Cirrus SR22T Workbook

SR-Series Workbook ___________________________________________________
Cirrus Aircraft, Duluth, MN
13
17. (T) What is the corrective action if the manifold pressure exceeds
32” (TN) or 37” (T) inches during takeoff?
18. (T) List the procedures for a Rich of Peak (ROP) climb.
19. (T) List the procedures for a Lean of Peak (LOP) climb.
20. (T) (True / False) Leaning the mixture control when operating lean of
peak EGT will cause the CHT’s to increase.
21. (T) What is the corrective action if CHT’s exceed 380° F (TN) or
420° F (T) during a LOP climb?
22. (T) What is the maximum altitude a Lean of Peak (LOP) climb can
be used (TN only)?
23. The climb checklist should be completed no lower than what
altitude? (Flight Operations Manual)
24. (T) List the procedure for setting cruise power.
Throttle _______________________
Mixture _______________________
Boost pump _______________________

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