SCHEMPP-HIRTH FLUGZEUGBAU GmbH., KIRCHHEIM/TECK
Ventus-2cM
FLIGHT MANUAL
November
2003
Revision --
7.12.2
+
-
+ -
ELECTRICAL SYSTEM - AVIONIC
M03 RE 832/1
antenna cable
A
B
C
1
F
L
N
K
O
P
H
I
J
BATT.
AVIONIC
E
BATT.
AVIONIC
E
BATT.
ENGINE
red
blue
AWG 18
AWG 18
G
G
A
A Battery 12V / 2 x 7.2Ah or 1 x 28Ah in fuselage nose
or 1x16-18Ah at panel base
B Battery 12V / 1 x 7 - 7.2Ah or 1 x 18Ah at panel base
1 or 2 Batteries 12V / 7 - 7.2Ah r.h.s. of wheel box
D Battery 12V / 7 - 7.2Ah in fin
I
BATT.
ENGINE
BATT.
FIN
BATTERY - MOUNTING POSITIONS
BATT.
AVIONIC
C
1
E Circuit breaker - 6.3A (mounted on battery)
F Fuse board (description on page 7.3.7)
G Bus bar (e.G. AMP-Terminal)
H Main switch Power plant
Main switch Avionic
J Battery selector switch /
K Consumer load fuse (e.G. VHF-Transceiver, E-Vario etc.)
L VHF-Transceiver
M Antenna
N PTT button
O Boom mike
P Speaker
Q Headset connector
R Rotary multipoint switch
(Option)
Low
voltage
indicator
BATT.
AVIONIC
C
2
C
2
BATT.
ENGINE
BATT.
AVIONIC
*)
Parts listed on page 7.12.4
Q
R W
D
battery in fin
BATT.
FIN
M
E
W
bus bar
(e.g. AMP-Terminal)
NOTE:
VHF-Transceiver and other additional equipment
to be wired in compliance with the manufacturer's
instructions and be fused individually.
Summary of Contents for Ventus-2cM
Page 11: ......