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 1240-01-412-6608
NSN 7021-00-284-3777
NSN 6760-01-514-8294
NSN 6730-00-471-9670
NSN 7050-01-540-2934
NSN 7450-00-254-2159
NSN 6760-01-035-7119
NSN 6760-01-093-8326
NSN 6605-01-521-4472
NSN 5836-00-574-4446
NSN 1285-01-092-4149
NSN 6350-00-926-4384
Last modified 11/06/2024