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 5836-01-494-5942
NSN 1430-00-145-8924
NSN 5820-00-625-5416
NSN 7450-01-565-6652
NSN 5815-01-604-7516
NSN 7050-00-604-0676
NSN 5895-01-521-4800
NSN 5820-01-431-8931
NSN 6350-01-162-5958
NSN 5836-01-118-0861
NSN 5841-01-499-3273
NSN 7050-00-807-0320
Last modified 06/17/2024