2-16
P/N 11934-003
Section 2
Cirrus Design
Limitations
SR20
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
The maximum allowable fuel imbalance is 7.5 U.S. gallons (¼ tank).
Approved Fuel ............... Aviation Grade 100 LL (Blue) or 100 (Green)
Total Fuel Capacity ..................................... 60.5 U.S. gallons (229.0 L)
Total Fuel Each Tank .................................. 30.3 U.S. gallons (114.5 L)
Total Usable Fuel (all flight conditions) ....... 56.0 U.S. gallons (212.0 L)
Maximum Operating Altitude
Maximum Operating Altitude ........................................ 17,500 ft. 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.
Refer to Oxygen System Limitations in this Section.
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
Occupancy of this airplane is limited to four persons (the pilot and
three passengers).
Revision A6
Summary of Contents for SR20
Page 10: ...1 2 P N 11934 003 Section 1 Cirrus Design General SR20 Intentionally Left Blank Revision A3 ...
Page 22: ...2 2 P N 11934 003 Section 2 Cirrus Design Limitations SR20 Placards 2 21 Revision A6 ...
Page 308: ...9 2 P N 11934 003 Section 9 Cirrus Design Supplements SR20 Intentionally Left Blank Reissue A ...