Cessna T206 Turbo Stationair weight and balance & performance calculator

Cessna T206 Turbo Stationair key figures by model

¹ Typical empty mass from the POH sample loading; your aircraft's current weighing report applies. Useful load = MTOW − empty mass − usable fuel (people, baggage, oil if not included).

Cessna T206 Turbo Stationair takeoff and landing distance

BriefingPal result at MTOW, sea level, 15 °C, no wind, dry paved runway, normal takeoff and landing per POH with the app's default flap setting, without safety factor:

Hot and high: at 5,000 ft and 25 °C (density altitude about 7,300 ft) the T206H Turbo Stationair (G1000) needs about 760 m (2,500 ft) to clear 50 ft – 43 % more than at sea level. Calculate density altitude →

In BriefingPal you enter your actual weight, airfield, temperature and wind. The app reads the POH charts for these conditions, compares the result with TORA/LDA of the selected runway and can add a 1.15 safety factor.

Cessna T206 Turbo Stationair climb and cruise performance

MTOW, ISA, default power setting of the POH cruise table (≈70 % power for T206H Turbo Stationair (G1000)). Values change with weight, temperature and the power you choose in the app.

Cessna T206 Turbo Stationair weight and balance in BriefingPal

Loading stations: seat row 1, seat row 2, seat row 3, baggage area 1, baggage area 2, baggage area 3, baggage area 4, baggage area 5, baggage area 6, combined baggage limit, fuel. Maximum baggage: 82 kg (180 lb). Demonstrated crosswind: 20 kt. Best rate of climb speed Vy: 89 KIAS. Service ceiling: 27,000 ft. Fuel: AVGAS.

Crosswind calculator with the demonstrated crosswind of the Cessna T206 Turbo Stationair →

How to calculate Cessna T206 Turbo Stationair weight and balance

1. Choose the Cessna T206 Turbo StationairType the registration or pick Cessna → Cessna T206 Turbo Stationair → your model. Stored weighing data of the registration are used automatically.
2. Enter people, baggage and fuelWeights in kg or lb, fuel in US gallons or litres. MTOW and every station limit are checked instantly.
3. Check the CG envelopeTakeoff, zero-fuel and landing points are drawn into the Cessna T206 Turbo Stationair envelope from the POH.
4. Add airfields and routeTakeoff and landing distances, climb, cruise and fuel follow from the same weight – then print the briefing PDF.

Data source

All figures come from the manufacturer's Pilot's Operating Handbook / Airplane Flight Manual of each model (weight and balance section and performance section) and are computed with the BriefingPal engine. BriefingPal is a planning aid; the original POH/AFM of your aircraft and its weighing report remain authoritative.