Maneuver Limits; Flight Load Factor Limits; Minimum Flight Crew; Original Issue - Cirrus DESIGN SR20 Pilot's Operating Handbook And Flight Manual

Cirrus Design
SR20

Maneuver Limits

Aerobatic maneuvers are prohibited.
Spins are prohibited.
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°.
Because the aircraft 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, Spins.

Flight Load Factor Limits

Flaps UP (0%), 3050 lb. .....................................................+3.8g, -1.9g
Flaps 50%, 3050 lb................................................................+1.9g, -0g
Flaps 100% (Down), 3050 lb. ................................................+1.9g, -0g

Minimum Flight Crew

The minimum flight crew is one pilot.
P/N 11934-004

Original Issue

• Note •
Section 2
Limitations
2-11