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 1285-01-339-8074
NSN 5820-01-497-6563
NSN 6675-01-565-2644
NSN 6730-01-437-6128
NSN 6730-01-215-1189
NSN 6110-01-534-6299
NSN 5805-01-497-5471
NSN 5995-01-479-4588
NSN 6605-00-933-8770
NSN 5995-01-199-9553
NSN 7450-01-089-9325
NSN 7021-01-290-2682
Last modified 05/04/2024