Extra 200 - Page 30

CHAPTER 03
PAGE 6
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RA - FLUGZEUGBAU GmbH
SERVICE MANUAL EXTRA 200
PAGE DATE: 1. July 1996
03-10-05 Fuel System
Tanks: 2 integral wing tanks, 1 center and
1 acro tank behind the firewall
(cockpit side)
Fuel supply: mechanical engine driven pump,
additional electrically operated
boost pump,
03-10-06 Electrical system
Power supply: engine driven 12 V alternator,
integrated DV converter, 28 Ah
starter battery, master switch
Circuits: equiped with automatic circuit
breakers
Ignition: magneto system, independent from
electrical power supply
DESCRIPTION
DESCRIPTION