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 5841-01-456-1136
NSN 5826-01-592-4410
NSN 5836-01-202-7916
NSN 5805-01-065-1084
NSN 5975-01-632-4976
NSN 5820-01-200-8019
NSN 6350-00-471-3368
NSN 5965-01-252-8701
NSN 5965-01-504-8199
NSN 5831-01-632-4493
NSN 5840-01-432-2094
NSN 6760-01-024-6479
Last modified 05/03/2024