Part Details | GUIDED MISSILE MAINTENANCE FIXTURE
4935-00-238-2273 A fixture designed to mount or position guided missile subassemblies such as rate sensing units, control subassemblies, missile guidance sections or the like to facilitate inspection, repair, and/or replacement of component parts.
Alternate Parts: 16ADA27825, 4935-00-238-2273, 00-238-2273, 4935002382273, 002382273
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 49 | SEP 14, 1972 | 00-238-2273 | 38312 ( FIXTURE, GUIDED MISSILE MAINTENANCE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 4935-00-238-2273
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 16ADA27825 | 09205 | LOCKHEED MARTIN CORPELECTRONICS AND MISSILES DIV |
Technical Data | NSN 4935-00-238-2273
| Characteristic | Specifications |
|---|---|
| OVERALL LENGTH | 24.000 INCHES NOMINAL |
| OVERALL WIDTH | 11.000 INCHES NOMINAL |
| OVERALL HEIGHT | 29.000 INCHES NOMINAL |
| SPECIAL FEATURES | CONSISTS OF A FORWARD ROCKER ARM SUPPORT AND AN AFT ROCKER ARM SUPPORT; A GAS ACTUATED CYLINDER LOCATED AT THE BACK OF THE INSTALLATION FIXTURE IS USED TO APPLY A 1000 LB FORCE TO THE PIVOT PLATE. CYLINDER PISTON IS CONTROLLED BY A SELECTOR FED FROM A 1500 PSI DRY NITROGEN OR AIR SUPPLY; ANOTHER CYLINDER, MOUNTED VERTICALLY ON TOP OF THE FIXTURE HAS A SPECIAL TIP; SHOP AIR 80-100 PSI USED TO RETURN CYLINDERS TO STARTING POSITIONS |
| END ITEM IDENTIFICATION | AIM-9 SIDEWINDER MISSILE |
| FUNCTIONAL DESCRIPTION | USED TO ASSEMBLE THE PIEZOELECTRIC CRYSTAL WITH ALUMINUM RING INTO THE FORWARD AND AFT ROCKER ARM CAVITIES |
| REFERENCE DATA AND LITERATURE | 33DA-1-122 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | B.T. CRYSTAL INSTALLATION FIXTURE |