SR22
CIRRUS SR-22
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
Manufactured 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 (metric)
11.68 m
Length (metric)
7.92 m
Height (metric)
2.72 m
Powerplant
1 x Continental IO-550-N Six cylinder horizontally opposed aircraft engine, 310 hp (230 kW).
Engine Model(s)
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
