Acm se end item identification, continuity test of the impact sensor assembly is required to impact sensor test; a pre-power static manually measure the impact sensor loop .
Continuity test of the impact sensor assembly is required to impact sensor test; a pre-power static manually measure the impact sensor loop and the ordnance alarm loop circuit continuity. The impact sensor loop continuity resistance is not to exceed 2.0 ohms. The ordnance alarm loop continuity resistance is not to exceed 1.0 ohm.Afm-124
An item specifically designed to provide azimuth and elevation deviation rate information obtained by tracking a moving target. The electrical error voltages are used to provide corrective command signals to a guided missile in flight. Excludes accelerometer (as modified); gyroscope, rate; and moving target indicator group.
Generator
Pulse Regenerator Synchro
Gaircraft model f4e end item identification
Display assembly, guided missile remote control system end item identification
Diode Protection
NSN 5831-01-181-5470
NSN 6675-00-016-7640
NSN 5810-01-554-1040
NSN 7520-01-416-4322
NSN 6675-01-224-8415
NSN 7021-01-417-8286
NSN 5821-01-138-1676
NSN 6675-00-491-2332
NSN 1285-01-419-3931
NSN 7021-01-428-4365
NSN 5831-00-809-3180
NSN 6675-01-098-1225
Last modified 11/02/2024