SLF/VREF
GROUND SPEED/MACH READOUT
Airspeed Tape
Figure 10A
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305M
MINIMUM
SELECTED DESCENT 1 000 ALTITUDE
ALTITUDE
MDA
-130
LANDING
ALTITUDE
ALERT BAR
CURRENT ALTITUDE
LANDING
ALTITUDE
CAUTION BAR
MINIMUM DECISION ALTITUDE
LANDING ALTITUDE LANDING
REFERENCE BUG ALTITUDE
QFE
BAROMETRIC
REFERENCE
STD
QFE/QNE
1013 HPA
ANNUNCIATION
Barometric Altitude Tape
Figure 10B
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FCC
IRS
SELECTED
FLIGHT
AIRSPEED PATH IRS VECTOR ATTITUDE
FMCS LANDING/TAKEOFF SPEEDS
SWC
MAX/MIN
AIRSPEED
ADC
COMPUTED
AIRSPEED
ADC
MACH
FMCS TRACK FCC FLIGHT DIRECTOR
ADC ALTITUDE
IRS VERTICAL SPEED
ILS GLIDESLOPE
RADIO ALTIMETER
IRS EFIS CP
HEADING DECISION HEIGHT
PFD Failure Flags
Figure 10C
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TCAS Resolution Advisory Symbols
Figure 10D
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B. Engaged Pitch Mode
(1)
The engaged autopilot pitch mode is indicated by one of the
following messages.
TO/GA
ALT
V/S
VNAV
FLCH SPD
G/S
FLARE
VNAV PTH
VNAV SPD
VNAV ALT
(2)
A change in the engaged mode is annunciated by a green colored box displayed around the message for ten seconds.
(3)
An invalid FCC/FMC pitch mode is indicated by a blank message field.
(4)
An FCC/FMC engaged pitch mode fault is indicated by a yellow colored horizontal line displayed through the center of the message.
C. Engaged Roll Mode
(1)
The engaged autopilot roll mode is indicated by one of the
following messages.
HDG HOLD
HDG SEL
LNAV
LOC
B/CRS
ROLLOUT
ATT
TO/GA
(2)
A change of the engaged mode is annunciated by a green colored box displayed around the message for ten seconds.
(3)
An invalid FCC roll mode is indicated by a blank message field.
(4)
An FCC engaged roll mode fault is indicated by a yellow colored horizontal line displayed through the center of the message.
D. Armed Pitch Mode
(1)
The armed autopilot pitch mode is indicated by one of the
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