Cirrus System 55X Autopilot User Manual

Cirrus Design Section 2
SR22T Limitations
P/N 13772-005 2-11P/N 13772-005 2-11
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°.
• Note •
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, Inadvertent Spin Entry.
Flight Load Factor Limits
Flaps UP (0%), 3600 lb. .....................................................+3.8g, -1.9g
Flaps 50%, 3600 lb................................................................+1.9g, -0g
Flaps 100%, 3600 lb..............................................................+1.9g, -0g
Minimum Flight Crew
The minimum flight crew is one pilot.
Original Issue

Cirrus System 55X Autopilot Specifications

General

Brand	Cirrus
Model	System 55X Autopilot
Category	Aircrafts
Language	English