3-14 P/N 13772-002
Section 3 Cirrus Design
Emergency Procedures SR22
Emergency Descent
Emergency Descent
1. Power Lever ............................................................................IDLE
2. Mixture ................................................................... AS REQUIRED
3. Airspeed .................................................................V
NE
(200 KIAS)
Amplification
• Caution •
If significant turbulence is expected do not descend at
indicated airspeeds greater than V
NO
(177 KIAS)
Maximum Glide
Best Glide Speed
88 KIAS at 3400 lb
Maximum Glide Ratio ~ 9.6: 1
Conditions Example:
Power OFF Altitude 10,000 ft. AGL
Propeller Windmilling Airspeed Best Glide
Flaps 0% (UP) Glide Distance 15.8 NM
Wind Zero
14000
12000
10000
8000
6000
2000
4000
0
68
10 12 14 16 18
42
20
0
GROUND DISTANCE - NAUTICAL MILES
HEIGHT ABOVE GROUND - FEET
Reissue A
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