Learjet 60 - Integrated Standby Indicator System (Figure 5-9 B); Integrated Standby Indicator System (ISIS)

LeaQet 60

Pilot's Manual
INTEGRATED STANDBY INDICATOR SYSTEM (ISIS)
(Aircraft 60-249 and Subsequent)
An Integrated Standby Indicator System (ISIS) is
located on the center
instrument
panel
. This indicator is a Smiths Industries
solid state,
graphic display standby indicator system . The system consists
of a self-
sensing
single
box unit and is powered by 28 VDC supplied by EMER
BAT 1 . Power is also
provided to RTU 1 and NAV 1 . This single LCD
indicator provides the pilot and copilot with pitch and
bank angle,
slip/skid indications, altitude, airspeed, Mach number, dual baro-set,
and
Vmo/Mmo indications . Localizer and glideslope deviation is pro-
vided if NAV 1 is tuned to
an ILS . It is designed to mimic the primary
EFIS system .
For a more detailed description of this system, refer to the current
Smiths
Industries Integrated Standby Indicator System Pilot's Guide
(P/N CDK316) .
INTEGRATED STANDBY
INDICATOR SYSTEM
Figure 5-913
PM-123
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