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winds to drag the airplane further. As a result of landing impact,
the doors may jam. If the doors cannot be opened, break out the
windows with the egress hammer, located in the console between
the front seats, and crawl through the opening.
March 2010
3-24 Information Manual
Section 3 Cirrus Design
Emergency Procedures SR20
Landing Emergencies
If all attempts to restart the engine fail and a forced landing is
imminent, select a suitable field and prepare for the landing. If flight
conditions or terrain does not permit a safe landing, CAPS deployment
may be required. Refer to Section 10, Safety Information, for CAPS
deployment scenarios and landing considerations.
A suitable field should be chosen as early as possible so that
maximum time will be available to plan and execute the forced landing.
For forced landings on unprepared surfaces, use full flaps if possible.
Land on the main gear and hold the nose wheel off the ground as long
as possible. If engine power is available, before attempting an “off
airport” landing, fly over the landing area at a low but safe altitude to
inspect the terrain for obstructions and surface conditions.
• Note •
Use of full (100%) flaps will reduce glide distance. Full flaps
should not be selected until landing is assured.
Emergency Landing Without Engine Power
1. Best Glide Speed ........................................................ ESTABLISH
2. Radio............................................. Transmit (121.5 MHz) MAYDAY
giving location and intentions
3. Transponder ........................................................... SQUAWK 7700
4. If off airport, ELT ........................................................... ACTIVATE
5. Power Lever ............................................................................IDLE
6. Mixture ............................................................................. CUTOFF
7. Fuel Selector............................................................................OFF
8. Ignition Switch ..........................................................................OFF
9. Fuel Pump................................................................................OFF
10.Flaps (when landing is assured) ...........................................100%
11.Master Switches.......................................................................OFF
12.Seat Belt(s) ................................................................... SECURED
March 2010
Information Manual 3-25
Cirrus Design Section 3
SR20 Emergency Procedures
Ditching
1. Radio ............................................ Transmit (121.5 MHz) MAYDAY
giving location and intentions
2. Transponder ........................................................... SQUAWK 7700
3. CAPS............................................................................. ACTIVATE
If available, life preservers should be donned and life raft should
be prepared for immediate evacuation upon touchdown.
Consider unlatching a door prior to assuming the emergency
landing body position in order to provide a ready escape path.
4. Airplane.........................................................................EVACUATE
It may be necessary to allow some cabin flooding to equalize
pressure on the doors. If the doors cannot be opened, break out
the windows with the egress hammer and crawl through the
opening.
5. Flotation Devices ............ INFLATE WHEN CLEAR OF AIRPLANE
Landing Without Elevator Control
The pitch trim spring cartridge is attached directly to the elevator and
provides a backup should you lose the primary elevator control
system. Set elevator trim for a 80 KIAS approach to landing.
Thereafter, do not change the trim setting until in the landing flare.
During the flare, the nose-down moment resulting from a power
reduction may cause the airplane to hit on the nosewheel. At
touchdown, bring the power lever to idle.
1. Flaps ................................................................................SET 50%
2. Trim ............................................................................SET 80 KIAS
3. Power ....................................AS REQUIRED FOR GLIDE ANGLE
March 2010
3-26 Information Manual
Section 3 Cirrus Design
Emergency Procedures SR20
System Malfunctions
Primary Flight Display System
In the unlikely event of a PFD failure, the pilot may lose the ability to
control the autopilot through the PFD controls. If this malfunction
occurs, the PFD circuit breakers may be pulled and the airplane flown
using the mechanical standby instruments. With the PFD circuit
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