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GF1010_038
FLIGHT CONTROLS
SLAT IN
FLAP 0
AIL
ELEV
RUDDER
AIL
ELEV
FLIGHT CONTROLS
SLAT OUT
FLAP 30
AIL
ELEV
RUDDER
AIL
ELEV
If the flaps are at commanded position, the flap position indication and flap surface
will turn green.
If the flaps are in motion, the flap position indication and flap surface will turn white.
If the"FLAP FAIL"or "FLAP FAULT" message is displayed,
the flap position indication and flap surface will turn amber.
HALFSPEED
DRIVE OVERHEAT 1
DRIVE OVERHEAT 2
DRIVE OVERHEAT 1−2
FLAP HALFSPD
Flap Position Indication and Surface color
Synoptic Failure Annunciations Logic
FLIGHT CONTROLS
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
10−10−33
SLAT/FLAP CONTROL LEVER
An integrated slat/flap control lever located in the flight compartment (centre pedestal) will command
position of the slat/flap system operation.
Slat/Flap Control Lever
To deploy slat/flap: move the
slat/flap control lever aft to
the position that corresponds
to the required slat/flap angle.
GF1010_039
The slat/flap configuration is as follows:
SLAT POSITION FLAP POSITION PLACARD SPEED PROTECTION
IN 0 N/A LATCH
OUT 0 225 kts GATE
OUT 6 210 kts GATE
OUT 16 210 kts DETENT
OUT 30 185 kts LATCH
FLAP OVERRIDE SWITCH
A flap override switch is located on the centre pedestal in the flight compartment. The switch is used
to cancel the flap aural warning if the flaps cannot be correct configured for OUT/30 landing.
EGPWS FLAP OVRD (safe guarded)
Switch
FLAP OVRD − When selected, mutes
the flap aural warning with the flaps not
in the correct landing configuration.
GF1010_041
EGPWS
MUTED OVRD OFF
FLIGHT CONTROLS
Flight Crew Operating Manual Rev 2A, Apr 11, 2005
CSP 700−5000−6
Volume 2
10−10−34
FLIGHT CONTROL SYNOPTIC DISPLAY
FLIGHT CONTROLS
SLAT OUT
FLAP 30
AIL
ELEV
RUDDER
AIL
ELEV
GF1010_042
SLAT/FLAP PRIMARY EICAS DISPLAY
GEAR
OUT
30
DN DN DN
ND
STAB
NU
NL RUDDER
LWD RWD
NR
TRIMS
7.2
AIL
FLIGHT CONTROLS
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
10−10−35
SLAT/FLAP PRIMARY EICAS DISPLAY (CONT'D)
The following represents slat and flap configurations in both serviceable and failure conditions.
FLIGHT CONTROLS
Flight Crew Operating Manual Rev 2A, Apr 11, 2005
CSP 700−5000−6
Volume 2
10−10−36
SLAT/FLAP OPERATION
Both SFCU 1 and 2 receive input signals from the slat/flap control lever. The SFCUs then release the
brakes from the motor drive units of the PDUs and asymmetry brake detectors. The PDU powers the
driveline and actuators to achieve slat/flap travel.
The position sensors return signals to the SFCUs to confirm correct operation of speed, rotation and
position. Each SFCU sends signals to FCUs 1 and 2 which process this logic for system(s) operation.
SLAT/FLAPS SCHEMATIC
GF1010_045a
FLIGHT CONTROLS
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
10−10−37
FLAP/SLAT/GEAR EXTENSION SPEED BUGS
The flap/slat/gear extension speed bugs are displayed as a sideways letter “T”, as illustrated
below.
The flap/slat/gear extension speed bugs are displayed in a fixed position on the airspeed tape and
will go out of view beyond the ends of the airspeed tape.
NOTE
Speed bugs are displayed at 18,000 feet and below or with
Flap/Slat/Gear out.
The flap/slat/gear extension speed symbols are as follows:
250
240
230
220
210
200
190
180
240
215
6
4
GF1010_047a
FLIGHT CONTROLS
Flight Crew Operating Manual Rev 2A, Apr 11, 2005
CSP 700−5000−6
Volume 2
10−10−38
SLAT/FLAP EICAS MESSAGES
CONFIG SLAT/FLAP
SLAT FAULT
SLAT HALFSPD
FLAP HALFSPD
SLAT DRIVE OVHT
FLAP DRIVE OVHT
SLATFLAP
BIT
FLAP FAULT
"NO TAKEOFF"
FLAP HALFSPD
SLATFLAP
BIT
FLAP FAIL
SLAT FAULT
SLAT HALFSPD
SLAT FAIL
FLAP FAULT
SLAT FAIL
FLAP FAIL
GF1010_048a
FLIGHT CONTROLS
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual
　
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