Diamond DA40 NG Weight and Balance Calculator

Aircraft reference: Diamond DA40 NG production years, model information and certification

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

Enter the aircraft loading and fuel plan to check takeoff and expected landing conditions. After calculating, you can print or save the completed weight and balance worksheet as a PDF.

Diamond DA40 NG (2822 lb, standard tanks) specifications

Specification	Value
Maximum takeoff weight	2,822 lbs
Maximum landing weight	2,681 lbs
Minimum flight weight	2,072 lbs
Forward CG at 2,072 lbs	94.5 in
Forward CG at 2,381 lbs	94.5 in
Forward CG at 2,822 lbs	96.9 in
Aft CG limit	99.6 in
Usable fuel	28 US gal
Fuel arm	103.5 in

Source: Diamond DA40 NG AFM, Doc. 6.01.15-E, Revision 4.

Diamond DA40 NG (2822 lb, standard tanks) CG limits

Aircraft weight	Forward CG limit	Aft CG limit
2,072 lbs	94.5 in	99.6 in
2,381 lbs	94.5 in	99.6 in
2,822 lbs	96.9 in	99.6 in

The calculator uses the published CG envelope points and linear interpolation between forward-limit breakpoints where applicable.

Diamond DA40 NG (2822 lb, standard tanks) loading stations

Station	Arm	Limit
Front seats	90.6 in
Rear seats	128 in
Standard baggage compartment	143.7 in	66 lbs

Diamond DA40 NG (2822 lb, standard tanks) fuel capacity

This calculator uses 28 US gallons of usable fuel at an arm of 103.5 inches.

Diamond DA40 NG (2822 lb, standard tanks) baggage limits

Standard baggage compartment is limited to 66 lbs

Normal category limits

The CG envelope on this page is for the normal category.

About this Diamond DA40 NG (2822 lb, standard tanks) configuration

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.

Related aircraft

Diamond DA40 Diamond Star (2535 lb, standard tanks)

Diamond DA40 NG (2822 lb, standard tanks) FAQ

What maximum takeoff weight does this Diamond DA40 NG (2822 lb, standard tanks) calculator use?

This calculator uses a maximum takeoff weight of 2,822 lb for the configuration identified on this page.

How much usable fuel is represented for the Diamond DA40 NG (2822 lb, standard tanks)?

This page uses up to 28 US gal of usable fuel at an arm of 103.5 in.

What baggage limit is represented for the Diamond DA40 NG (2822 lb, standard tanks)?

Standard baggage compartment is limited to 66 lb on this page.

Source and applicability

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.

WBcalc is a planning aid. Check the current POH or AFM, aircraft weight and balance record, equipment list and applicable supplements before flight.

Need model context? View the Diamond DA40 NG Aircraft Reference page for production years, family information and certification details.

Weight and balance guides: Weight and balance · Center of gravity · CG envelope · Moment · Basic empty weight · Fuel weight

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