Pdimensions: height 14.1, width 20.9, depth 15.8, weigh (lbs) 102.0, volume (cu.Ft.) crated 2.7; control indicator unit (ciu) is located in the control room, ciu contains the logic circuit and indicators that are required to operate and monitor the dawg, it is arranged with the electrical switches and indicators on the front panel, the electronic assemblies within the case, and the electrical connectors on the back of the case, the power interlock switch and precondition switch are all located within the case; the front panel is organized to enable an operator to perform two functions: control and status monitoring and test; the control and status portion of the penl is divided into three sections, which are laeled system status, system stopped, and system control; ciu electronics are divided into two separate assemblies designated a1 and a2; a1 consists of internally mounted power supplies and connectors while a2 consists of logic circuit boards mounted in a slide-out drawer
A component which performs the dual function of presenting visual information from other sources such as navigation, radar and the like and regulating the mode of operation of those sources. This item is essential to the end use or operation of the other sources. See also control-monitor.
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 6110-00-534-1441
NSN 5836-01-053-5729
NSN 1240-00-536-5557
NSN 6110-01-607-1351
NSN 5805-01-058-4808
NSN 7050-01-146-8433
NSN 6675-01-442-2105
NSN 5831-01-290-3697
NSN 1240-00-555-1661
NSN 6110-01-274-8039
NSN 5841-01-378-5758
NSN 5831-01-010-3519
Last modified 11/08/2024