Date of Issue: 01/2016
Document No.: LSA-AOI-2-1-0-CL
7.10 Electrical system
Battery
The battery is mounted on the forward side of the firewall.
Master switch
Master switch connects the electrical system to the 12 Volt battery and
charger/coils, controlled by the regulator. See Engine Manual for electrical
system details.
NOTE
Ignition system is independent on the power source and will operate even
with Master switch and/or breaker off.
Ignition Switch
Ignition must be on BOTH to operate the engine: For safety, remove key
when engine is not running.
NOTE
All switches and or engine controls are "up" or "push forward" for
operation, except the choke, cabin heat and carburetor pre-heat, which is
"Pull" for "on". Optional equipment, switches and/or fuses are subject to
change or installed as requested. See Aircraft Equipment List and Photo
and Description of equipment and controls in the cockpit.
7.11 Pitot and static pressure system
Pitot tube (optionally heated) is located below the left wing. Pressure
distribution to the instruments is through flexible plastic hoses.
Static ports are located on both sides of the fuselage at the tail.
Keep the pitot head clean to ensure proper function of the system.
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