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Cessna P210 Pressurized Centurion weight and balance & performance calculator

The Cessna P210 Pressurized Centurion is a six-seat high-performance single-engine aircraft with retractable gear and piston engine. BriefingPal has 1 model of the Cessna P210 Pressurized Centurion on file – P210N Pressurized Centurion – with data from the Pilot's Operating Handbook for weight and balance, takeoff and landing distances, climb and cruise. Free, no sign-up.

Open the Cessna P210 Pressurized Centurion calculatorfree · no sign-up · POH dataAll Cessna aircraft
1,814 kgMTOW
87 US galUsable fuel
660 mTakeoff over 50 ft*
151 ktCruise TAS*

* P210N Pressurized Centurion, MTOW, sea level / 6,500 ft, ISA – details below

Calculate the Cessna P210 Pressurized Centurion weight, CG and takeoff distance

Loading
Your own empty mass (weighing report, optional)

Leave empty to use the typical POH empty mass. Your aircraft's weighing report is what counts.

Airfield and runway (takeoff and landing)
Full flight planning in BriefingPal →

Calculated on the BriefingPal server from the POH data. Nothing is stored, no cookie. Planning aid only – the POH/AFM and your weighing report are authoritative.

Cessna P210 Pressurized Centurion key figures by model

ModelBuiltMTOWEmpty mass¹Usable fuelMax. baggageUseful load with full fuel¹
P210N Pressurized Centurion19821,814 kg (4,000 lb)1,132 kg (2,496 lb)87 US gal (329 L)91 kg (200 lb)446 kg (982 lb)

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 P210 Pressurized Centurion 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:

ModelTakeoff ground rollTakeoff over 50 ftLanding over 50 ftLanding ground roll
P210N Pressurized Centurion395 m (1,300 ft)660 m (2,170 ft)455 m (1,500 ft)235 m (770 ft)

Hot and high: at 5,000 ft and 25 °C (density altitude about 7,300 ft) the P210N Pressurized Centurion needs about 990 m (3,250 ft) to clear 50 ft – 50 % 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 P210 Pressurized Centurion climb and cruise performance

ModelRate of climb at sea levelTime / fuel to 6,500 ftCruise TAS at 6,500 ftFuel flow
P210N Pressurized Centurion940 fpm7 min / 3.2 US gal151 kt14.6 US gal/h (55 L/h)

MTOW, ISA, default power setting of the POH cruise table. Values change with weight, temperature and the power you choose in the app.

Cessna P210 Pressurized Centurion weight and balance in BriefingPal

Loading stations: seat row 1, seat row 2, seat row 3, baggage area 1, baggage area 2, combined baggage limit, fuel. Maximum baggage: 91 kg (200 lb). Maximum landing mass 1,724 kg (3,800 lb) (P210N Pressurized Centurion) – BriefingPal checks the landing point after trip fuel against it. Demonstrated crosswind: 21 kt. Best rate of climb speed Vy: 100 KIAS. Service ceiling: 23,000 ft. Fuel: AVGAS.

Crosswind calculator with the demonstrated crosswind of the Cessna P210 Pressurized Centurion →

How to calculate Cessna P210 Pressurized Centurion weight and balance

  1. Choose the Cessna P210 Pressurized CenturionType the registration or pick Cessna → Cessna P210 Pressurized Centurion → 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 P210 Pressurized Centurion 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.

Cessna P210 Pressurized Centurion – frequently asked questions

What is the maximum takeoff weight (MTOW) of the Cessna P210 Pressurized Centurion?

P210N Pressurized Centurion: 1,814 kg (4,000 lb).

How much usable fuel does the Cessna P210 Pressurized Centurion carry?

P210N Pressurized Centurion: 87 US gal (329 L).

What is the useful load of the Cessna P210 Pressurized Centurion with full fuel?

With the typical POH empty mass and full usable fuel: P210N Pressurized Centurion: 446 kg (982 lb). Your aircraft's real empty mass is in its weighing report – BriefingPal can store it per registration.

How long is the Cessna P210 Pressurized Centurion takeoff distance?

P210N Pressurized Centurion at MTOW, sea level, 15 °C, no wind: ground roll about 395 m (1,300 ft), over 50 ft about 660 m (2,170 ft). At 5,000 ft and 25 °C it grows to about 990 m (3,250 ft). Always check the POH for your exact conditions.

Is there a free Cessna P210 Pressurized Centurion weight and balance calculator?

Yes. BriefingPal is free and needs no account. It covers 1 model of the Cessna P210 Pressurized Centurion, draws the CG envelope from the POH and also computes takeoff and landing distances, climb, cruise and fuel – with a 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.

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Open the Cessna P210 Pressurized Centurion calculator

free · no sign-up · POH data

Open the Cessna P210 Pressurized Centurion calculatorfree · no sign-up · POH data