Cirrus Design Section 2
SR20 Limitations
P/N 21399-004 2-17P/N 21399-004 2-17
Taxi Power
Maximum continuous engine speed for taxiing is 1000 RPM on flat,
smooth, hard surfaces. Power settings slightly above 1000 RPM are
permissible to start motion, for turf, soft surfaces, and on inclines. Use
minimum power to maintain taxi speed.
Fuel Limits
Approved Fuel ............... Aviation Grade 100 LL (Blue) or 100 (Green)
Total Fuel Capacity..................................... 58.5 U.S. gallons (221.4 L)
Total Fuel Each Tank...................................29.3 U.S. gallons (110.9 L)
Total Usable Fuel (all flight conditions)....... 56.0 U.S. gallons (212.0 L)
Maximum Allowable Fuel Imbalance............... 7.5 U.S. Gallon (28.4 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 11934-S25 is required.
Maximum Occupancy
Serials w/o 2+1 Rear Seat
Occupancy of this airplane is limited to four persons, the pilot and
three passengers.
Serials w/ 2+1 Rear Seat
Occupancy of this airplane is limited to “4+1” persons, the pilot and
four passengers. If carrying three rear seat passengers, occupants
must be wearing a seat belt and shoulder harness with their hips and
back firmly against the seatback as show in the following illustration. If
Revision A1
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