Aquila A211 (AT01-100) weight and balance and performance calculator
Calculate the weight and balance of the Aquila A211 (AT01-100) 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 Aquila A211 (AT01-100) is a model of the Aquila A210/A211; build years not on file.
* MTOW, sea level, 15 °C, no wind – BriefingPal result from the POH data
Calculate the Aquila A211 (AT01-100) 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.
Aquila A211 (AT01-100) key figures
| Maximum takeoff mass (MTOW) | 750 kg (1,653 lb) |
|---|---|
| Typical empty mass (POH sample) | 506 kg (1,116 lb) |
| Usable fuel | 29 US gal (110 L) |
| Total fuel capacity | 31.7 US gal (120 L) |
| Fuel type | AVGAS |
| Useful load with full fuel | 165 kg (363 lb) |
| Maximum baggage | 40 kg (88 lb) |
| Demonstrated crosswind | 15 kt |
| Best rate of climb speed Vy | 65 KIAS |
| Service ceiling | 14,500 ft |
| Built | – |
| Loading stations | front seats, baggage compartment, fuel |
Empty mass and useful load depend on your aircraft – its weighing report applies.
Aquila A211 (AT01-100) 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 | 250 m (810 ft) | 460 m (1,510 ft) | 500 m (1,640 ft) | 210 m (680 ft) |
| 5,000 ft, 25 °C (density altitude ≈ 7,300 ft) | 370 m (1,210 ft) | 685 m (2,250 ft) | – | – |
Hot and high, the Aquila A211 (AT01-100) needs about 49 % more distance to clear 50 ft than at sea level. Calculate density altitude →
Aquila A211 (AT01-100) climb and cruise
| Rate of climb at sea level | Time / fuel to 6,500 ft | Cruise TAS at 6,500 ft | Fuel flow |
|---|---|---|---|
| 700 fpm | 12 min / 1.5 US gal | 113 kt | 5.2 US gal/h (20 L/h) |
MTOW, ISA, default power setting of the POH cruise table.
How to do the Aquila A211 (AT01-100) 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 Aquila A211 (AT01-100). 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.
Aquila A211 (AT01-100) compared with the other Aquila A210/A211 models
| Model | MTOW | Usable fuel | Takeoff over 50 ft* | Cruise TAS* |
|---|---|---|---|---|
| Aquila A210 | 750 kg | 29 US gal | 465 m | 113 kt |
| Aquila A211 (AT01-100) | 750 kg | 29 US gal | 460 m | 113 kt |
| Aquila A211G / A211GX | 750 kg | 29 US gal | 460 m | 113 kt |
* MTOW, sea level, 15 °C / 6,500 ft, ISA – BriefingPal result from the POH data.
Aquila A211 (AT01-100) – frequently asked questions
What is the MTOW of the Aquila A211 (AT01-100)?
The maximum takeoff mass of the Aquila A211 (AT01-100) is 750 kg (1,653 lb) according to the POH.
How much usable fuel does the Aquila A211 (AT01-100) carry?
29 US gal (110 L) usable (total capacity 31.7 US gal (120 L)). With the typical POH empty mass and full fuel, about 165 kg (363 lb) remain for people and baggage.
How long is the takeoff distance of the Aquila A211 (AT01-100)?
At MTOW, sea level, 15 °C and no wind the ground roll is about 250 m (810 ft) and the distance over 50 ft about 460 m (1,510 ft). At 5,000 ft and 25 °C it grows to about 685 m (2,250 ft). The calculator above gives the value for your conditions.
How do I calculate the CG of the Aquila A211 (AT01-100)?
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 Aquila A211 (AT01-100) POH (front seats, baggage compartment, fuel) and checks the CG against the envelope.
How does the Aquila A211 (AT01-100) differ from other Aquila A210/A211 models?
BriefingPal has 3 Aquila A210/A211 models on file. Compared with them the Aquila A211 (AT01-100) has an MTOW of 750 kg (1,653 lb) (range 750–750 kg), 29 US gal (110 L) usable fuel and a takeoff distance over 50 ft of 460 m (1,510 ft) at MTOW.
Is the Aquila A211 (AT01-100) 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 Aquila A211 (AT01-100) (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.
Other Aquila A210/A211 models
Calculators
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