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Aborted Takeoff
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 the
runway.
1. Power Lever ............................................................................ IDLE
2. Brakes.................................................................... AS REQUIRED
• 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 to avoid loss of control and/or a
blown tire.
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 Preflight Walk-Around Checklist for detail).
March 2010
3A-6 Information Manual
Section 3A Cirrus Design
Abnormal Procedures SR20
In-Flight Procedures
Inadvertent Icing Encounter
Flight into known icing conditions is prohibited. However, If icing is
inadvertently encountered:
1. Pitot Heat .................................................................................. ON
2. Exit icing conditions. Turn back or change altitude.
3. Cabin Heat .................................................................... MAXIMUM
4. Windshield Defrost ......................................................FULL OPEN
5. Alternate Induction Air............................................................... ON
Inadvertent IMC Encounter
Upon entering IMC, a pilot who is not completely proficient in
instrument flying should rely upon the autopilot to execute a 180° turn
to exit the conditions. Immediate action should be made to turn back
as follows:
1. Airplane Control ........................Establish Straight and Level Flight
2. Autopilot ............................... Engage to hold Heading and Altitude
3. Heading.................................................. Reset to initiate 180° turn
Door Open In Flight
The doors on the SR20 will remain 1-3 inches open in flight if not
latched. If this is discovered on takeoff roll, abort takeoff if practical. If
already airborne:
1. Airspeed...............................................REDUCE TO 80 – 90 KIAS
2. Land as soon as practical.
March 2010
Information Manual 3A-7
Cirrus Design Section 3A
SR20 Abnormal Procedures
Landing Procedures
Landing With Failed Brakes
One brake inoperative
1. Land on the side of runway corresponding to the inoperative
brake.
2. Maintain directional control using rudder and working brake.
Both brakes inoperative
1. Divert to the longest, widest runway with the most direct
headwind.
2. Land on downwind side of the runway.
3. Use the rudder for obstacle avoidance.
• Note •
Rudder effectiveness will decrease with decreasing airspeed.
4. Perform Emergency Engine Shutdown on Ground checklist.
Landing With Flat Tire
If a flat tire or tread separation occurs during takeoff and you cannot
abort, land as soon as conditions permit.
Main Gear
1. Land on the side of the runway corresponding to the good tire.
2. Maintain directional control with the brakes and rudder.
3. Do not taxi. Stop the airplane and perform a normal engine
shutdown.
Nose Gear
1. Land in the center of the runway.
2. Hold the nosewheel off the ground as long as possible.
3. Do not taxi. Stop the airplane and perform a normal engine
shutdown.
March 2010
3A-8 Information Manual
Section 3A Cirrus Design
Abnormal Procedures SR20
System Malfunctions
Alternator Failure
Abnormal ammeter indications and illumination of the LOW VOLTS
warning light may indicate electrical power supply system
malfunctions. A broken alternator drive belt, wiring fault or a defective
alternator control unit is most likely the cause of the alternator failure.
Usually, electrical power malfunctions are indicated by an excessive
rate of charge or a discharge rate.
Ammeter Indicates Excessive Rate of Charge
After starting engine and heavy electrical usage at low RPM, the
battery will be low enough to accept above normal charging during the
initial part of a flight. However, the ammeter should be indicating less
than two needle widths of charging current after thirty minutes of
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