SC-POH-1-1-17
SECTION 7
DESCRIPTION OF
AIRPLANE AND SYSTEMS
Revision: -
Date of issue: 2011-09-01
S
S
p
p
o
o
r
r
t
t
C
C
r
r
u
u
i
i
s
s
e
e
r
r
7-7
CAUTION
Do not overfill the tanks to avoid fuel overflow through venting tubes.
7.12 Electrical system
Generator
The AC generator
(250 W AC)
is integrated in the engine and it is connected
to the electric bus through the external rectifier regulator
(12 V 20 A DC)
.
Battery
The
12 V
battery is mounted on the front side of firewall.
Master battery switch
MASTER BAT
switch connects the
12 V
battery to the electrical system.
Master generator switch
MASTER GEN
switch connects the alternator to the electrical system.
Circuit breakers and switches
NOTE
Circuit breakers and switches description is shown in
Section 9, Supplement No. 02.
7.13 Instruments and Avionics
NOTE
Instruments and avionics description is shown in
Section 9, Supplement No. 02.
NOTE
For instruments and avionics operating instructions refer to the documentation
supplied with the instruments and avionics.
7.14 Pitot-static system
Standard
AVIATIK
WA037383 pitot-static probe
is located below the left
wing. Pressure distribution to the instruments is through flexible plastic hoses.
Keep the pitot head clean to ensure proper function of the system.
