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will turn green.
If the slats are in motion, the slat position indication and slat surface will turn white.
If the"SLAT FAIL"or " SLAT FAULT" message is displayed,
the slat position indication and slat surface will turn amber.
HALFSPEED
DRIVE OVERHEAT 1
DRIVE OVERHEAT 2
DRIVE OVERHEAT 1−2
SLAT HALFSPD
Synoptic Failure Annunciations Logic
FLIGHT CONTROLS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
10−10−29
FLAP CONTROL SYSTEM
The flap system has three flap panels with four actuators per wing connected to a flaps Power Drive
Unit (PDU), linked through a rigid driveline (torque tubes/bearings) and controlled by the slat/flap
handle position. The PDU is driven by two DC motors connected together in a speed sum
configuration. Each motor is controlled by a single channel SFCU. There is a brake on each flap
motor that is also controlled by the SFCU. The PDU provides protection against an overload and jam
condition.
To protect against asymmetry, there are dual coil brakes and position sensors located on each
outboard station, left and right, that interface with both SFCUs. There are also direction sensors on
the flap system used to detect actuator disconnects. The sensors on the left wing report to SFCU 1
and the sensors on the right wing report to SFCU 2.
Flap System Schematic
SLAT/FLAP
CONTROL
LEVER
FLAT SYSTEM
POWER DRIVE UNIT
ACTUATOR
SFCU 1 SFCU 2
GF1010_037
SENSOR
POSITION
TRANSDUCER
The flap position and surface position is displayed on the EICAS FLIGHT CONTROL synoptic
page. Flap indication is also shown on the EICAS PRIMARY PAGE.
FLIGHT CONTROLS
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
10−10−30
FLAP CONTROL SYSTEM (CONT'D)
Flap Position and Surface Indications
Failure annunciations
can be displayed below
the FLAP label
Flap Position Indication Flap Surface
Slat/Flap surfaces retracted Slat/Flap surfaces extended
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 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
10−10−31
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 41, Jul 08, 2004
CSP 700−6
Volume 2
10−10−32
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 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
10−10−33
SLAT/FLAP PRIMARY EICAS DISPLAY (CONT'D)
　
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