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 5820-00-082-1599
NSN 6675-01-208-8739
NSN 6350-01-411-6576
NSN 7450-01-384-2027
NSN 5895-01-606-8766
NSN 7021-00-775-8879
NSN 5826-01-630-2186
NSN 1430-01-417-2703
NSN 5820-01-557-9655
NSN 5826-01-645-6657
NSN 5965-01-292-0035
NSN 5826-01-604-3049
Last modified 07/01/2024