Envelope chart. Takeoff 1633 kg at 2.411 m.
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PEOPLE
BAGGAGE
FUEL
EMPTY MASS · F-HSML
F-HSML · empty 1463.5 kg, arm 2.4031 m · weighed 2018-02-14. From Avialpes load sheet.
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Data source
Avialpes load sheet F-HSML; DA42 NG AFM Section 6; club load sheet F-HSML · version avialpes-2026.07.2
- From Avialpes' load sheet for F-HSML (Feuille de centrage Avialpes 07-2026.xlsx), weighing of 14 February 2018. Verify against the tail's current weighing report.
- The sheet shows the empty arm as 2.4 m beside a moment of 3516.87 kg·m; the arm here is the moment over the mass (2.4031 m), as the sheet's own sums use it.
- Both limits move with mass. Forward: 2.35 m to 1468 kg, 2.418 m at 1900 kg, 2.434 m at 1999 kg. Aft: 2.454 m at 1450 kg, 2.48 m from 1700 kg.
- The club sheet works the load twice, with and without the de-icing fluid: set the fluid to 0 for the second.
The Diamond DA42 NG from its POH, for any tail: Diamond DA42 NG weight & balance
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 | 1464 | 2.403 | 3516.94 | |
| Pilot | 80 | 2.300 | 184.00 | |
| Front passenger | 0 | 2.300 | 0.00 | |
| Rear passengers | 0 | 3.250 | 0.00 | |
| Nose baggage | 0 | 0.600 | 0.00 | |
| Cabin baggage | 0 | 3.890 | 0.00 | |
| Rear baggage | 0 | 4.540 | 0.00 | |
| De-icing fluid | 0 L | 0 | 1.000 | 0.00 |
| Main tanks | 30 USG | 90 | 2.630 | 235.92 |
| Aux tanks | 0 USG | 0 | 3.200 | 0.00 |
| Zero fuel | 1544 | 2.398 | 3700.94 | |
| Takeoff | 1633 | 2.411 | 3936.86 |
Avialpes load sheet F-HSML; DA42 NG AFM Section 6; club load sheet F-HSML. For reference only; the aircraft’s flight manual and weighing report are the final authority. https://zulucheck.com/wb/f-hsml/
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