Cirrus SR22T Workbook

SR-Series Workbook ___________________________________________________
Cirrus Aircraft, Duluth, MN
8
20. The temperature at sea level is 30 degrees Celsius. Assuming
the standard temperature lapse rate of 2 degrees / 1000’, where
do you expect the freezing level to be?
21. In an engine failure situation with the prop windmilling, how can
you gain additional glide distance?
22. What is the only approved and demonstrated method for spin
recovery?
23. If only the airspeed indicator is giving erroneous information,
what kind of malfunction can you expect?
24. What is the corrective action for erroneous airspeed indications?
25. Will the auxiliary fuel pump provide enough fuel to power the
engine in the event of an engine driven fuel pump failure?
26. What 2 conditions will turn the oil annunciator light on?
27. What is the procedure for a propeller overspeed?
28. What is the procedure for a cabin fire in flight?
29. What procedure would you use to try to get ALT 1 back online in
the case of an ALT 1 failure? What would your next step be if
you could not get the alternator back online?

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