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 5820-01-431-2060
NSN 5820-01-360-5662
NSN 6110-01-395-3421
NSN 5820-00-967-1914
NSN 7450-01-502-5153
NSN 5975-01-477-3404
NSN 1285-00-552-5794
NSN 5841-01-633-9970
NSN 5895-00-280-7528
NSN 5841-01-539-0841
NSN 6605-00-864-1282
NSN 5805-00-556-0670
Last modified 05/03/2024