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Cirrus SR22T

V-speeds, cruise performance, fuel, and weights, digitized from the POH for planning and study.

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Cirrus SR22T preflight numbers at a glance: max gross weight 3600 lb, typical useful load 1100 lb, 92 gal usable fuel, cruise up to about 213 KTAS (POH figure at 25,000 ft, standard day). All figures below come from the FlightDecide curated aircraft library, digitized from the published POH/AFM. Use them for planning and study, and confirm against the POH for your specific serial number before flight.

Cirrus SR22T key numbers

EngineContinental TSIO-550-K (315 HP)
PropellerHartzell PHC-J3YF-1RF/F7693B
Max gross weight3600 lb
Empty weight (typical)2500 lb
Useful load (typical)1100 lb
Usable fuel92 gal

Cirrus SR22T V-speeds

Knots indicated (KIAS) unless the POH states otherwise. Speeds vary by model year and serial; the placarded speeds and your POH govern.

SpeedValueMeaning
VS064 ktStall, landing configuration
VS174 ktStall, clean configuration
VX88 ktBest angle of climb
VY103 ktBest rate of climb
VA140 ktDesign maneuvering speed (at max gross)
VFE110 ktMax flaps extended
VNO176 ktMax structural cruising
VNE205 ktNever exceed
Best glide92 ktBest glide speed
VPD140 kt

Cirrus SR22T cruise performance

Transcribed from the POH cruise tables. True airspeed and fuel flow depend on altitude, power setting, temperature, and leaning technique.

Pressure alt (ft)% powerTAS (kt)Fuel (GPH)
40005514512.7
40007516516.4
40008517418.3
80005515012.7
80007517116.4
80008518018.3
12,0005515512.7
12,0007517816.4
12,0008518718.3
17,5005516112.7
17,5007518716.4
17,5008519718.3
25,0005517112.7
25,0007520116.4
25,0008521318.3

Standard-day (ISA) rows shown, sampled across the POH table for readability; the FlightDecide app carries the full digitized table, including non-standard temperatures.

How much runway does a Cirrus SR22T need?

Book figures at 3600 lb, 0 ft pressure altitude, 15 °C. Real-world technique, wind, surface, and density altitude move these substantially, so apply your own margin (many pilots use 1.5× the book number) and run the numbers for the actual conditions.

POH figureDistance
Takeoff ground roll1130 ft
Takeoff over a 50 ft obstacle1605 ft
Landing ground roll520 ft
Landing over a 50 ft obstacle885 ft
Rate of climb1270 fpm

See how density altitude stretches these distances on a hot day.

Common Questions

Per the POH cruise table, up to about 213 KTAS at 25,000 ft on a standard day, burning roughly 18.3 GPH at that setting. Typical everyday cruise settings run slower and leaner; see the table above.

92 gallons usable. At a high-cruise burn of 18.3 GPH that is roughly 5.0 hours to dry tanks. Plan with reserves, never to zero.

About 1100 lb for a typically equipped example (3600 lb max gross minus a typical empty weight of 2500 lb). Your aircraft's actual empty weight and CG come from its own weight-and-balance records. Always use those, not type averages.

VNE (never exceed) is 205 kt and VNO (max structural cruising) is 176 kt. Full V-speed table above; verify against the POH for your serial.

Plan a flight in this aircraft

Crosswind Calculator

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Density Altitude Calculator

See what heat and elevation do to these takeoff and climb numbers.

The Go/No-Go Decision Framework

Fold these numbers into a structured preflight decision.

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Reference data for planning and study: approximate, and not a substitute for the FAA-approved AFM/POH for your specific aircraft, an official weather briefing, or your judgment as pilot in command (14 CFR 91.3). Source: Cirrus SR22T Pilot's Operating Handbook, Cirrus Aircraft Data synced from the FlightDecide aircraft library on 2026-07-17.