Maneuver Limits; Flight Load Factor Limits; Minimum Flight Crew - Cirrus DESIGN SR20 Information Manual

Section 2
Limitations

Maneuver Limits

Aerobatic maneuvers, including spins, are prohibited.
Because the SR20 has not been certified for spin recovery,
the Cirrus Airframe Parachute System (CAPS) must be
deployed if the airplane departs controlled flight. Refer to
Section 3 – Emergency Procedures, Inadvertent Spiral/Spin
Entry.
This airplane is certified in the normal category and is not designed for
aerobatic operations. Only those operations incidental to normal flight
are approved. These operations include normal stalls, chandelles, lazy
eights, and turns in which the angle of bank is limited to 60° .

Flight Load Factor Limits

Flaps UP (0%), 3000 lb.......................................................+3.8g, -1.9g
Flaps 50%, 3000 lb. ...............................................................+1.9g, -0g
Flaps 100% (Down), 3000 lb. ................................................+1.9g, -0g

Minimum Flight Crew

The minimum flight crew is one pilot.
2-10
• Note •
Cirrus Design
P/N 13999-002 Info Manual
September 2011
SR20