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in hours and minutes.
CHR time is displayed
in minutes.
CHR
Used to start, stop and
reset the CHR display
and second hand.
Overrides existing
elapsed time display.
First push starts
chronometer
Second push holds
chronometer readout
and second hand
Third push resets
second hand to zero
and returns display to
elapsed time
During time setting,
CHR button is used to
increment applicable
value.
ET
Controls elapsed time
readout and during time
setting, selects the
parameter to be set.
Flashing parameter can
be incremented by
pressing CHR.
Second Hand
NOTE
ET time corresponds to
airplane flight time and
starts when the airplane
takes off and stops at
touch down. ET can
only be reset on ground.
Effectivity:
Airplanes 7002 to 7672.
Vol. 1 12--60--11
REV 56, Jan 31/03
FLIGHT INSTRUMENTS
Standby Instruments and Clocks
Flight Crew Operating Manual
CSP A--013
MASTER
Clock Display <Airplanes 7673 and Subsequent>
Figure 12---60---8
MODE
Used in conjunction with ET SEL
and ET RST buttons to set UTC
time, date, and local time.
CHR
Used to start, stop and
reset the chronometer
display. Overrides
existing elapsed time
display.
ET RST
Used to reset the
elapsed time function
when the airplane is on
the ground.
Also used to increase the
data in one digit
increments during
manual setting of the
clock.
ET/CHR Display
Displays elapsed time
or chronometer time.
RST
SEL
ET
MODE
CHR
INT
CHR
Time/Date Display
Displays GPS time,
internal UTC time, local
time or date.
Time is displayed in
hours, minutes, and
seconds (HH:MMss)
DATE is displayed as
Day/Month/Year.
Mode annunciator
Indicates the present
mode of operation.
DT -- date
GPS -- GPS synchro--
nization enabled
INT -- internal time/
date operation (GPS
disabled).
LT -- local time
NOTE
ET time corresponds to
airplane flight time and
starts when the airplane
takes off and stops at
touch down. ET can
only be reset on ground.
Effectivity:
Airplanes 7673 and subsequent.
ET SEL
Used to select the
elapsed time function
when the chronometer
function is active.
Also used to decrease the
data in one digit
increments during
manual setting of the
clock.
REV 56, Jan 31/03
Vol. 1 12--60--12
FLIGHT INSTRUMENTS
Standby Instruments and Clocks
Flight Crew Operating Manual MASTER
CSP A--013
F. System Circuit Breakers
SYSTEM SUB--SYSTEM CB NAME BUS BAR CB
PANEL
CB
LOCATION
NOTES
Standby
Attitude
Indicator
STBY HORIZ
Standby
Airspeed,
Altitude,
Attitude
Indicator
STBY INSTR
DC BAT 2 N10
Standby
Integrated
Standby
Instrument
<0083>
INT STBY
INST
Instruments
CLK 1 MAIN BAT
DIR 5 A10
Clocks (A/C CLOCK 1 DC BAT 2 N11
7002 to 7672)
CLK 2 MAIN BAT
DIR 5 A11
CLOCK 2 DC BUS 2 2 H5
CLOCK 1
DC BAT 2 N11
Clocks (A/C
7673 and
MAIN BAT
6
B7
subsequent) CLOCK 2
DIR B8
DC BUS 2 2 H5
Vol. 1 12--70--1
REV 56, Jan 31/03
FLIGHT INSTRUMENTS
Head--Up Guidance System
Flight Crew Operating Manual
CSP A--013
MASTER
1. HEAD--UP GUIDANCE SYSTEM <0026>
The head--up guidance system (HGS) projects instrument and airplane systems data
holographically between the pilot and the pilot’s windshield. Attitude, airspeed, flight path
guidance and other information are displayed in symbolic format. HGS allows the pilot to fly
the airplane during Category IIIa instrument approaches in a head--up position. A combiner
optically diffracts (reflects) flight symbology to infinity and allows the pilot to look through the
display without eye movement or shift in eye focus.
HGS consists of the following:
S Combiner,
The combiner is mounted on the pilot’s windshield frame and can be used during ground
and flight operations. The combiner is deployed and stowed by actuating a lever on the
RH side. An infrared transmitter and alignment detector automatically check if the optical
element/combiner is out of position. The combiner also incorporates a manual/automatic
brightness control.
　
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