Cirrus DESIGN SR22T User Manual

4-6 P/N 13772-003
Section 4 Cirrus Design
Normal Procedures SR22T
f. Baggage Door ........................................... Closed and Secure
g. Static Button .............................................. Check for Blockage
h. Parachute Cover........................................ Sealed and Secure
3. Empennage
a. Tiedown Rope .............................................................Remove
b. Horizontal and Vertical Stabilizers .............................Condition
• Note •
Verify tape covering the forward and aft inspection holes
located on outboard ends of horizontal stabilizer is installed
and securely attached.
c. Elevator and Tab............................... Condition and Movement
d. Rudder.................................................. Freedom of Movement
e. Rudder Trim Tab ...................................Condition and Security
f. Attachment hinges, bolts and cotter pins...................... Secure
4. Right Fuselage
a. Static Button .............................................. Check for Blockage
b. Wing/Fuselage Fairings ..................................................Check
c. Door Lock ...................................................................... Unlock
5. Right Wing Trailing Edge
a. Flap and Rub Strips (if installed) ..........Condition and Security
b. Aileron and Tab................................. Condition and Movement
c. Aileron Gap Seal .........................................................Security
d. Hinges, actuation arm, bolts, and cotter pins ............... Secure
6. Right Wing Tip
a. Tip...........................................................................Attachment
b. Strobe, Nav Light and Lens ..................Condition and Security
c. Fuel Vent (underside) ......................................... Unobstructed
7. Right Wing Forward and Main Gear
a. Leading Edge and Stall Strips ...................................Condition
b. Fuel Cap ....................................... Check Quantity and Secure
c. Fuel Drains (2 underside) ............................ Drain and Sample
d. Wheel Fairings...................... Security, Accumulation of Debris
Original Issue

Cirrus DESIGN SR22T Specifications

General

Manufacturer	Cirrus Aircraft
Model	SR22T
Seating Capacity	5
Engine	Continental TSIO-550-K
Horsepower	315 hp
Avionics	Cirrus Perspective+ by Garmin
Type	Single-engine piston aircraft
Maximum Speed	213 knots
Cruise Speed	183 knots
Service Ceiling	25, 000 feet
Maximum Takeoff Weight	3, 600 lbs
Wingspan	38 feet 4 inches
Length	26 ft
Height	8 feet 11 inches
Safety Features	Cirrus Airframe Parachute System (CAPS)
Cabin Width	49 inches
Cabin Height	50 inches