WBcalc > Diamond > Diamond DA20-A1 / DA20-100 (912 S3, 1653 lb)
This calculator represents the DA20-A1 / DA20-100 with Rotax 912 S3 and 1653 lb maximum permissible weight. Enter the current basic empty weight and arm from the certified weight and balance record for the individual aircraft.
Maximum takeoff weight: 1,653 lbs. Usable fuel represented: 19.5 US gal. Fuel arm: 32.44 in.
Data source: Diamond DA20/100 Flight Manual and TCDS IM.A.223. How WBcalc sources aircraft data
| Specification | Value |
|---|---|
| Maximum takeoff weight | 1,653 lbs |
| Maximum landing weight represented | 1,653 lbs |
| Usable fuel represented | 19.5 US gal |
| Fuel arm | 32.44 in |
| Fuel density used by calculator | 6.01 lbs/US gal |
| Reference datum | Tangent to the leading edge of the wing at the root rib |
| Weight | Forward CG | Aft CG |
|---|---|---|
| 1,000 lbs or less | 9.84 in | 15.35 in |
| 1,653 lbs | 9.84 in | 15.35 in |
Where a published limit changes between points, WBcalc uses straight-line interpolation between those points.
| Station | Arm | Limit |
|---|---|---|
| Pilot and passenger | 5.63 in | |
| Baggage | 32.44 in | 44 lbs |
DA20-A1 / DA20-100 with Rotax 912 S3 and 1653 lb maximum permissible weight. Usable fuel is 19.5 US gal. Maximum baggage is 44 lb.
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 DA20-A1 / DA20-100 (912 S3, 1653 lb) configuration identified in Diamond DA20/100 Flight Manual and TCDS IM.A.223. The calculator uses a maximum takeoff weight of 1,653 lb and 19.5 US gal of usable fuel.
The reference datum for the loading arms on this page is Tangent to the leading edge of the wing at the root rib.
Need help with the terminology? Read the aircraft weight and balance guide or the CG envelope guide.
This calculator uses a maximum takeoff weight of 1,653 lb for the configuration identified on this page.
This page uses up to 19.5 US gal of usable fuel at an arm of 32.4 in.
Baggage is limited to 44 lb on this page.
Source: Diamond DA20/100 Flight Manual and TCDS IM.A.223. Check the current POH or AFM, aircraft weight and balance record, equipment list and applicable supplements for the individual aircraft.