A
A
I
I
R
R
P
P
L
L
A
A
N
N
E
E
T
T
E
E
C
C
H
H
N
N
I
I
C
C
A
A
L
L
D
D
E
E
S
S
C
C
R
R
I
I
P
P
T
T
I
I
O
O
N
N
,
,
O
O
P
P
E
E
R
R
A
A
T
T
I
I
N
N
G
G
,
,
M
M
A
A
I
I
N
N
T
T
E
E
N
N
A
A
N
N
C
C
E
E
A
A
N
N
D
D
R
R
E
E
P
P
A
A
I
I
R
R
M
M
A
A
N
N
U
U
A
A
L
L
2-49
Document No.:
EV97SLNOEN
Date of Issue:
02/2008
Revision:
-
2.3.18 Wiring
2.3.18.1 Wiring description
The electric system is single-wire type with the negative side connected to the chassis. The power
source is a single-phase generator integral to the engine. A 12V/16Ah maintenancefree battery is
located on the firewall. The system is protected by the main circuit breaker (ACCU) 30 Amps.
The circuits of the particular sections are guarded individually by circuit breakers. Separate
appliances have separate switches.
The dual engine ignition is a separate part of the electrical system. Each ignition circuit has its own
on position on the ignition box to allow ignition check and BOTH position for normal operation.
Piper type external power socket can be installed optionally. Socket is located on the right side of
the fuselage, behind the firewall.
2.3.18.2 Wiring diagram
The wiring system will vary and depends on the instrumentation, electronic equipment, and electric
acessories of your aircraft.
For wiring diagrams of the concrete airplane see Section 6. APPENDICES
2.3.18.3 Circuit breakers
The circuit breakers are generally located under the left-hand side of the instrument panel
–
see
2.3.8.3 Instrument panel.
