Part Details | INERTIAL NAVIGATION SYSTEM
6605-01-418-3279 A self-contained, dead-reckoning system that senses acceleration along the pitch, yaw and roll axis of land vehicle, watercraft or aircraft and calculates the distance from a reference point. They can include INERTIAL NAVIGATION UNIT(s); PLATFORM, INERTIAL; power supplies; subsystems; mode selectors; and control displays.
Alternate Parts: 342005500003, 34200550-0003, 901370347201, 901-370-347-201, 6605-01-418-3279, 01-418-3279, 6605014183279, 014183279
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 66 | AUG 24, 1995 | 01-418-3279 | 53295 ( INERTIAL NAVIGATION SYSTEM ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6605-01-418-3279
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 34200550-0003 | 0BFA5 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 901-370-347-201 | 77272 | THE BOEING COMPANYDBA BOEING |
Technical Data | NSN 6605-01-418-3279
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | ESSENTIAL TO WEAPON SYSTEM PERFORMANCE OR OPERATION OR THE PRESERVATION OF LIFE OR SAFETY OF OPERATING PERSONNEL. |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| FUNCTIONAL DESCRIPTION | FUNTIONS AS A STAPDOWN,SELF-CONTAINED ALL ATTITTUDE UNIT PROVIDING 0.8NMPH CEP FREE INERTIAL PERFORMANCE FOR UP TO SIX HOURS MINIMUM. |
| END ITEM IDENTIFICATION | V-22 AIRCRAFT |