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 5895-00-449-3380
NSN 5831-01-140-0436
NSN 7450-01-384-2027
NSN 5895-01-307-6748
NSN 5840-01-035-1194
NSN 5965-00-439-6287
NSN 7021-01-589-9446
NSN 5815-01-010-8571
NSN 5965-01-024-6137
NSN 6730-01-484-2886
NSN 7450-01-100-4446
NSN 5820-01-433-2499
Last modified 05/03/2024