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Cirrus SR20


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Cirrus SR20

The new Cirrrus SR20 aircraft are a giant leap in technology and performance, from the 1950's design of the typical Cessna or Piper used in most flying training schools. As well as the obvious state of the art Flight Displays and Digital Electronic Flight Management Systems, these aircraft are designed and built to the latest 21st century safety standards. Whole aircraft parachute systems, 26G impact "walk-away" structure, Airbags etc. Combined, these active and passive systems, make for Safety standards that were unimagined only a few years ago.

Avionics
GPS
Garmin 430 x 2
VHF NAV/COM
Garmin 430 x 2
ADF
nil
ATC SSR
Garmin

 

Cirrus SR20

Specifications
  • Powerplant: Teledyne Continental IO360ES, six-cylinder, horizontally opposed, fuel injected 200 hp
  • Length 26 ft / 7.92 M
  • Height 8 ft 11 in / 2.71 M
  • Cabin Width 49" / 124 cm
  • Cabin Height 50' / 127 cm
  • Seats 4
  • Empty weight, typical 2080 lb / 945 kg
  • Maximum gross weight 3050 LB / 1386 kg
  • Useable fuel 56 US gal / 212 litres
Cirrus SR20
Performance @ ISA
  • Takeoff distance, ground roll 1,446 ft
  • Takeoff distance over 50-ft obstacle 2,064 ft
  • Max demonstrated crosswind component 21 kt
  • Rate of climb, sea level 1,132 fpm
  • Cruise speed @ 77% power 157 ktas @ 8000'
  • Landing distance over 50-ft obstacle 2,040 ft
  • Landing distance, ground roll 1014 ft

Limiting and Recommended Airspeeds
Cirrus SR20
  • Vx (best angle of climb) 81 kias
  • Vy (best rate of climb) 96 kias
  • Vso (stall, in landing configuration) 56 kcas
  • Vne (never exceed) 200 kias
        
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