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Vertical Speed
Readout
Roll Scale
Boresight Symbol
Airspeed
Readout
Flight Path
Acceleration
Symbol
Pilot’s and copilot’s PFDs will
display a ‘ROLLOUT’ message
upon airplane touchdown.
Rollout Indications on EFIS
AIII
Roll Indicator
Slip/Skid Indicator
Heading Bug
Selected
Course
Bug
DME Distance
Readout
Navigation Source
Indicator
Horizon Line
Heading Scale
Lateral
Deviation Line
REV 56, Jan 31/03
Vol. 1 12--70--42
FLIGHT INSTRUMENTS
Head--Up Guidance System
Flight Crew Operating Manual MASTER
CSP A--013
Primary Mode --- Attitude Indications
Figure 12---70---18 Sheet 1
Slip/Skid Indicator
If displaced from
centre, the airplane is
either slipping or
skidding.
Roll Scale Roll Pointer
Roll angle is displayed
by pointer read against
fixed roll scale .
10 10
AP 10
SYNC
PRI
HDG
ALT
LOC 1
GS
5 5
21
--5 --5
M .545
240
220
200
180
160
VOR 1
10.0 NM
190 GS
ADF1
ADF2
0.0 VS
21 30
2 000
100
900
800
00
000
1
A fixed symbol
centre of the
display),
wherein the
airplane
attitude (pitch
and roll) is
referenced to.
Pitch Scale
5 5
Slip/Skid Indicator
(single engine)
During one--engine
inoperative conditions,
the slip/skid indicator
is repeated below the
the flight path symbol
to reduce pilot
scanning.
Used with the
boresight symbol to
indicate current
airplane pitch attitude.
Vertical tick marks
point to the direction
of the horizon line.
Pitch Scale
(Take--Off / Go--Around Mode)
15 15
When the airplane is in the take--off
mode or the go--around mode (TO,
GA, TO/WS or GA/WS), either the
is displayed without a gap in the
middle (drawn solid) to be used as
a pitch reference during take--off or
go--around.
Markings indicate bank angle (degrees of roll).
tick marks are
only displayed
when the roll
pointer gets to
these tick marks
or beyond. .
Boresight
Symbol
Vol. 1 12--70--43
REV 56, Jan 31/03
FLIGHT INSTRUMENTS
Head--Up Guidance System
Flight Crew Operating Manual
CSP A--013
MASTER
Primary Mode --- Attitude Indications
Figure 12---70---18 Sheet 2
10 10
AP 10
SYNC
PRI
HDG
ALT
LOC 1
GS
5 5
21
--5 --5
M .545
240
220
200
180
160
VOR 1
10.0 NM
190 GS
ADF1
ADF2
0.0 VS
21
30
2 000
100
900
800
00
000
1
Extreme Pitch
Chevron
Points to the
direction of level
flight during
extreme pitch
Horizon Line
The horizon line represents
the airplane’s zero degrees of
pitch attitude (an artificial
horizon which is not adjusted
for the curvature of the earth).
20 20
15 15
10 10
5 5
Pitch Compression
The point of a downward
pointing chevron represents
The point of an upward
pointing chevron represents
Unusual attitudes / Unusual AOAs
An unusual attitude or unusual AOA would result in
either the horizon line or the flight path symbol
exceeding the limits of their display areas. The affected
symbol will then be ghosted (displayed in dashed lines).
In this event, the vertical components of the attitude
display will be compressed to provide a consistent
display which is relatively correct to each other,
although no longer conformal to the outside scene.
REV 56, Jan 31/03
Vol. 1 12--70--44
FLIGHT INSTRUMENTS
Head--Up Guidance System
Flight Crew Operating Manual MASTER
CSP A--013
Primary Mode --- Attitude Indications
Figure 12---70---18 Sheet 3
Attitude Failure Flags
ROL and/or PIT and/or
An IRS failure is indicated by the above
failure flags and the affected attitude data is
removed from the display.
A miscompare is indicated by the same
failure flags but affected attitude data is
retained. The flags flash for 5 seconds
when the miscompare is first detected and
thereafter remain displayed until the
condition is corrected.
V/S
Attitude Source
Default source is ATT 1 and is
not annunciated.
　
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