Cirrus SR22T Workbook

SR-Series Workbook ___________________________________________________
Cirrus Aircraft, Duluth, MN
14
25. (T) When should the boost pump be turned off during cruise?
26. (True / False) The fuel BOOST must be used when switching
tanks?
27. (T) CHT’s should be kept above what temperature during descent?
28. (T) List 3 factors that affect CHT cooling during descent?
29. (T) What power setting can be used during descent?
30. The descent checklist should be completed by what point?
(Flight Operations Manual)
31. What distance from the destination airport should you start a
descent from 17,500’ MSL to a traffic pattern of 2,500’ MSL with
a groundspeed of 180 knots when using:
a. 500 fpm descent _______ NM
b. 1000 fpm descent _______ NM
32. (True / False) The mixture should be full rich and boost pump on
before landing.
33. (True / False) Normal landings are not allowed with 0% or 50%
flaps.
34. On a crosswind landing, at what point will you transition from a
wings-level crab angle into a sideslip?
35. Power goes to what setting on a balked landing/go-around?

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