Cessna T210N Turbo Centurion weight and balance and performance calculator
Calculate the weight and balance of the Cessna T210N Turbo Centurion online: enter people, baggage and fuel and get the takeoff mass, the CG and whether both are within the limits of the POH – plus the takeoff and landing distance for your airfield, temperature and wind. Free, no sign-up. The Cessna T210N Turbo Centurion is a model of the Cessna T210 Turbo Centurion; built 1982.
* MTOW, sea level, 15 °C, no wind – BriefingPal result from the POH data
Calculate the Cessna T210N Turbo Centurion weight, CG and takeoff distance
Your own empty mass (weighing report, optional)
The POH has no standard empty moment for this model – enter the empty mass CG from your weighing report to get the CG.
Leave empty to use the typical POH empty mass. Your aircraft's weighing report is what counts.
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 T210N Turbo Centurion key figures
| Maximum takeoff mass (MTOW) | 1,814 kg (4,000 lb) |
|---|---|
| Typical empty mass (POH sample) | 1,071 kg (2,362 lb) |
| Usable fuel | 87 US gal (329 L) |
| Total fuel capacity | 90 US gal (341 L) |
| Fuel type | AVGAS |
| Useful load with full fuel | 506 kg (1,116 lb) |
| Maximum baggage | 91 kg (200 lb) |
| Maximum landing mass | 1,724 kg (3,800 lb) |
| Demonstrated crosswind | 21 kt |
| Best rate of climb speed Vy | 100 KIAS |
| Service ceiling | 27,000 ft |
| Built | 1982 |
| Loading stations | seat row 1, seat row 2, seat row 3, baggage area 1, baggage area 2, baggage area 3, combined baggage limit, fuel |
Empty mass and useful load depend on your aircraft – its weighing report applies.
Cessna T210N Turbo Centurion takeoff and landing distance
BriefingPal result from the POH charts at MTOW, no wind, dry paved runway, normal procedure, default flap setting, without safety factor. Use the calculator above for your mass, airfield, temperature and wind.
| Conditions | Takeoff ground roll | Takeoff over 50 ft | Landing over 50 ft | Landing ground roll |
|---|---|---|---|---|
| Sea level, 15 °C | 395 m (1,300 ft) | 660 m (2,170 ft) | 455 m (1,500 ft) | 235 m (770 ft) |
| 5,000 ft, 25 °C (density altitude ≈ 7,300 ft) | 600 m (1,960 ft) | 990 m (3,250 ft) | – | – |
Hot and high, the Cessna T210N Turbo Centurion needs about 50 % more distance to clear 50 ft than at sea level. Calculate density altitude →
Cessna T210N Turbo Centurion climb and cruise
| Rate of climb at sea level | Time / fuel to 6,500 ft | Cruise TAS at 6,500 ft | Fuel flow |
|---|---|---|---|
| 930 fpm | 7 min / 3.1 US gal | 165 kt | 16.5 US gal/h (62 L/h) |
MTOW, ISA, default power setting of the POH cruise table (≈75 % power).
How to do the Cessna T210N Turbo Centurion weight and balance
- Enter the loadingWeights of pilot, passengers and baggage per station, fuel in litres or US gallons. Each station limit and the MTOW are checked.
- Use your own empty massOptional: enter empty mass and empty CG from the weighing report of your Cessna T210N Turbo Centurion. Without it the typical POH empty mass is used.
- Check CG and massThe traffic light shows whether the takeoff mass and the CG with and without fuel lie within the envelope of the POH.
- Takeoff and landingElevation, QNH, temperature, wind and runway give the takeoff and landing distance – compared with the runway length if you enter it.
Cessna T210N Turbo Centurion compared with the other Cessna T210 Turbo Centurion models
| Model | MTOW | Usable fuel | Takeoff over 50 ft* | Cruise TAS* |
|---|---|---|---|---|
| Cessna T210J Turbo Centurion | 1,542 kg | 89 US gal | 425 m | 160 kt |
| Cessna T210N Turbo Centurion | 1,814 kg | 87 US gal | 660 m | 165 kt |
* MTOW, sea level, 15 °C / 6,500 ft, ISA – BriefingPal result from the POH data.
Cessna T210N Turbo Centurion – frequently asked questions
What is the MTOW of the Cessna T210N Turbo Centurion?
The maximum takeoff mass of the Cessna T210N Turbo Centurion is 1,814 kg (4,000 lb) according to the POH.
How much usable fuel does the Cessna T210N Turbo Centurion carry?
87 US gal (329 L) usable (total capacity 90 US gal (341 L)). With the typical POH empty mass and full fuel, about 506 kg (1,116 lb) remain for people and baggage.
How long is the takeoff distance of the Cessna T210N Turbo Centurion?
At MTOW, sea level, 15 °C and no wind the ground roll is about 395 m (1,300 ft) and the distance 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). The calculator above gives the value for your conditions.
How do I calculate the CG of the Cessna T210N Turbo Centurion?
Multiply each mass by its arm, add up the moments and divide by the total mass – the calculator above does this with the stations of the Cessna T210N Turbo Centurion POH (seat row 1, seat row 2, seat row 3, baggage area 1, baggage area 2, baggage area 3, combined baggage limit, fuel) and checks the CG against the envelope.
How does the Cessna T210N Turbo Centurion differ from other Cessna T210 Turbo Centurion models?
BriefingPal has 2 Cessna T210 Turbo Centurion models on file. Compared with them the Cessna T210N Turbo Centurion has the highest MTOW (1,814 kg (4,000 lb)), 87 US gal (329 L) usable fuel and a takeoff distance over 50 ft of 660 m (2,170 ft) at MTOW.
Is the Cessna T210N Turbo Centurion weight and balance calculator free?
Yes. The calculator on this page and the BriefingPal app are free and need no account. The app adds route planning, weather, NOTAM, fuel planning and a briefing PDF.
Data source
All figures come from the Pilot's Operating Handbook / Airplane Flight Manual of the Cessna T210N Turbo Centurion (weight and balance and performance sections) and are computed with the BriefingPal engine – the same calculation as in the app. Planning aid only; the original POH/AFM and the weighing report of your aircraft remain authoritative.
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