FLIGHT CONTROLS
Description
Aircraft Operations Manual
8.1
PAGE 9
Apr 01/15
B
FLAPS light (amber).
The FLAPS light comes on if there is a
malfunction in the flap electrical control
system. The light will also come on when
FLAPS test switch is activated.
Axxxxx
A
TEST 1
STALL
FIRE
LAMPS FLAPS
UPR
LWR
AUTOCOARS
L
R
FUEL
L
R
BLD LEAK
L
R
SMOKE
FIRE SHORT
1
2
ACC
+
TEST 1 PANEL
B
L ENG
OIL PRESS
A
B
C
D
1
2
3
4
5
6
7
8
9
10
1
2
3
4
5
6
7
8
9
10
L ENG
FIRE
AVIONIC
SMOKE
CARGO
SMOKE
LAV
SMOKE
CABIN
PRESS
R ENG
FIRE
R ENG
OIL PRESS
L TAIL P
HOT
R TAIL P
HOT
PROP
BRAKE
AUTO
TRIM
AUTO
COARSEN
CONFIG
PITCH
TRIM
RUDDER
LIMIT
L FIRE
DET FAIL
R FIRE
DET FAIL
FUEL
ELEC
ICE
PROT
ENGINE
FLAPS
AIRCOND
PARK
BRK ON
HYDR
EMER LTS
UNARMED
OXYGEN
DOORS
AVIONICS
VENT
AVIONICS
A
−
SKID
INOP
L STALL
FAIL
GUST
LOCK
PUSHER
SYSTEM
R STALL
FAIL
CENTRAL WARNING PANEL
RST
L
R
A
PITCH TRIM light (amber).
The PITCH TRIM lights comes on when
pitch trim synchronization is deactivated.
GUST LOCK light (amber).
The GUST LOCK light comes on if gust
lock handle is in off position but the
rudder gust lock remains engaged.
FLAPS test light (green).
Comes on flashing when FLAPS test
switch is activated and the flap position
does not correspond to flap handle posi-
tion or the flap system is inoperative.
Comes on steady when FLAPS test
switch is activated and the flap position
corresponds to flap handle position and
the flap system is operative. It can also
come on if a flap fault is detected and the
FLAPS light on the CWP is on.
FLAPS test switch.
When actived, the FLAPS light on CWP
with associated warnings, and flaps test
light come on steady indicating an opera-
tive system.
CONFIG light (red).
The CONFIG light comes on when apply-
ing take
−
off power on ground for:
−
Pitch trim tabs out of take
−
off range
(green band).
−
CL not in MAX position.
−
Flaps not in take
−
off position.
RUDDER LIMIT light (amber).
The RUDDER LIMIT light comes on if the
rudder limiting system fails.
Fig. 5 Flight controls
−
controls and indicators