WBcalc > Diamond > Diamond DA40 NG (2822 lb, standard tanks)
This calculator represents the DA40 NG 1280 kg / 2822 lb configuration without MÄM 40-662, standard tanks. Enter the current basic empty weight and arm from the certified weight and balance record for the individual aircraft.
Maximum takeoff weight: 2,822 lbs. Usable fuel represented: 28 US gal. Fuel arm: 103.5 in.
Data source: Diamond DA40 NG AFM, Doc. 6.01.15-E, Revision 4. How WBcalc sources aircraft data
| Specification | Value |
|---|---|
| Maximum takeoff weight | 2,822 lbs |
| Maximum landing weight represented | 2,681 lbs |
| Usable fuel represented | 28 US gal |
| Fuel arm | 103.5 in |
| Fuel density used by calculator | 7.01 lbs/US gal |
| Reference datum | Datum Plane defined by the DA40 NG AFM |
| Weight | Forward CG | Aft CG |
|---|---|---|
| 2,072 lbs or less | 94.5 in | 99.6 in |
| 2,381 lbs | 94.5 in | 99.6 in |
| 2,822 lbs | 96.9 in | 99.6 in |
Where a published limit changes between points, WBcalc uses straight-line interpolation between those points.
| Station | Arm | Limit |
|---|---|---|
| Front seats | 90.6 in | |
| Rear seats | 128 in | |
| Standard baggage compartment | 143.7 in | 66 lbs |
DA40 NG 1280 kg / 2822 lb configuration without MÄM 40-662, standard tanks. Standard tanks provide 28.0 US gal usable Jet fuel. AFM loading density is 7.01 lb/US gal.
Basic empty weight and empty CG are intentionally not prefilled. Use the current values from the individual aircraft's certified weight and balance record.
WBcalc is a planning aid. Verify serial-number applicability, POH/AFM revisions, supplements, STCs and the current aircraft weight and balance record before flight.
This page represents the normal-category Diamond DA40 NG (2822 lb, standard tanks) configuration identified in Diamond DA40 NG AFM, Doc. 6.01.15-E, Revision 4. The calculator uses a maximum takeoff weight of 2,822 lb and 28 US gal of usable fuel.
The reference datum for the loading arms on this page is Datum Plane defined by the DA40 NG AFM.
Need help with the terminology? Read the aircraft weight and balance guide or the CG envelope guide.
Diamond DA40 Diamond Star (2535 lb, standard tanks)
This calculator uses a maximum takeoff weight of 2,822 lb for the configuration identified on this page.
This page uses up to 28 US gal of usable fuel at an arm of 103.5 in.
Standard baggage compartment is limited to 66 lb on this page.
Source: Diamond DA40 NG AFM, Doc. 6.01.15-E, Revision 4. Check the current POH or AFM, aircraft weight and balance record, equipment list and applicable supplements for the individual aircraft.