Rans S-20 RAVEN, Текстовое руководство

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RANS S-20 RAVEN TEXT MANUAL
13A-4
09/01/2013
FUEL LIMITATIONS
Approved Fuel Grades: .......................................................... Dependent on engine used
Fuel Capacity with 2.75 gallon header tank:
Total Capacity: ............................................................................. 28.75 U.S. GAL
Total Capacity each Wing Tank: ........................................................ 13 U.S. GAL
Header Tank Capacity .................................................................... 2.75 U.S. GAL
Total Usable: ............................................................................... 28.45 U.S. GAL
Total Unusable: ................................................................................ 0.3 U.S. GAL
OR
Fuel Capacity with 6.9 gallon header tank:
Total Capacity: ................................................................................ 32.9 U.S. GAL
Total Capacity each Wing Tank: ........................................................ 13 U.S. GAL
Header Tank Capacity ...................................................................... 6.9 U.S. GAL
Total Usable: ................................................................................. 32.6 U.S. GAL
Total Unusable: ................................................................................ 0.3 U.S. GAL
►NOTE:
Due to cross feeding between fuel tanks, the tanks should be re-topped after
each refueling to assure maximum capacity.
The fuel quantity indicator is calibrated to read correct in horizontal level flight
(cruise) only.
The readings given by the fuel quantity indicator in 3-wheel ground attitude (taildragger)
are therefore not correct.
The fuel remaining in the tanks after the fuel quantity indicator reads zero (in level flight
attitude in cruise condition) cannot be safely used in flight.
OTHER LIMITATIONS
Flap Limitations:
Approved Takeoff Range: ................... retracted, 1
st
or 2
nd
notch flaps (0° to 24.5°)
Approved Landing Range: .................................... retracted to full flaps (0° to 49°)