NSN 5340-00-664-0671
Part Details | DUST AND MOISTURE SEAL PROTECTIVE CAP
5340-00-664-0671 An item specifically designed to fit over the opening(s) of various items to provide mechanical protection and/or to prevent the entrance of foreign matter during painting, shipping, storage, or the like. It is not designed to retain fluids under pressure during equipment operation. Excludes COVER, ELECTRICAL CONNECTOR; HOOD, SEALING, BOTTLE; and STOPPER, BOTTLE. For items designed to fit into or over the opening(s) of various items, see CAP-PLUG, PROTECTIVE, DUST AND MOISTURE SEAL.
Alternate Parts: A7208403, A7208-403, M550111F6, M5501/11-F6, MILC550111, MIL-C-5501/11, NAS8326, NAS832-6, NAS8326, NAS832-6, CD6, CD6, M550111F6, M5501/11F6, CD6, CD-6, 5340-00-664-0671, 00-664-0671, 5340006640671, 006640671
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | JAN 01, 1963 | 00-664-0671 | 13432 ( CAP, PROTECTIVE, DUST AND MOISTURE SEAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5340-00-664-0671
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| A7208-403 | 55806 | ALLOYTEK INC |
| M5501/11-F6 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-C-5501/11 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| NAS832-6 | 80205 | NATIONAL AEROSPACE STANDARDSCOMMITTEE AEROSPACE INDUSTRIES |
| NAS832-6 | 050R4 | PATRIOT VALVE & FITTING CORPORATIONDBA PATRIOT LOGISTICS |
| CD6 | F2521 | PLASTIFRANCE |
| CD6 | 95760 | PROTECTIVE CLOSURES CO INC |
| M5501/11F6 | D9182 | ZF INDUSTRIEANTRIEBE WITTEN GMBH |
| CD-6 | D9182 | ZF INDUSTRIEANTRIEBE WITTEN GMBH |
Technical Data | NSN 5340-00-664-0671
| Characteristic | Specifications |
|---|---|
| MATERIAL | PLASTIC |
| DESIGN TYPE | THREADED |
| THREAD SIZE AND SERIES/TYPE DESIGNATOR | 9 TO 16-18 UNF |
| THREAD CLASS | 1B |
| OVERALL DIAMETER | 0.625 INCHES NOMINAL |
| INSIDE DIAMETER LENGTH | 0.500 INCHES NOMINAL |
| ROUND CAP OUTSIDE SURFACE CONDITION | KNURLED |
| END ITEM IDENTIFICATION | W/S:ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); TRIDENT HULL STRUCTURE; AIRCRAFT, C-2A (REPROCURED); AIRCRAFT, SOF (AC-130H, MC-130H, EC-130E, HC-130); ENGINE, AIRCRAFT, TF-33-P-7 (C-141A/B); ENGINE, AIRCRAFT, TF39-GE-1 (C-5A); SUBMARINE AUXILLARY AND MISCELLANEOUS SYSTEMS; HELICOPTER LANDING SYSTEM, LAMPS MK III; MISSILE, TOMAHAWK; ENGINE, AIRCRAFT, F100-PW-100 (F-15A/B/C/D) |