Aircraft Type: CTSW
FLIGHT DESIGN
Aircraft Operating Instructions
Page: 3-2
AU 010 01000
Rev. No: 7
Original Issue Date: 28-Feb-2005
Revision Date: 29-Apr-2008
3.2 Propeller
For a complete description of the propeller see Operator’s Manual for appropriate propeller
Applicability
CTSW
Classic Light
CTSW
Classic
CTSW
Advanced
Neuform TXR-65, 2-blade
•
Neuform CR3-65, 3-blade
• •
Kaspar, 3-blade in-flight adjustable
•* •*
* - available as an option
3.3 Fuel and fuel capacity
The fuel valve is purely on/off and has to be in the appropriate maximum position. This
engine does not have a mixture valve or require leaning.
Fuel specification: Premium Automotive Unleaded per ASTM D 4814, minimum AKI 91
for Rotax 912ULS.
SUPER leaded, DIN 51600, ONORM C 1103
EURO-SUPER ROZ 95 unleaded, DIN 51603, ONORM 1101
SUPER PLUS ROZ 98 unleaded, DIN 51607, ONORM 1100
AVGAS 100 LL.
ATTENTION!
AVGAS loads the valve seats with high lead content and forms more
combustion chamber deposits and should be used only in case of
vapor lock or insufficient octane on auto fuel.
Each wing has an integral fuel tank with a capacity of 65l / 17 U.S. gallons of which 62l /
16.5 gallons are usable.
The total fuel capacity is 130l / 34 U.S. gallons of which 124l / 33 gallons are usable.
For complete fuel specifications see the Rotax 912 Operator’s Manual
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