TM 1-1510-224-10
CHAPTER 4
MISSION EQUIPMENT
Section I. MISSION AVIONICS
4-1. MISSION CONTROL PANEL.
a.
Description. The mission control panel (fig. 4-1),
mounted on the copilot's sidewall, consists of three
sections.
The
top
section
contains
the
mission
caution/advisory annunciator panel. The annunciator
panel incorporates all mission annunciators along with
three aircraft system annunciators (CABIN OVERTEMP,
NO INS UPDATE, and INS UPDATE). The center
section contains a digital DC volt/ammeter, digital AC
volt/frequency meters (2), and AC digital load meters (2).
The bottom section contains the mission equipment
control switches and the mission equipment circuit
breakers.
b.
Mission Control Panel Controls, Indicators, and
Functions.
(1)
Mission
annunciator
panel
Mission
annunciator panel functions are described in table 2-8.
(2)
Battery voltmeter. A liquid crystal display
indicator placarded VDC, which indicates aircraft battery
voltage.
(3)
Battery ammeter. A liquid crystal display
indicator placarded AMPS, which indicates aircraft battery
current.
(4)
AC volt-frequency meters. Two liquid
crystal display meters, placarded VAC FREQ indicate the
voltage and frequency output of the # 1 and # 2 three-
phase inverters respectively. The meters indicate the
voltage and -frequency of either the A, B, or C phase of
the inverters, depending on the position of the METERS
switch.
(5)
AC loadmeters. Two liquid crystal display
meters placarded AC% LOAD, indicate the load in
percent on the # I and # 2 three-phase inverters
respectively. The meters indicate the load on either the
A, B, or C phase of the inverters, depending on the
position of the METERS switch.
(6)
Rotating boom antenna operating position
control switch. The rotating boom antenna operating
position control switch, placarded ANT ORIDE, OPR POS
AUTO ROTATE, allows overriding antenna operating
position on the ground or automatic operation. The
antenna normally rotates to a vertical position when the
landing gear is retracted and automatically rotates to a
horizontal position when the landing gear is extended.
Moving the switch to the OPR POS allows rotation of the
antenna to the vertical position while on the ground.
(7)
Mission equipment control switch. The
mission equipment control switch, placarded MISSION
CONTROL ORIDE - AUTO - OFF controls power to the
mission equipment.
(a)
ORIDE.
The
ORIDE
(override)
position is used to apply AC and DC power to the mission
equipment when one generator has failed and the aircraft
is not operating on external power.
(b)
AUTO.
The
AUTO
(automatic)
position applies AC and DC power to the mission
equipment. Power is automatically removed from the
mission equipment if a generator fails, and the aircraft is
not operating on external power.
(c)
OFF. The OFF position removes
power from the mission equipment.
(8)
Radio altimeter switch. The radio altimeter
switch, placarded RADIO ALT ON, OFF, controls
operation of the radio altimeter system. This switch
allows turning off the radio altimeter system to reduce
radio emissions from the aircraft.
(9)
ELINT power switch. The ELINT power
switch, placarded ELINT ON OFF, controls power to the
ELINT mission equipment.
(a)
ON. Applies power to the ELINT
mission equipment.
(b)
OFF. Removes power from the
ELINT mission equipment.
(10)
COMINT power switch. The COMINT
power switch, placarded COMINT ON OFF, controls
power to the CHALS, lowband, and remaining mission
equipment.
(a)
ON. Applies power to the CHALS,
lowband, and remaining mission equipment.
(b)
OFF. Removes power from the
CHALS, lowband, and remaining mission equipment.
4-1