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airplane is airborne or either thrust lever is retarded.
Note: NO TAKEOFF advisory message will appear during taxi, prior to advancing throttles.
AURAL AND VISUAL WARNINGS
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
03−10−26
LANDING CONFIGURATION WARNING
The “GEAR” aural will sound if any gear is not down and locked and the airplane is below 16,500 feet
and:
· The radio altitude is less than 1,000 feet AGL and the descent rate is more than 400 feet per
minute
OR
· The radio altitude is less than 500 feet AGL and at least 2 minutes after ground to air transition
and both throttles are below 25° throttle lever angle (approximately CRZ thrust)
OR
· The radio altitude is less than 500 feet AGL and the flaps position is 30° at any throttle position
NOTE
The “GEAR” aural can not be muted during any of these conditions.
The “Too low gear” (EGPWS) aural warning is heard if any landing gear is not down and locked with
the radio altitude less than 500 feet AGL and the indicated airspeed at less than 190 knots.
If neither radio altimeter is valid, the “GEAR” aural will sound if any gear is not down and locked and
the airplane is below 16,500 feet and landing flaps selected or either thrust lever at idle and:
· 2 minutes after ground to air transition and airspeed less than 191 knots with flaps at 0°.
OR
· 2 minutes after ground to air transition and the airspeed is less than 165 knots.
OR
NOTE
The landing gear horn may be muted (press muted horn switch/light on
landing gear control panel) with one thrust lever at IDLE and airplane
below 16,500 feet and any landing gear not in the down and locked
position and conditions A or B not satisfied.
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
03−10−27
EICAS DISPLAY
GF0310_025
TOTALFUEL(LBS) 41550
1.54 1.54
73.3 73.3
789 789
14600 10000 14600
2350 ND
STAB
NU
NL RUDDER
LWD
NR
TRIMS
N2
FF (PPH)
OIL TEMP
OIL PRESS
93.4
5750
115
81
93.4
5750
115
81
EPR
N1
ITT
AIL
GEAR
OUT
30
DN DN DN
1.65 1.65
7.2
RWD
TOTALFUEL(LBS) 41550
1.54 1.54
73.3 73.3
789 789
14600 10000 14600
2350 ND
STAB
NU
NL RUDDER
LWD RWD
NR
TRIMS
7.2
N2
FF (PPH)
OIL TEMP
OIL PRESS
93.4
5750
115
81
93.4
5750
115
81
EPR
N1
ITT
AIL
1.65 1.65
Crew Alerting System Window
14 message lines with Gear/Slats/Flaps
pop up displayed.
Slats/Flaps, Spoilers and Gear Position Pop Up
The pop up display will be removed from the
primary page (in flight only) 30 seconds after
the gear and flaps indicate up, ans no
predetermined malfunctions exist, or flight
spoilers out.
The pop up display will appear with flap selection
greater than zero degrees, gear selected down
and/or if any predetermined malfunctions exist.
Trims
Indications for Aileron, Rudder and Stabilizer Trim.
For more information see Chapter 10, FLIGHT
CONTROLS.
NOTE
EICAS will automatically be displayed when
airplane is powered up (BATT MASTER ON)
Crew Alerting System Window
24 message lines with Gear/Slats/Flaps
pop up not displayed.
Engine Indicating
Indications of EPR, N1, ITT, N2, FF,
OIL TEMP and OIL PRESSURE. For more
information see Chapter 18, POWER PLANT.
Fuel
Indications of total fuel quantity and
individual tank quantity. For more
information see Chapter 12, FUEL.
AURAL AND VISUAL WARNINGS
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
03−10−28
SYSTEMS DISPLAY (STAT PAGE)
NOTE
SYSTEM display will automatically be displayed when airplane is powered up (BATT MASTER ON).
GF0310_026
OIL QTY (QTS)
ENG
APU
RES
RPM EGT
BRAKE TEMP
10.4
90
13% 13%
100 400
03 03 03 03
4.5
5.0
10.4
OXYGEN
OPEN OPEN
OUTFLOW VALVES
0 0
1 2
1 2
2
APU
%
1
CKPT (°C) AFT
CABIN (°C) CABIN (°C)
FWD
20
1300
20 0.00
CAB ALT
CAB RATE
23 P
19 21 22
CKPT/CABIN Temperature
　
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