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compartment. The switch is used to cancel the flap aural warning if the flaps cannot be
correctly configured for an OUT/30 landing.
SLAT POSITION FLAP POSITION PLACARD SPEED PROTECTION
IN 0 N/A LATCH
OUT 0 225 GATE
OUT 6 210 kts GATE
OUT 16 210 kts DETENT
OUT 30 185 kts LATCH
SLAT
6
16
30
0
0
OUT
OUT
OUT
OUT
IN
FLAP
SLAT/
FLAP
GX_10_030
Slat/Flap Control Lever
To deploy slats move the
slat selector aft to the position
that corresponds to the required
slat angle.
/flaps,
/flap
/flap
EGPWS
TERRAIN
OFF
G/S WARN
MUTED
FLAP OVRD
OVRD
FLAP OVRD
(safe guarded)
OVRD
Switch
- When selected, mutes
the flap aural warning with the
flaps not in the correct landing
configuration.
GX_10_031
P I LOT T R A I N I N G GU I D E
FLIGHT CONTROLS
10-36 For Training Purposes Only
Sept 04
FLIGHT CONTROL SYNOPTIC DISPLAY
SLAT/FLAP Primary EICAS Display
FLIGHT CONTROLS
FLAP
AIL
ELEV
RUDDER
SLAT OUT
AIL
ELEV
3O
GX_10_032
SLAT Surface "Retracted" Position
The outline of the slat surfaces align
with the wing leading edge.
Slat Surface “Extended”
Position
Slat extended – The
outline of the surface is as
shown.
Flap Surface “Extended”
Position
Flap extended – The
outline of the surface is as
shown.
Flap Surface “Retracted”
Position
The outline of the flap surfaces
align with the wing trailing edge.
5O
O
3.4
75O
115
81
ART
I
G
N
ND
STAB
789 DN DN DN
OUT
3O
GEAR
–TRIMS–
NL RUDDER NR
AIL
LWD RWD
7.2
NU
GX_10_033
Slat Position Indication
Displays symbol and position
annunciation.
Flap Position Indication
Displays symbol and
numerical value.
Slats/Flaps, Spoilers and Gear Position Pop-Up
The pop-up display will be removed from the EICAS
page (in flight only), 30 seconds after the gear and flaps
indicate up, spoilers retracted and no predetermined
malfunctions exist.
The pop-up display will appear with flap selection
greater than zero degrees, gear selected down, spoilers
deployed and/or if any predetermined malfunctions exist.
OUT
3O
For Training Purposes Only
Sept 04
10-37
P I LOT T R A I N I N G GU I D E
FLIGHT CONTROLS
The following represents slat and flap configurations in both serviceable and failure
conditions.
SLATS OUT, FLAPS IN TRANSIT
Wing
Outline
Slat Position
Annunciation
Detent Position
Scale
Slat Surface
Icon
CLEAN: SLATS IN TRANSIT, FLAP 0 DEGREES
SLATS OUT, FLAPS AT 16 DEGREES
EXAMPLES OF SLATS AND FLAPS
FAILURES DETECTED DATA INVALID
GX_10_034
O
IN
O
12
OUT
16
OUT
4 ––
–––
Selected Detent
Flaps Position
Thermometer
Flaps
Readout
P I LOT T R A I N I N G GU I D E
FLIGHT CONTROLS
10-38 For Training Purposes Only
Sept 04
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 Flight Control Units (FCUs)
1 and 2 which process this logic for system(s) operation.
GX_10_035
SLAT SENSORS AND BRAKES FLAP SENSORS AND BRAKES
SLAT ACTUATORS FLAP ACTUATORS
CONTROL MONITOR CONTROL MONITOR
SFCU 1 SFCU 2
FLIGHT CONTROL UNIT 1 FLIGHT CONTROL UNIT 2
S
L
A
T
S
F
L
A
P
S
E
X
T
E
N
D
E
D
E
X
T
E
N
D
E
D
SLAT
PDU
FLAP
PDU
MOTOR MOTOR MOTOR MOTOR
SLAT
6
16
30
0
0
OUT
OUT
OUT
OUT
IN
FLAP
SLAT/
FLAP
For Training Purposes Only
Sept 04
10-39
P I LOT T R A I N I N G GU I D E
FLIGHT CONTROLS
FLAP/SLAT/GEAR EXTENSION SPEED BUGS
　
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