NSN 6615-00-592-1963
Part Details | SERVOCYLINDER
6615-00-592-1963 A hydraulically or pneumatically powered actuating cylinder with provisions for directional control (positioning) in direct relation with a primary control of comparatively low level force. The primary control input to the servocylinder may be mechanical and/or electrical.
Alternate Parts: 167301A, 16730-1A, 167301A, 16730-1A, 167301A, 16730-1A, 6615-00-592-1963, 00-592-1963, 6615005921963, 005921963
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
66 | JAN 01, 1963 | 00-592-1963 | 31309 ( SERVOCYLINDER ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6615-00-592-1963
Part Number | Cage Code | Manufacturer |
---|---|---|
16730-1A | 77068 | ALLIED-SIGNAL INCDBA ALLIED-SIGNAL AEROSPACE CO |
16730-1A | 19315 | HONEYWELL INTL INC DEFENSE AVIONICSSYSTEMS FORMER BENDIX NAVIGATION AND |
16730-1A | 0ZWK8 | MOOG INC.DBA MOOG AIRCRAFT GROUP TORRANCE |
Technical Data | NSN 6615-00-592-1963
Characteristic | Specifications |
---|---|
DESIGN CHARACTERISTICS | SINGLE ACTING SINGLE CYLINDER |
INTEGRAL VALVE OPERATION METHOD | HYDRAULIC |
OVERALL WIDTH | 4.250 INCHES NOMINAL |
OVERALL HEIGHT | 8.125 INCHES NOMINAL |
EXTENDED LENGTH | 13.000 INCHES NOMINAL |
COMPRESSED LENGTH | 11.250 INCHES NOMINAL |
BODY MATERIAL | STEEL |
BORE DIAMETER | 0.500 INCHES NOMINAL |
FSC APPLICATION DATA | AUTOMATIC PILOT SYSTEM |