AVSIG: Cirrus Design Model Specs wwswsigarch.jpg (7236 bytes)

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AVSIG Discussion Sections >> Cirrus Design

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Mike OverlyAdministrator
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Reged: 04/09/01
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Loc: Columbus, OH
Cirrus Design Model Specs
      #163029 - 07/22/07 09:38 PM

SR20
Single Continental IO-360-ES
Horsepower: 200

Seating including pilot: 4
Useful Load: 912 lb
Cruise @ 75-percent Power: 150 ktas
Cruise Range with Reserve @ 75-percent Power 620 nm
Runway Requirements/Takeoff over 50-ft Obstacle: 2064 ft
Runway Requirements/Landing over 50-ft Obstacle: 2040 ft
Climb Rate: 880 ft/min
Stall Speed w/Flaps: 56 kcas


SR22
Single Continental IO-550-N
Horsepower: 310

Seating including pilot: 4
Useful Load: 1170 lb
Cruise @ Maximum Power: 185 ktas
Cruise Range with Reserve @ 65-percent Power: 1049 nm
Runway Requirements/Takeoff over 50-ft Obstacle: 1594 ft
Runway Requirements/Landing over 50-ft Obstacle: 2344 ft
Climb Rate: 1400 ft/min
Stall Speed w/Flaps: 60 kcas


SR22 Turbo
Single Continental IO-550-N with Tornado Alley Turbo-normalizing System
Horsepower: 310

Seating including pilot: 4
Useful Load: 1070 lb
Cruise @ Maximum Power: 219 ktas
Cruise Range with Reserve @ 75-percent Power: 925 nm
Runway Requirements/Takeoff over 50-ft Obstacle: 1594 ft
Runway Requirements/Landing over 50-ft Obstacle: 2344 ft
Climb Rate: 1400 ft/min
Stall Speed w/Flaps: 60 kcas


Data compiled by www.AVSIG.com.
Data is subject to error and omission and not for flight planning, operation, or navigation.


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