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 6940-01-641-6356
NSN 5821-00-553-6475
NSN 6675-00-308-7248
NSN 5826-00-011-9630
NSN 5840-01-506-8111
NSN 6675-01-177-3651
NSN 6675-00-246-3749
NSN 6675-00-427-3609
NSN 5820-01-228-0177
NSN 5821-01-443-1645
NSN 7050-00-351-0542
NSN 1430-01-422-1058
Last modified 05/03/2024