Cirrus System 55X Autopilot User Manual

Cirrus Design Section 3A
SR22T Abnormal Procedures
P/N 13772-005 3A-23P/N 13772-005 3A-23
Other Conditions
Aborted Takeoff
1. Power Lever ............................................................................ IDLE
2. Brakes.................................................................... AS REQUIRED
Amplification
Use as much of the remaining runway as needed to safely bring the
airplane to a stop or to slow the airplane sufficiently to turn off runway.
• Caution •
For maximum brake effectiveness, retract flaps, hold control
yoke full back, and bring the airplane to a stop by smooth,
even application of the brakes.
After a high-speed aborted takeoff, brake temperatures will be
elevated; subsequent aborted takeoffs or other high-energy
use of the brakes may cause brake overheat, failure and
possibly even fire. A 25-minute cooling time is recommended
following high-energy use of the brake system before
attempting to conduct operations that may require further
high-energy braking. Brake temperature indicator should be
inspected prior to flight following a high-energy brake event.
Refer to Section 4, Preflight Inspection Checklist for additional
detail.
Original Issue

Cirrus System 55X Autopilot Specifications

General

Brand	Cirrus
Model	System 55X Autopilot
Category	Aircrafts
Language	English