Envelope chart. Takeoff 1073 kg at 2.441 m.
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PEOPLE
BAGGAGE
FUEL
EMPTY MASS · F-HSTR
F-HSTR · empty 925.5 kg, arm 2.44 m · weighed 2017-04-25. From Avialpes load sheet.
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Data source
Avialpes load sheet F-HSTR; DA40 NG AFM Section 6; club load sheet F-HSTR · version avialpes-2026.07.2
- From Avialpes' load sheet for F-HSTR (Feuille de centrage Avialpes 07-2026.xlsx), weighing of 25 April 2017. Verify against the tail's current weighing report.
- Forward limit 2.40 m up to 1080 kg, straight line to 2.468 m at 1310 kg; aft limit 2.53 m.
- Maximum landing mass 1280 kg is not on the club sheet; it is the AFM's.
The Diamond DA40 NG from its POH, for any tail: Diamond DA40 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 | 926 | 2.440 | 2258.22 | |
| Pilot | 80 | 2.300 | 184.00 | |
| Front passenger | 0 | 2.300 | 0.00 | |
| Rear passengers | 0 | 3.250 | 0.00 | |
| Baggage | 0 | 3.650 | 0.00 | |
| Fuel | 80 L | 67 | 2.630 | 176.74 |
| Zero fuel | 1006 | 2.429 | 2442.22 | |
| Takeoff | 1073 | 2.441 | 2618.96 |
Avialpes load sheet F-HSTR; DA40 NG AFM Section 6; club load sheet F-HSTR. For reference only; the aircraft’s flight manual and weighing report are the final authority. https://zulucheck.com/wb/f-hstr/
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