If you wish to contribute or participate in the discussions about articles you are invited to join SKYbrary as a registered user

 Actions

CIRRUS SR-20

From SKYbrary Wiki

SR20
Aircraft
Name SR-20
Manufacturer CIRRUS
Body Narrow
Wing Fixed Wing
Position Low wing
Tail Regular tail, low set
WTC Light
APC A
Type code L1P
Engine Piston
Engine count Single
Position Nose mounted
Landing gear Tricycle fixed
Mass group 1


Manufacturered as:

CIRRUS SR-20
CIRRUS SR-20 SRV
CIRRUS SRV


CIRRUS SR-20

CIRRUS SR-20 CIRRUS SR-20 3D

Description

The Cirrus SR20 is an American piston engine, five-seat, composite monoplane built by Cirrus Aircraft of Duluth, Minnesota.

Technical Data

Wing span 11.68 m38.32 ft
Length 7.92 m25.984 ft
Height 2.71 m8.891 ft
Powerplant 1 x Continental IO-360-ES, 200 hp (149 kW).
Engine model Continental IV-1430

Performance Data

Take-Off Initial Climb
(to 5000 ft)
Initial Climb
(to FL150)
Initial Climb
(to FL240)
MACH Climb Cruise Initial Descent
(to FL240)
Descent
(to FL100)
Descent (FL100
& below)
Approach
V2 (IAS) kts IAS 85 kts IAS 80 kts IAS 80 kts MACH TAS 155 kts MACH IAS 140 kts IAS kts Vapp (IAS) 65 kts
Distance 451 m ROC 830 ft/min ROC 500 ft/min ROC 0 ft/min ROC ft/min MACH ROD ft/min ROD 1000 ft/min MCS 75 kts Distance 260 m
MTOW 13611,361 kg
1.361 tonnes
kg
Ceiling FL175 ROD ft/min APC A
WTC L Range 785785 nm
1,453,820 m
1,453.82 km
4,769,750.66 ft
NM

Accidents & Serious Incidents involving SR20

None on SKYbrary