PILOT’S OPERATING HANDBOOK
Section 7
Airplane and System
Description
2015-07-20
7-15
Doc. No. POH-20101308
7.13 Electrical System
The airplane is equipped with 14 V DC electrical installation. A generator with
power of 250 W is the primary source of electrical energy. The secondary source
of energy is the accumulator 12V/15Ah that is located in the engine compartment
on the fire wall. It is used for engine starting and in case of generator failure as
an emergency source of energy and also serves as the smoothing filter of power
system.
DC voltage is distributed to individual systems by main bus bar. Each system is
protected by circuit breaker. If overloading of any of the circuits occurs, then the
circuit breaker is pulled out. Circuit breakers are listed in the Aircraft
Maintenance and Inspection Procedures.
CAUTION
DO NOT USE CIRCUIT BREAKERS FOR NORMAL
SWITCHING OFF OF THE SYSTEMS.
After switching Master switch (
HAUPTSCHALTER)
on and by turning the ignition
key to
START
position the starter is activated. The starter is power supplied from
the accumulator before engine start. After engine has been started and idle RPM
reached, generator starts supplying current into electrical network.
7.13.1 Lighting
Airplane can be equipped with an external lighting.
External lighting can be composed of position lights and anti-collision beacons
which are located in wing tip and landing headlight which is located in left wing
leading edge or in the lower engine cowling. Position lights are switched by
POS
LICHTER
switch and anti-collision lights by
ACL
switch. Landing headlight is
switched by
REFLEKTOR
switch.
7.13.2 Electrical System Scheme
See Airplane Maintenance Manual for SportStar MAX.
Содержание SportStar MAX
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