Robin DR 400/180 weight & balance
POH figures for the type
- MTOW1100 kg
- MLM1045 kg
- Typical empty615 kg
- Typical empty CG0.32 m
Envelope chart. Takeoff 789 kg at 0.350 m.
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PEOPLE
BAGGAGE
FUEL
EMPTY MASS · YOUR AIRCRAFT
Typical for the type, 615 kg at 0.32 m. Edit it to your aircraft’s own, from its weighing report.
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Data source
Manuel de vol DR 400/180 Section 6; club load sheets F-GMXF, F-GEIH, F-GFXS · version type
- Forward limit 0.205 m up to 750 kg, then straight to 0.428 m at 1100 kg; aft limit 0.564 m.
- Maximum landing mass 1045 kg: at full mass, 55 kg of fuel must be used before landing.
- Club sheets use 0.71 kg/L for Avgas; the manual's 0.72 is used here.
For reference only. The aircraft’s approved flight manual and weighing report are the final authority.
| Station | Load | Mass kg | Arm m | Moment kg·m |
|---|---|---|---|---|
| Empty aircraft | 615 | 0.320 | 196.80 | |
| Pilot | 80 | 0.410 | 32.80 | |
| Front passenger | 0 | 0.410 | 0.00 | |
| Rear passengers | 0 | 1.190 | 0.00 | |
| Baggage | 0 | 1.900 | 0.00 | |
| Front tank | 80 L | 58 | 0.100 | 5.76 |
| Centre tank | 50 L | 36 | 1.120 | 40.32 |
| Supplementary tank (if fitted) | 0 L | 0 | 1.610 | 0.00 |
| Zero fuel | 695 | 0.330 | 229.60 | |
| Takeoff | 789 | 0.350 | 275.68 |
Manuel de vol DR 400/180 Section 6; club load sheets F-GMXF, F-GEIH, F-GFXS. For reference only; the aircraft’s flight manual and weighing report are the final authority. https://zulucheck.com/wb/type/robin-dr400-180/
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