7-13
DESCRIPTION OF AIRPLANE AND SYSTEMS / INSTRUMENTS
ICON A5 / PILOT’S OPERATING HANDBOOK
CHANGE A3
CHA
P
TER
7
7.6
INSTRUMENTS
7.6.1
GENERAL INFORMATION
FIGURE 7-4
INSTRUMENT STACK
The flight, engine, and fuel instruments in the A5 have been located
according to their priority for controlling the aircraft. The most
prominent instruments used for aircraft control form the Primary
Cluster across the top of the instrument stack. These include the
angle of attack (AOA) gauge (1), airspeed indicator (2), and altimeter
(3). The AOA gauge collects data from ports located on the leading
edge of the left wing. The face of the gauge incorporates a unique
ICON design employing green, yellow, and red segments to clearly
indicate available lift margin above stall at all times. The airspeed
indicator and altimeter are electric gauges connected to the
pitot-static system. In the remote event of a complete electrical
failure each gauge has a backup battery that will power the gauge
for a minimum of 30 minutes. If the backup battery is allowed to fully
charge under normal use, the altimeter digital displays will remain
illuminated for approximately 30 minutes once the master switch is
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