SR20
CIRRUS SR-20
CIRRUS SR-20
Aircraft
Name
SR-20
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-20
CIRRUS SR-20 SRV
CIRRUS SRV
SR20
The Cirrus SR20 is an American piston engine, five-seat, composite monoplane built by Cirrus Aircraft of Duluth, Minnesota.
Technical Data
Wing span (metric)
11.68 m
Length (metric)
7.92 m
Height (metric)
2.71 m
Powerplant
1 x Continental IO-360-ES, 200 hp (149 kW).
Engine Model(s)
Continental IV-1430
Indicative Performance Data
Take-Off
V2
n/a
Distance
451 m
MTOW
1361 kg
Initial Climb (to 5000 ft)
IAS
85 kts
ROC
830 ft/min
Initial Climb (to FL150)
IAS
80 kts
ROC
500
Initial Climb (to FL240)
IAS
80 kts
ROC
0 ft/min
MACH Climb
MACH
n/a
ROC
n/a
Cruise
TAS
155 kts
MACH
n/a
Ceiling
175
Range
785 NM
Initial Descent (to FL240)
MACH
n/a
ROD
n/a
Descent (to FL100)
IAS
140 kts
ROD
1000 ft/min
Descent (FL100 & below)
IAS
n/a
MCS
75 kts
ROD
n/a
Approach
Vapp (IAS)
65 kts
Distance
260 m