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

2-10 P/N 13999-002 Info Manual
Section 2 Cirrus Design
Limitations SR20
Maneuver Limits
Aerobatic maneuvers, including spins, are prohibited.
• Note •
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.
September 2011