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 7520-00-466-6290
NSN 5810-01-633-9441
NSN 5995-00-647-3558
NSN 5820-00-823-5675
NSN 1285-01-430-3968
NSN 6350-01-163-6713
NSN 6605-00-602-2076
NSN 5965-01-556-4337
NSN 5810-00-144-2628
NSN 5995-00-156-0808
NSN 7450-00-332-9200
NSN 5826-01-207-2103
Last modified 05/12/2024