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 5815-01-648-2038
NSN 5836-01-548-6920
NSN 6675-01-391-7140
NSN 5810-01-539-2175
NSN 7021-00-775-8879
NSN 7450-00-214-0893
NSN 6110-01-462-8995
NSN 7520-00-109-5350
NSN 7450-00-686-6069
NSN 7450-00-004-5616
NSN 6110-01-099-6893
NSN 6675-01-412-0367
Last modified 04/29/2024