Cirrus SR22T Workbook

SR-Series Workbook ___________________________________________________
Cirrus Aircraft, Duluth, MN
21
7. Airplane and Systems Description
This section will cover Section 7 (Systems) from your Pilots Operating
Handbook. Answers to all questions will be found in the appropriate
section of the POH, unless otherwise noted.
1. What are the three flap settings?
________% ________º
________% ________º
________% ________º
2. (True / False) The horizontal stabilizer is a two piece unit
attached at empennage.
3. (True / False) It is possible to have an asymmetrical flap
deployment in a Cirrus aircraft.
Hint: Look at the flap control diagram.
4. Why are Cirrus aircraft not equipped with gust locks?
5. (True / False) The autopilot also uses the electric roll trim.
6. The landing gear struts are made of what?
7. Below what temperature does the oil bypass the oil cooler?
8. What is the recommended extended flight oil level for the
engine?
9. Where is the alternate air control knob? Does a SR22 TN or
SR22T have an alternate air control knob? Why?
10. What will cause an OIL warning light to illuminate?
11. Describe when oil is metered into and out of the prop hub.

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