The unit functions as a server between the main system computer in the surveillance information processingcenter and the airborne digital processing unit in each flight line test. The unit accepts direction finding, built-in-test and mode command requests from the main system computer over the local area network and commands the aircraft to carry out direction finding processing. Carries out built-in-test and reports status containing flight line test set inertial navigation system data. Te unit may also obtain the current system data. Te unit may also obtain the current system time from the global positioning satellite system
Interface Adapter
4920-01-465-7013 end item identification, solid state circuit construction type, 0.5 hertz operating channel frequency per channel
-10.0 to 55.0 deg celsius storage temp range, 8.8 inches unpackaged unit length, 2.7 inches unpackaged unit width, 8.2 inches unpackaged unit height
Boeing cabinet assembly e130 end item identification, chassis, mission computer processor
Boeing dual mission console 141-45-01 end item identification, usb/nic rear transmition module
NSN 7520-00-579-9082
NSN 5820-00-151-6751
NSN 6675-01-478-5065
NSN 6730-00-585-3086
NSN 5810-01-658-5200
NSN 5995-00-853-5911
NSN 6350-01-140-8332
NSN 5836-00-578-9614
NSN 5975-01-652-6549
NSN 5836-00-081-9880
NSN 7050-01-060-2253
NSN 6675-01-431-6915
Last modified 05/03/2024