 in |
| Thickness Tolerance | ±0.003 to ±0.005 in |
| Weight | .005 lb |
Cross-reference
No interchangeable or dimensionally similar parts are on record for MS29513-215. Try the cross-reference lookup to search by a different part number.
Catalog data updated 2026-07-05. Report a data error