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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
3-16 Information Manual
Section 3 Cirrus Design
Emergency Procedures SR22
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
Cirrus Design Section 3
SR22 Emergency Procedures
Information Manual 3-17
Engine System Emergencies
Oil Pressure Out of Range
OIL PRESS Warning
Oil pressure below 10 psi or above 100 psi. If low oil pressure is low,
the engine has probably lost a significant amount of its oil and engine
failure may be imminent. Immediately reduce engine power to idle and
select a suitable forced landing field.
If low oil pressure is accompanied by normal oil temperature, it is
possible that the oil pressure sensor, gage, or relief valve is
malfunctioning. In any case, land as soon as practical and determine
cause.
• Note •
This message will appear prior to engine start and should
clear after engine start.
1. Oil Pressure Gage ............................................................. CHECK
If pressure normal:
a. If On-Ground .......................... CORRECT PRIOR TO FLIGHT
　
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