Here’s a detailed rundown of the Cirrus SR22, with a focus on VX/VY and flap speeds, plus range, useful load, and other key flying considerations:
Core Characteristics & Variants
- The Cirrus SR22 is a four- or five-seat, single-engine, composite aircraft, in continuous production since 2001. It's famous for its Cirrus Airframe Parachute System (CAPS)—earning it the nickname "the plane with the parachute" en.wikipedia.org.
- Several generations exist:
- G2 (circa 2004),
- G3 (airframe/wing updates, higher fuel capacity),
- G5 (2013, higher gross weight up to 3,600 lb and improved CAPS, plus increased flap speeds),
- G6 (2017, cockpit/lighting enhancements),
- G7 (2024, redesigned interior, touch‑screen flight deck),
- G7+ (2025, added Garmin Safe Return autoland) en.wikipedia.org.
V-speeds (G2 Example / Typical SR22)
According to a reliable G2/GTS spec sheet:
- VS0 (stall, landing config): 59 kt.
- VS (clean stall): 70 kt.
- Vx (best angle climb): 88 kt.
- Vy (best rate climb): 101 kt.
- Va (maneuvering speed): 133 kt.
- VNO (normal cruise limit): 178 kt.
- VNE (never exceed): 200 kt johnbellaircraft.com.
Flap Speeds
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G5 and later: Maximum flap extension speeds are:
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First notch: 150 KIAS,
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Second notch: 110 KIAS,
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Full flaps: slightly more extension, but same limit www.aopa.orgen.wikipedia.org.
-
Community‑reported numbers for typical SR22 (G‑series) include:
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Flap‑10°: 91 KIAS,
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Flap‑20°: 85 KIAS,
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Flap‑25° (full): 85 KIAS community.infiniteflight.com. These are conservative guide figures compared to manufacturer cert speeds.
Range & Useful Load
Useful Load
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SR22T G‑series (as per Cirrus site):
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Useful Load: 1,328 lb,
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Payload with 3‑hour fuel + 45‑min reserve: 963 lb cirrusaircraft.com.
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G6 example: Useful load ≈ 1,330 lb, with up to 92 gallons (~553 lb) usable fuel www.flyingmag.com.
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Standard SR22:
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Fuel capacity ~486 lb,
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Payload with full fuel ~464 lb www.globalair.com.
Range
- Typical range (standard model): around 659 nm johnbellaircraft.com.
- SR22T turbo version: maximum range around 1,046–1,100 nm depending on configuration en.wikipedia.org.
- SR22T G‑series (55 % power cruise) (from Cirrus spec):
- Max Range: 1,169 nm (higher spec) cirrusaircraft.com.
Practical User Experience
- From community pilots: If carrying 320 lb front, 200 lb rear, 100 lb baggage (~950 lb usable load), then with lean-of-peak at ~14 gph, you get ~3 h55m endurance → ~522 nm IFR range forum.cirruspilots.org.
- Adding options like TKS, A/C, avionics reduces useful load and thus range forum.cirruspilots.org.
Other Pertinent Flying Info
- Glass cockpit & envelope protection: SR22 was trailblazer in glass cockpits; newer generations include Garmin ESP and advanced flight envelope systems en.wikipedia.org.
- Service ceiling: SR22 models are certified to 17,500 ft; turbocharged variants can reach 25,000 ft en.wikipedia.org.
- CAPS: Ever‑present safety feature, with strong safety record—fatal accident rates dropped significantly as pilots trained to deploy CAPS correctly en.wikipedia.org.
- Payload trade-offs: Options like FIKI system, air conditioning, TKS, autoland systems—great for capability but decrease useful load and range proportionally. For example, adding a lighter 3‑blade prop can increase useful load by about 12 lb cirrusaircraft.com.
Summary
Parameter | Typical Value (G2/GTS) | G5/G6/G7 Notables / Turbo Variants |
---|---|---|
Vx (best angle) | ~88 kt | Similar across models |
Vy (best rate) | ~101 kt | — |
Flap speeds | Flaps 10°: ~91 KIAS | |
Flaps 20–25°: ~85 KIAS | G5+: 1st notch 150 KIAS; 2nd: 110 KIAS johnbellaircraft.comwww.aopa.orgcommunity.infiniteflight.comen.wikipedia.org | |
Useful Load | ~1,050 lb (G2) | |
1,328 lb (G5/GTS) | ~1,330 lb (G6); payload with fuel ~960 lb | |
Range | ~659 nm (NA) | |
1,046–1,100 nm (Turbo) | Up to 1,169 nm at 55% power (Turbo G-series) | |
Service Ceiling | ~17,500 ft | Turbo: up to 25,000 ft |
Unique Features | CAPS, glass cockpit | Autoland (G7+), advanced avionics |
Final Thoughts
- Flap speeds vary slightly by generation—refer to your specific POH, but G5 and later offer higher flap deployment speeds, improving descent control.
- Range and useful load are strongly influenced by configuration choices—options add capability, but trade down weight and fuel.
- Aircraft management: Be mindful of weight balance with passengers, baggage, fuel; lean-of-peak operation extends range.
- Safety features: CAPS remains a cornerstone of safety; modern avionics and autoland add layers of automation and protection.