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.COMPLEMENTARY
FLIGHT MANUAL
SECTION 7.12
.LIGHTING
1
CABIN LIGHTING
The system consists
of a movable spot light,
at the front
for the crew and R
two swivel dome lights.
at the rear, for the passengers.
R
The lamps of the dome lights
are switched on and off by means of two
R
push-buttons.
R
The movable spot light
is used as an emergency light
in case of total
R
lighting
failure.
R
Lighting
is controlled
by means of a potentiometer.
R
.The
movable spot light
is directly
supplied from the battery
and the
R
circuit
is protected
by a fuse.
R
The rear dome lights
are protected
by a fuse on the RH side fuse panel.
For aircraft
equipped with the Public Air Transport
kit,
the rear dome
R
light
is supplied from the battery
direct
busbar and controlled
by means
R
of a switch available
to the pilot.
2
INSTRUMENT PANEL AND CONSOLE LIGHTING
The instruments are lit
by two separate circuits:
R
-LiGhtinG
circuit
1
Supplies:
.the
control
unit
(HONEYWELL) on the console,
R
.the
radio sets on the instrument panel.
R
.the
radio sets on the console.
R
-LiGhtinG
circuit
2
.
Supplies:
.the
indicators
having integrated
lighting.
R
.the
lighting
control
plate.
R
.the
engine control
plate,
R
.the
NR indicator
lighting
fixture,
R
.the
stand-by compass lighting,
controlled
by means of the Day/Night
R
selector,
R
.the
VEMD front face.
R
.R
350 B3
7 .12
00-23
Page 1
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