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MS29513-231
Military Standard Ring O
Description
Inner diameter: 2.609", thickness 0.139", preformed packing, hydrocarbon fuel resistant, MS29513 series o-ring
Specifications
| Center Hole Diameter | Between 2.599 inches and 2.619 inches |
|---|---|
| Compound Specification Number | MIL-P-5315 |
| Cross-Sectional Height | Between 0.135 inches and 0.143 inches |
| End Application | T-2 tf-33-p-7 (c-141a/b); aircraft aircraft b-52h); engine aircraft tf33-p-3/5/9 (c/ec-135 hc-130); engine ec-130e mc-130h (ac-130h b-2 bomber (atb); aircraft ec-135h/k/p); aircraft aircraft tf33-pw-102 (c-135e c-2a (reprocured); engine w/s: dispenser ptbl m33a1; aircraft |
| Industry Standards/Certification | MS29513 |
| Inside Diameter | 2.609 in |
| Inside Diameter Tolerance | ±0.003 to ±0.005 in |
| Material | Rubber |
| NIIN | 00-291-3073 |
| NSN | 5331-00-291-3073 |
| Outside Diameter | Between 2.859 inches and 2.915 inches |
| Temperature Range | -65 to 200 ºF |
| Thickness | 0.103 in |
| Thickness Tolerance | ±0.003 to ±0.005 in |
| Weight | .005 lb |
Cross-reference
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Catalog data updated 2026-07-05. Report a data error