ALIGN ON DC
FAULT DC FAIL
ALIGN Light
Illuminated (white) –
.
steady – the related IRS is operating in the ALIGN mode, the initial ATT mode, or the shutdown cycle
.
flashing – alignment cannot be completed due to IRS detection of:
.
significant difference between previous and entered positions or an unreasonable present position entry
.
no present position entry.
Extinguished –
.
IRS not in ALIGN mode
.
with mode selector in NAV, alignment is complete, and all IRS
information is available
.
with mode selector in ATT, attitude information is available. Heading
information is available following entry of initial magnetic heading.
Copyright . The Boeing Company. See title page for details.
11.10.16 March 28, 2005
Flight Management, Navigation -Controls and Indicators 737 Flight Crew Operations Manual
FAULT Light
Illuminated (amber) – a system fault affecting the related IRS ATT and/or NAV modes has been detected.
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 and 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.
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.
Copyright . The Boeing Company. See title page for details.
Flight Management, Navigation -Controls and Indicators 737 Flight Crew Operations Manual
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.
IRS Transfer Switch
Inertial Reference System (IRS) Transfer Switch
BOTH ON L – switches the flight instruments attitude and heading source to left IRS.
NORMAL – flight instruments attitude and heading source is from default IRS.
BOTH ON R – switches the flight instruments attitude and heading source to right IRS.
Copyright . The Boeing Company. See title page for details.
11.10.18 March 28, 2005
Flight Management, Navigation -Controls and Indicators
Radio Navigation Systems Automatic Direction Finding (ADF) Control
YA613, YA626, YA801 - YA809, YD651 - YD655
Frequency Indicator
Shows the frequency selected with the related frequency selector. Shows if the system is in the ADF or antenna (ANT) mode.
Frequency Selector
Rotate – . outer knob sets the hundreds number
.
middle knob sets the tens number
.
inner knob sets the tenths and ones number.
Mode Selector Switch
ADF –
.
audio reception possible
.
ADF bearing sent to the DUs and the standby radio magnetic indicator. ANT –
.
audio reception optimized
.
no ADF bearing data available. OFF – removes power from selected receiver.
Copyright . The Boeing Company. See title page for details.
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