Cirrus SR22T User Manual

Cirrus Design Section 3
SR22T Emergency Procedures
P/N 13772-005 3-17P/N 13772-005 3-17
Emergency Descent
Emergency Descent
1. Power Lever ............................................................................ IDLE
2. Mixture ................................................................... AS REQUIRED
3. Airspeed................................................................. V
NE
(205 KIAS)
Amplification
• Caution •
If significant turbulence is expected do not descend at
indicated airspeeds greater than V
NO
(176 KIAS)
Maximum Glide
Best Glide Speed
92 KIAS at 3600 lb
Maximum Glide Ratio ~ 8.6 : 1
Conditions Example:
Power OFF Altitude 10,000 ft. AGL
Propeller Windmilling Airspeed Best Glide
Flaps 0% (UP) Glide Distance 14.2 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
SR22_FM03_3564
Original Issue

Cirrus SR22T Specifications

General

Manufacturer	Cirrus Aircraft
Engine	Continental TSIO-550-K
Horsepower	315 hp
Max Takeoff Weight	3, 600 lbs
Service Ceiling	25, 000 ft
Cabin Width	49 in
Cabin Height	50 in
Seating Capacity	4
Avionics	Cirrus Perspective+ by Garmin
Category	Single-engine piston aircraft
Propeller	Hartzell 3-blade composite
Wingspan	38 ft 4 in
Length	26 ft
Height	8 ft 11 in
Maximum Cruise Speed	213 KTAS
Fuel Capacity	92 gallons
Stall Speed	64 knots
Safety Features	Cirrus Airframe Parachute System (CAPS)
Cruise Speed	183 knots