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Part Information
Wstablilzation performance of the system is enchanced in both azimuth andelevation servo channels, the imc consists of a stabilized mirror assembly suspended by bendix flex pivots from astationary platform, four voice coil type linear actuators are driven bt stabilization loop error signals in both azimuth and elevation. Feedback is provided via four eddy current promimity sensors. The imc subsystem mounts diretly to the optical bench with its mirror assembly within the optical path
Part Number | RNVC | RNAAC | DAC | CAGE |
---|---|---|---|---|
6380623 | 2 | 9Z | 4 | 3U331 |
Code | Definition |
---|---|
FN | Factory New. Parts manufactured by then OEM and includes manufacturer certification. |
NE | New. Parts manufactured by the OEM. May include manufacturer certification or company certification. |
NS | New Surplus. New material item purchased from excess inventory. |
OH | Overhauled. Product has been rebuilt and tested in accordance with the manufacturer's specifications by a repair shop (MRO). |
SV | Serviceable product. |
AR | As Removed. Product removed from aircraft or platform with no guarentee on the functionality of the part. |
RP | Repairable. Product can be repaired by a MRO and be given a FAA 8130 or EASA Form 1 certification. |