TM 1-1510-224-10
Operation of the system is through the aircraft
survivability
equipment/avionics
control
system
(ASE/ACS). Depressing L1 when the UTILITY page is
displayed will call up the DATA TRANSFER page.
4-8.
AIRCRAFT
SURVIVABILITY
EQUIPMENT/
AVIONICS CONTROL SYSTEM (ASE/ACS).
The aircraft survivability equipment/avionics control
system (ASE/ACS) consists of a multifunction display
(MFD), a keyboard unit (KU), and a remote terminal unit
(RTU). The ASE/ACS is the primary way that the flight
crew interfaces with the following systems:
UHF Transceiver (AN/ARC/164), (two each)
VHF-FM (SINCGARS, AN/ARC-201A)
Inertial Navigation System
Global Positioning System
Voice Security System (KY-58)
Flare and Chaff Dispenser System (M-130)
Radar Signal Detecting Set (AN/APR-39(V)I)
Radar Signal Detecting Set (AN/APR-39(V)2)
Radar Warning Receiver (AN/APR-44(V)3)
Prime
Mission
Equipment
Intercommunications
Control Panels (2 each, C-499/AIC)
For operation of the Aircraft Survivability Equipment/
Avionics Control System (ASE/ACS) refer to latest
Operator's
Manual
for
the
Aircraft
Survivability
Equipment/ Avionics Control System (ASE/ACS) for the
RC-12 Guardrail/Common Sensor Aircraft.
4-11/(4-12 blank)
