Cirrus SR22T User Manual

P/N 13772-151 19 of 52
Cirrus Design Section 9
SR22T Supplements
which may not be adequate to wet-out the entire panel if the
Pre-Flight Inspection is performed at warmer temperatures.
Increasing the system flow rate (MAX vs. HIGH or HIGH w/
PUMP BKUP vs. HIGH) will increase the arterial pressure of
the system which promotes the complete wet-out of the
porous panels.
Pre-Flight Inspection
1. Cabin
a. Circuit Breakers................................................................. SET
b. Battery 1 Master Switch ......................................................ON
c. Flaps................................................................................100%
d. Avionics Master Switch........................................................ON
e. Cabin Speaker.....................................................................ON
f. Cabin Doors ................................................................. CLOSE
g. WIND SHLD Push-Button ............................................PRESS
(1) Verify evidence of deicing fluid from spray nozzles.
h. PUMP BKUP Switch............................................................ON
(1) Metering Pump Duty Cycle ...........Verify Continuously ON
(2) Deicing Fluid and Endurance Indications.............. CHECK
i. PUMP BKUP Switch..........................................................OFF
j. ICE PROTECT System Switch............................................ON
k. ICE PROTECT Mode Switch......................................... NORM
(1) Metering Pump Duty Cycle ..........Verify 30s ON, 90s OFF
(2) Deicing Fluid and Endurance Indications.............. CHECK
l. ICE PROTECT Mode Switch........................................... HIGH
(1) Metering Pump Duty Cycle ...........Verify Continuously ON
(2) Deicing Fluid and Endurance Indications.............. CHECK
m. ICE Inspection Lights Switch...............................................ON
(1) Verify LH and RH Operation.
Continued on following page.
Original Issue: 02-01-13

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