Cirrus Design
SR22
Fuel Limits
Approved Fuel ............... Aviation Grade 100 LL (Blue) or 100 (Green)
Total Fuel Capacity...................................... 94.5 U.S. Gallon (358.0 L)
Total Fuel Each Tank ................................. 47.25 U.S. Gallon (179.0 L)
Total Usable Fuel (all flight conditions) ........ 92.0 U.S. Gallon (348.0 L)
Maximum Allowable Fuel Imbalance ............. 10.0 U.S. Gallon (37.9 L)
The fuel pump must be set to BOOST for takeoff, climb, landing, and
for switching fuel tanks.
Altitude Limits
Maximum Takeoff Altitude ..........................................10,000 Feet MSL
Maximum Operating Altitude ......................................17,500 Feet MSL
The operating rules (FAR Part 91 and FAR Part 135) require the use of
supplemental oxygen at specified altitudes below the maximum
operating altitude.
Environmental Conditions
For operation of the airplane below an outside air temperature of -10°F
(-23°C), use of cowl inlet covers approved by Cirrus Design and listed
in the Winterization Kit AFM Supplement P/N 13772-118 is required.
P/N 13772-004
P/N 13772-004
Original Issue
Section 2
Limitations
2-17
2-17