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FLIGHT DESIGN CT - Page 29

FLIGHT DESIGN CT
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Document Title Document No. Revision
Date Section
Supplement S3 to the AMM CTLS-LSA –
CTLS-LSA with ROTAX 912iS
AF 0480 0011 00 05-Aug-12 28-00-2
Approval Ref.: Approved on the Basis of Manufacturer Self Declaration
From shutoff valve fuel flows through a fine filter to the injection lines, the injection valves
and the fuel pressure regulator. The fuel pressure regulator keeps injection pressure at the
desired level and allows surplus fuel to feed back to the header tank. The back-flow line is
also blocked when the fuel shut-off valve is closed.
The Fuel System is presented schematically on the following diagram (Fig. 28-00-1).
Fig. 28-00-1. Scheme of Fuel System

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