BRISTELL S-LSA, Руководство по техническому обслуживанию и инспекции

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11.CHAPTER
– ELECTRICAL SYSTEM
Document: SLSA-MIP-5-4-0-US Date of Issue: 05/2016 Revision: -
11-4
11.2.2 Fuses
Fuses serve for protecting individual electrical circuits from overloading. Every fuse is marked
by the placard with a fuse designation (see Tab. 11-2). Fuses are located on the right
instrument panel. Wiring diagrams are shown in 16.CHAPTER
– WIRING DIAGRAMS.
NOTE
There are not used classical fuses in the aircraft.
Fuses
Designation Description
Current
rating
ALTERNATOR Fuse of alternator 35A
ENG INSTR
Fuse of engine instruments 3A
PANEL INSTR Fuse of panel instruments 5A
NAV LITE Fuse of Nav lites 10A
STROBE LITE Fuse of strobe lites 10A
LAND LITE Fuse of land lite 15A
FUEL PUMP Fuse of fuel pump 10A
RADIO 1 Fuse of radio 1 5A
RADIO 2 Fuse of radio 2 5A
XPONDER
Fuse of transponder 3A
GPS Fuse of GPS 3A
AVIONICS Fuse of avionics 5A
SPARE Spare fuse 10A
Tab. 11-2
Fuses
11.2.3 Generator
Rotax 912 iS internal generator has two isolated coils integrated (individual generators).
During the starting operation, the EMS system is powered by the battery. With sufficient
engine speed generator B takes over this function. After the EMS system check, generator
A takes over the supply of the EMS system (engine), if the switching threshold is exceeded.
Generator B is then used to supply the aircraft instruments and for charging the battery. While
the engine is running, generator B can be used for the board instrumentation.

Generator A 14.2 V/16 A (220 W nominal capacity at 20 °C / 68 °F)

Generator B 14.2 V/30 A (420 W nominal capacity at 20 °C / 68 °F)
NOTE
If generator A fails, generator B takes over its functions. The onboard computer and
instruments will be supplied by the battery. The battery will no longer be charged!