Cirrus SR22T User Manual

4-6 P/N 13772-005
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
(Continued on following page)
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