Part Details | INTERFACE DEVICE ADAPTER ASSEMBLY
4920-01-080-8239 A device designed to facilitate connection, provide accommodation, enable application, to permit use of a given item with an unlike item.
Alternate Parts: 16U145721, 16U14572-1, 16U145721, 16U14572-1, 4920-01-080-8239, 01-080-8239, 4920010808239, 010808239
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 49 | AUG 02, 1979 | 01-080-8239 | 51091 ( ADAPTER ASSEMBLY, INTERFACE DEVICE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 4920-01-080-8239
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 16U14572-1 | 94117 | BAE SYSTEMS INFORMATION ANDELECTRONIC SYSTEMS INTEGRATION INC. |
| 16U14572-1 | 81755 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
Technical Data | NSN 4920-01-080-8239
| Characteristic | Specifications |
|---|---|
| END ITEM IDENTIFICATION | F-16A/B ACFT AGE. |
| SPECIAL FEATURES | MANUFACTURERS NAME - ADAPTER ASSEMBLY, PILOT'S CONTROL USED WITH A SPRING RESILIENCY TESTER TO APPLY THE 20 LBS OF FORCE NEEDED TO PRODUCE THE 120 INCH POUNDS OF TORQUE REQUIRED TO INSTALL THE RETAINING NUT ON THE CONTROL STICK. THIS NUT HOLDS THE PILOT'S CONTROL GRIP ONTO THE CONTROL STICK |
| FUNCTIONAL DESCRIPTION | CLAMPS ONTO THE PILOT CONTROL GRIP RETAINING NUT TO APPLY SUFFICIENT TORQUE TO REMOVE/INSTALL THE NUT |
| REFERENCE DATA AND LITERATURE | TO 1F-16A-4-4 |