CHAPTER 28
PAGE 3
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RA - FLUGZEUGBAU GmbH
SERVICE MANUAL EXTRA 200
PAGE DATE: 1. July 1996
28-00-00 GENERAL
The fuel system (refer to Figure 1) consists of a center tank
(3) with acro tank (5), two wing tanks (1), a fuel selector
valve (2), a gascolator (8) , an electrically driven auxiliary
pump (7) and an engine driven rotary pump (6). Concerning
the fuel drains (4) also refer to Chapter 12-10-03.
On the rear instrument panel one fuel quantity indicator for
the center tank and one for the wing tanks, the switch/circuit
breaker for the boost pump and the circuit breaker for the
indication are installed.
For fuel tank capacities refer to Chapter 12-10-01.
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