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Boeing 737-800
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737 Flight Crew Operations Manual
Flight Management, Navigation -
Controls and Indicators
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
11.10.18 D6-27370-866-EGP
3 Inertial Reference System (IRS) Mode Selector
OFF –
alignment is lost
all electrical power is removed from the system after a 30 second
shutdown cycle.
ALIGN –
rotating the selector from OFF to ALIGN initiates the alignment cycle
rotating the selector from NAV to ALIGN automatically updates
alignment and zeroes ground speed error.
NAV (detented position) –
system enters the NAV mode after completion of the alignment cycle
and entry of present position
in NAV mode, all IRS information is available to airplane systems for
normal operations.
ATT – provides only attitude and heading information:
attitude information is invalid (attitude flag in view) until ALIGN light
is extinguished
heading information is invalid (heading flags in view) until the actual
magnetic heading is manually entered after the ALIGN light is
extinguished
position and ground speed information is not available until the IRS is
aligned on the ground
the selector must be cycled to OFF before reselecting ALIGN or NAV.
4 ON DC Light
Illuminated (amber)
the related IRS is operating on DC power from the switched hot battery
bus (AC power not normal)
if on the ground, the ground–call horn in the nose wheel well sounds,
providing an alert that a battery drain condition exists
momentary illumination is normal during alignment self–test.
5 DC FAIL Light
Illuminated (amber) –
DC power for the related IRS is not normal
if the other lights are extinguished, the IRS is operating normally on AC
power.
September 15, 2016

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