Part Details | SERVOCYLINDER
1650-00-113-7674 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: 318700012, 3187000-12, 318700012, 3187000-12, A51H900012, A51H9000-12, A51H900012, A51H9000-12, 1650-00-113-7674, 00-113-7674, 1650001137674, 001137674
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 16 | FEB 22, 1974 | 00-113-7674 | 31309 ( SERVOCYLINDER ) |
REFERENCE DRAWINGS & PICTURES
BEARING TYPE
BEARING TYPE
GASKET SEAL
Cross Reference | NSN 1650-00-113-7674
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 3187000-12 | 77068 | ALLIED-SIGNAL INCDBA ALLIED-SIGNAL AEROSPACE CO |
| 3187000-12 | 0ZWK8 | MOOG INC.DBA MOOG AIRCRAFT GROUP TORRANCE |
| A51H9000-12 | 26512 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV MISSION SYSTEMS |
| A51H9000-12 | 61174 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NORTHROP GRUMMAN AEROSPACE |
Technical Data | NSN 1650-00-113-7674
| Characteristic | Specifications |
|---|---|
| DESIGN CHARACTERISTICS | DOUBLE ACTING SINGLE CYLINDER |
| INTEGRAL VALVE OPERATION METHOD | HYDRAULIC |
| OVERALL WIDTH | 7.450 INCHES NOMINAL |
| OVERALL HEIGHT | 12.230 INCHES NOMINAL |
| BODY OUTSIDE DIAMETER | 6.130 INCHES NOMINAL |
| BODY MATERIAL | STEEL |
| BORE DIAMETER | 5.474 INCHES NOMINAL |
| FIRST PISTON ROD END STYLE | BEARING TYPE |
| MOUNTING TYPE AND LOCATION | TONGUE CYLINDER HEAD END |
| PORT LOCATION AND QUANTITY | 4 CENTER SECTION |
| PORT STYLE | GASKET SEAL |
| PORT THREAD SERIES DESIGNATOR | UNJF |
| PORT THREAD DIAMETER | 0.875 INCHES |
| PORT THREAD QUANTITY PER INCH | 14 |
| PORT THREAD CLASS | 3B |
| PRESSURE RATING | 3000.0 POUNDS PER SQUARE INCH NOMINAL |
| SPECIAL FEATURES | RIGHT HAND INSTALLATION |
| REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | AS DIFFERENTIATED BY SOURCE CONTROL DWG NO. |
| FSC APPLICATION DATA | HYDRAULIC SYSTEMS,AIRCRAFT |