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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
June 2007
Information Manual 3-25
Cirrus Design Section 3
SR22 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
June 2007
3-26 Information Manual
Section 3 Cirrus Design
Emergency Procedures SR22
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
breakers pulled, autopilot lateral control is available in GPSS steering
mode through GPS 1 and autopilot vertical control is available through
the Vertical Speed (VS) and Altitude (ALT) modes on the autopilot
head. Dim brightness level to black if PFD is found distracting.
PFD - Loss of Air Data
In the event the PFD detects a loss of air data, the affected indicator is
removed from the display and replaced with a red “X”. If loss of air data
occurs, refer to the mechanical standby instruments (altitude,
airspeed) and perform the following procedure:
1. Land as soon as practical.
2. Standby Instruments (altitude, airspeed) .......................MONITOR
If failure occurs while flying in IMC:
3. Exit IMC.
PFD - Loss of Attitude Data
In the event the PFD detects a loss of attitude data, the affected
indicator is removed from the display and replaced with a red “X”. If
　
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