Part Details | LINEAR ACTUATING CYLINDER HEAD
1650-01-252-1140 An item designed to attach to the actuating end of a linear cylinder. It has an orifice to accommodate a piston rod and packing, bearing, or the like to retain fluid in the cylinder assembly. The item may include ports, valves, and the like. For items opposite the actuating end, see CAP, LINEAR ACTUATING CYLINDER.
Alternate Parts: 68A6925192003, 68A692519-2003, 1650-01-252-1140, 01-252-1140, 1650012521140, 012521140
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 16 | MAR 29, 1987 | 01-252-1140 | 61755 ( HEAD, LINEAR ACTUATING CYLINDER ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 1650-01-252-1140
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 68A692519-2003 | 76301 | BOEING COMPANY, THEDBA BOEING |
Technical Data | NSN 1650-01-252-1140
| Characteristic | Specifications |
|---|---|
| END ITEM IDENTIFICATION | F-15 AIRCRAFT |
| OVERALL LENGTH | 6.619 INCHES MAXIMUM |
| OVERALL WIDTH | 4.4452 INCHES MAXIMUM |
| OVERALL THICKNESS | 3.550 INCHES MAXIMUM |
| SPECIAL FEATURES | MATERIAL 7075-T73,QQ-A-367 COND T73;C/O INSERT,6-PLUG SET;ANODIZE PER PS13201 TY II CL I,EXCEPT HARDCOATED AREA AND AREAS SPECIFIED;ANODIZE AFTER PEENING OPERATIONS;GLASS BEAD PEEN ENTIRE INTERNAL SURFACE IN AREAS NOTED PER PS 14023;FSC APPLICATION DATA:AIRCRAFT HYDRAULIC VACUUM DEICING SYSTEMS;FUNCTIONAL DESCRIPTION:NHA 68A692516-1001,1650012418062 |