CIRRUS SR-22

Aircraft
Name: 
SR-22
Manufacturer: 
Body: 
Narrow
Wing: 
Fixed Wing
Position: 
Low wing
Tail: 
Regular tail, low set
WTC
L
APC
A
Type Code: 
L1P
Engine: 
Piston
Engine Count: 
Single
Position: 
Nose mounted
Landing gear: 
Tricycle fixed
Manufacturered as
CIRRUS SR-22

SR22

The Cirrus SR22 is a single-engine, originally four and later five-seat, composite aircraft, built by Cirrus Aircraft starting in 2001. It is a more powerful version of the Cirrus CIRRUS SR-20, with a larger wing, higher fuel capacity, and a has fixed (non-retractable) landing gear.

Technical Data
Wing span: 
11.68 m
Length: 
7.92 m
Height: 
2.72 m
Powerplant: 

1 x Continental IO-550-N Six cylinder horizontally opposed aircraft engine, 310 hp (230 kW).

Engine Model: 
Continental IO-550
Indicative Performance Data
Take-Off
V2: 
n/a
Distance: 
490 m
MTOW: 
1500 kg
Initial Climb (to 5000 ft)
IAS: 
n/a
ROC: 
n/a
Initial Climb (to FL150)
IAS: 
n/a
ROC: 
n/a
Initial Climb (to FL240)
IAS: 
n/a
ROC: 
n/a
MACH Climb
MACH: 
n/a
ROC: 
n/a
Cruise
TAS: 
180 kts
MACH: 
n/a
Ceiling: 
175
Range: 
700 NM
Initial Descent (to FL240)
MACH: 
n/a
ROD: 
n/a
Descent (to FL100)
IAS: 
n/a
ROD: 
n/a
Descent (FL100 & below)
IAS: 
n/a
MCS: 
n/a
ROD: 
n/a
Approach
Vapp (IAS): 
n/a
Distance: 
700 m

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