NSN 1680-01-418-0807
Part Details | AIRCRAFT CONTROL COLUMN
1680-01-418-0807 A device for maintaining control of an aircraft about its pitch and roll axis. It consists of a CONTROL WHEEL, AIRCRAFT mounted at the upper end of a lever, the wheel being turned to control the aircraft about its roll axis, the lever being pushed forward or pulled back to control the aircraft about its pitch axis, excludes operation of trim tabs or the like.
Alternate Parts: 10259703, 1025-970-3, 901301009103, 901-301-009-103, 1680-01-418-0807, 01-418-0807, 1680014180807, 014180807
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 16 | AUG 21, 1995 | 01-418-0807 | 61399 ( CONTROL COLUMN, AIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 1680-01-418-0807
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1025-970-3 | 99194 | D E B MANUFACTURING, INC |
| 901-301-009-103 | 77272 | THE BOEING COMPANYDBA BOEING |
Technical Data | NSN 1680-01-418-0807
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL |
| AIRCRAFT LOCATION | MECHANICAL FLIGHT CONTROL SYSETM OF V-22 OSPREY TILTROTOR AIRCRAFT |
| OVERALL LENGTH | 2.81 INCHES MAXIMUM |
| OVERALL WIDTH | 2.00 INCHES MAXIMUM |
| SPECIAL FEATURES | 23.5" LB/RAD/SEC |
| END ITEM IDENTIFICATION | SUPPORT OF PRE-PROVISIONING ITEMS WHICH ALSO ACT AS POINT OF ENTRY FOR V-22 OSPREY |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | DAMPER ASSY |
| FUNCTIONAL DESCRIPTION | THE DAMPER IS USED IN LONGITUDINAL, LATERAL, AND DIRECTIONAL COCKPIT CONTROLS OF THE V-22 AIRCRAFT. |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| SUPPLEMENTARY FEATURES | OPERATING TEMPERATURE RANGE: -65 TO 160F |