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should be memorized for accomplishment without reference to the
procedure.
March 2010
Information Manual 3-7
Cirrus Design Section 3
SR20 Emergency Procedures
Ground Emergencies
Engine Fire During Start
A fire during engine start may be caused by fuel igniting in the fuel
induction system. If this occurs, attempt to draw the fire back into the
engine by continuing to crank the engine.
1. Mixture ..............................................................................CUTOFF
2. Fuel Pump ...............................................................................OFF
3. Fuel Selector............................................................................OFF
4. Power Lever ..................................................................FORWARD
5. Starter ............................................................................... CRANK
6. If flames persist, perform Emergency Engine Shutdown on
Ground and Emergency Ground Egress checklists.
Emergency Engine Shutdown On Ground
1. Power Lever ............................................................................ IDLE
2. Fuel Pump (if used) .................................................................OFF
3. Mixture ..............................................................................CUTOFF
4. Fuel Selector............................................................................OFF
5. Ignition Switch..........................................................................OFF
6. Bat-Alt Master Switches...........................................................OFF
March 2010
3-8 Information Manual
Section 3 Cirrus Design
Emergency Procedures SR20
Emergency Ground Egress
• WARNING •
While exiting the airplane, make sure evacuation path is clear
of other aircraft, spinning propellers, and other hazards.
1. Engine........................................................................SHUTDOWN
• Note •
If the engine is left running, set the Parking Brake prior to
evacuating the airplane.
2. Seat belts ....................................................................... RELEASE
3. Airplane...................................................................................EXIT
• Note •
If the doors cannot be opened, break out the windows with
egress hammer, located in the console between the front
seats, and crawl through the opening.
March 2010
Information Manual 3-9
Cirrus Design Section 3
SR20 Emergency Procedures
In-Flight Emergencies
Engine Failure On Takeoff (Low Altitude)
If the engine fails immediately after becoming airborne, abort on the
runway if possible. If altitude precludes a runway stop but is not
sufficient to restart the engine, lower the nose to maintain airspeed
and establish a glide attitude. In most cases, the landing should be
made straight ahead, turning only to avoid obstructions. After
establishing a glide for landing, perform as many of the checklist items
as time permits.
• WARNING •
If a turn back to the runway is elected, be very careful not to
stall the airplane.
1. Best Glide or Landing Speed (as appropriate) .......... ESTABLISH
2. Mixture ..............................................................................CUTOFF
3. Fuel Selector............................................................................OFF
4. Ignition Switch..........................................................................OFF
5. Flaps ...................................................................... AS REQUIRED
If time permits:
6. Power Lever ............................................................................ IDLE
7. Fuel Pump ...............................................................................OFF
8. Bat-Alt Master Switches...........................................................OFF
9. Seat Belts ..................................................... ENSURE SECURED
March 2010
3-10 Information Manual
Section 3 Cirrus Design
Emergency Procedures SR20
Maximum Glide
Best Glide Speed
3000 lb 96 KIAS
2500 lb 87 KIAS
Maximum Glide Ratio ~ 10.9 : 1
Conditions Example:
Power OFF Altitude 7,000 ft. AGL
Propeller Windmilling Airspeed Best Glide
Flaps 0% (UP)
Wind Zero Glide Distance 12.5 NM
14000
12000
10000
8000
6000
2000
4000
0
0 2 4 6 8 10 12 14 16 18 20
GROUND DISTANCE - NAUTICAL MILES
HEIGHT ABOVE GROUND - FEET
SR20_FM03_1046
Figure 3-1
Maximum Glide
March 2010
Information Manual 3-11
Cirrus Design Section 3
　
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