Processor direction finding
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 6605-01-367-2656
NSN 5820-01-384-9095
NSN 5895-01-170-1003
NSN 1240-01-078-4706
NSN 5840-01-301-5287
NSN 6605-01-321-7720
NSN 7450-00-351-8115
NSN 5841-00-011-1058
NSN 1240-01-459-0504
NSN 6350-00-772-8528
NSN 6940-00-767-3417
NSN 5820-01-257-4721
Last modified 05/03/2024