Cirrus DESIGN SR22T - Original Issue; Emergency Descent; Maximum Glide

Cirrus Design Section 3
SR22T Emergency Procedures
P/N 13772-003 3-15
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 ~ 8.1 : 1
Conditions Example:
Power OFF Altitude 10,000 ft. AGL
Propeller Windmilling Airspeed Best Glide
Flaps 0% (UP)
Wind Zero Glide Distance 13.3 NM
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
SR22_FM03_3276
Original Issue