Part Details | SERVOCYLINDER
1650-01-089-6829 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: 318700013, 3187000-13, 318700013, 3187000-13, A51H900013, A51H9000-13, A51H900013, A51H9000-13, 1650-01-089-6829, 01-089-6829, 1650010896829, 010896829
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 16 | FEB 06, 1980 | 01-089-6829 | 31309 ( SERVOCYLINDER ) |
REFERENCE DRAWINGS & PICTURES
BEARING TYPE
BEARING TYPE
Cross Reference | NSN 1650-01-089-6829
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 3187000-13 | 77068 | ALLIED-SIGNAL INCDBA ALLIED-SIGNAL AEROSPACE CO |
| 3187000-13 | 0ZWK8 | MOOG INC.DBA MOOG AIRCRAFT GROUP TORRANCE |
| A51H9000-13 | 26512 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV MISSION SYSTEMS |
| A51H9000-13 | 61174 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NORTHROP GRUMMAN AEROSPACE |
Technical Data | NSN 1650-01-089-6829
| Characteristic | Specifications |
|---|---|
| DESIGN CHARACTERISTICS | SINGLE ACTING SINGLE CYLINDER |
| INTEGRAL VALVE OPERATION METHOD | HYDRAULIC |
| OVERALL HEIGHT | 12.230 INCHES NOMINAL |
| EXTENDED LENGTH | 43.740 INCHES MINIMUM AND 43.860 INCHES MAXIMUM |
| COMPRESSED LENGTH | 34.990 INCHES MINIMUM AND 35.110 INCHES MAXIMUM |
| BORE DIAMETER | 5.474 INCHES NOMINAL |
| FIRST PISTON ROD END STYLE | BEARING TYPE |
| FIRST END HOLE DIAMETER | B1.8745 INCHES AND C1.8750 INCHES |
| FIRST END OUTSIDE DIAMETER | 4.320 INCHES |
| PISTON ROD END SIMILARITY | NOT IDENTICAL |
| SECOND PISTON ROD END STYLE | BEARING TYPE |
| SECOND END HOLE DIAMETER | B1.4995 INCHES AND C1.5000 INCHES |
| SECOND END OUTSIDE DIAMETER | B4.100 INCHES AND C4.220 INCHES |
| MOUNTING TYPE AND LOCATION | BEARING BOTH ENDS |
| REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | AS DIFFERENTIATED BY THE SOURCE CONTROL DRAWING NO. |
| CRITICALITY CODE JUSTIFICATION | AAMDX$$AAMGS |
