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Robin DR 401-155CDI weight and balance and performance calculator

Calculate the weight and balance of the Robin DR 401-155CDI 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 Robin DR 401-155CDI is a model of the Robin DR 400; built 2018.

1,100 kgMTOW
28.7 US galUsable fuel
400 mTakeoff over 50 ft*
413 kgUseful load, full fuel

* MTOW, sea level, 15 °C, no wind – BriefingPal result from the POH data

Robin DR 401-155CDI
Photo: Dylan Agbagni, CC0 (Wikimedia Commons)

Calculate the Robin DR 401-155CDI 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)

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.

Robin DR 401-155CDI key figures

Maximum takeoff mass (MTOW)1,100 kg (2,425 lb)
Typical empty mass (POH sample)600 kg (1,323 lb)
Usable fuel28.7 US gal (109 L)
Total fuel capacity29 US gal (110 L)
Fuel typeJet A-1 / diesel
Useful load with full fuel413 kg (910 lb)
Maximum baggage40 kg (88 lb)
Demonstrated crosswind22 kt
Best rate of climb speed Vy78 KIAS
Service ceiling16,500 ft
Built2018
Loading stationsseat row 1, seat row 2, baggage compartment, fuel

Empty mass and useful load depend on your aircraft – its weighing report applies.

Robin DR 401-155CDI 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.

ConditionsTakeoff ground rollTakeoff over 50 ftLanding over 50 ftLanding ground roll
Sea level, 15 °C215 m (700 ft)400 m (1,310 ft)415 m (1,360 ft)175 m (570 ft)
5,000 ft, 25 °C (density altitude ≈ 7,300 ft)330 m (1,080 ft)615 m (2,030 ft)––

Hot and high, the Robin DR 401-155CDI needs about 54 % more distance to clear 50 ft than at sea level. Calculate density altitude →

Robin DR 401-155CDI climb and cruise

Rate of climb at sea levelTime / fuel to 6,500 ftCruise TAS at 6,500 ftFuel flow
740 fpm9 min / 1.4 US gal93 kt4.0 US gal/h (15 L/h)

MTOW, ISA, default power setting of the POH cruise table.

How to do the Robin DR 401-155CDI weight and balance

  1. Enter the loadingWeights of pilot, passengers and baggage per station, fuel in litres or US gallons. Each station limit and the MTOW are checked.
  2. Use your own empty massOptional: enter empty mass and empty CG from the weighing report of your Robin DR 401-155CDI. Without it the typical POH empty mass is used.
  3. 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.
  4. Takeoff and landingElevation, QNH, temperature, wind and runway give the takeoff and landing distance – compared with the runway length if you enter it.

Robin DR 401-155CDI compared with the other Robin DR 400 models

ModelMTOWUsable fuelTakeoff over 50 ft*Cruise TAS*
Robin DR 400 2+2865 kg26.4 US gal510 m103 kt
Robin DR 400/120 Dauphin 2+2900 kg28.8 US gal535 m100 kt
Robin DR 400/140B Major1,000 kg28.7 US gal590 m117 kt
Robin DR 400/160 Chevalier/Major1,050 kg49.9 US gal590 m125 kt
Robin DR 400/180 Régent1,100 kg49.9 US gal515 m127 kt
Robin DR 400/180 R Remorqueur1,000 kg28.8 US gal400 m118 kt
Robin DR 400/160 ed. 11,050 kg49.9 US gal620 m123 kt
Robin DR 400/180 Régent ed. 11,100 kg49.9 US gal610 m129 kt
Robin DR 400/140 Major1,000 kg29.1 US gal550 m121 kt
Robin DR 401-155CDI1,100 kg28.7 US gal400 m93 kt
Robin DR 400/500 Président 200i1,150 kg48.6 US gal465 m130 kt

* MTOW, sea level, 15 °C / 6,500 ft, ISA – BriefingPal result from the POH data.

Robin DR 401-155CDI – frequently asked questions

What is the MTOW of the Robin DR 401-155CDI?

The maximum takeoff mass of the Robin DR 401-155CDI is 1,100 kg (2,425 lb) according to the POH.

How much usable fuel does the Robin DR 401-155CDI carry?

28.7 US gal (109 L) usable (total capacity 29 US gal (110 L)). With the typical POH empty mass and full fuel, about 413 kg (910 lb) remain for people and baggage.

How long is the takeoff distance of the Robin DR 401-155CDI?

At MTOW, sea level, 15 °C and no wind the ground roll is about 215 m (700 ft) and the distance over 50 ft about 400 m (1,310 ft). At 5,000 ft and 25 °C it grows to about 615 m (2,030 ft). The calculator above gives the value for your conditions.

How do I calculate the CG of the Robin DR 401-155CDI?

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 Robin DR 401-155CDI POH (seat row 1, seat row 2, baggage compartment, fuel) and checks the CG against the envelope.

How does the Robin DR 401-155CDI differ from other Robin DR 400 models?

BriefingPal has 11 Robin DR 400 models on file. Compared with them the Robin DR 401-155CDI has an MTOW of 1,100 kg (2,425 lb) (range 865–1,150 kg), 28.7 US gal (109 L) usable fuel and a takeoff distance over 50 ft of 400 m (1,310 ft) at MTOW.

Is the Robin DR 401-155CDI 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 Robin DR 401-155CDI (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 Robin DR 400 models

Calculators

Open the Robin DR 401-155CDI calculator

free · no sign-up · POH data