Diamond DA20-A1 / DA20-100 Weight and Balance Calculator
This calculator represents the Diamond DA20/100 with Rotax 912 S3 and 1,653 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. Maximum landing weight: 1,653 lbs. Usable fuel represented: 19.5 US gal. Fuel arm: 32.44 in.
Data source: Diamond DA20/100 Flight Manual, Doc. 202-100 / DA202-100, Rotax 912 S3 configuration. 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 DA20/100 (Rotax 912 S3, 1653 lb) specifications
| Specification | Value |
|---|---|
| Maximum takeoff weight | 1,653 lbs |
| Maximum landing weight | 1,653 lbs |
| Forward CG at 1,000 lbs or less | 9.84 in |
| Forward CG at 1,653 lbs | 9.84 in |
| Aft CG limit | 15.35 in |
| Usable fuel | 19.5 US gal |
| Fuel arm | 32.44 in |
Source: Diamond DA20/100 Flight Manual, Doc. 202-100 / DA202-100, Rotax 912 S3 configuration.
Diamond DA20/100 (Rotax 912 S3, 1653 lb) CG limits
| Aircraft weight | Forward CG limit | Aft CG limit |
|---|---|---|
| 1,000 lbs | 9.84 in | 15.35 in |
| 1,653 lbs | 9.84 in | 15.35 in |
The calculator uses the published CG envelope points and linear interpolation between forward-limit breakpoints where applicable.
Diamond DA20/100 (Rotax 912 S3, 1653 lb) loading stations
| Station | Arm | Limit |
|---|---|---|
| Pilot and passenger | 5.63 in | |
| Baggage | 32.44 in | 44 lbs |
Diamond DA20/100 (Rotax 912 S3, 1653 lb) fuel capacity
This calculator uses 19.5 US gallons of usable fuel at an arm of 32.44 inches.
Diamond DA20/100 (Rotax 912 S3, 1653 lb) baggage limits
Baggage is limited to 44 lbs
Normal category limits
The CG envelope on this page is for the normal category.
About this Diamond DA20/100 (Rotax 912 S3, 1653 lb) configuration
This page represents the normal-category Diamond DA20/100 with Rotax 912 S3 covered by the Diamond DA20/100 Flight Manual. The calculator uses a maximum takeoff and landing weight of 1,653 lb and 19.5 US gal of usable fuel.
The represented fuel arm is 32.44 in, and baggage is limited to 44 lb at the same loading arm.
The reference datum is the tangent to the leading edge of the wing at the root rib.
This page should not be treated as a generic calculator for every DA20-A1 certification or configuration. In particular, certification and fuel-system data can differ between DA20 branches and jurisdictions. Verify the AFM applicable to the individual aircraft.
Need help with the terminology? Read the aircraft weight and balance guide or the CG envelope guide.
Related aircraft
Diamond DA20/100 FAQ
What maximum weight does this DA20/100 calculator use?
This configuration uses a maximum takeoff and landing weight of 1,653 lb.
How much usable fuel is represented?
This page represents 19.5 US gal of usable fuel at an arm of 32.44 in.
What baggage limit is represented?
Baggage is limited to 44 lb on this page.
Does this calculator represent every DA20-A1?
No. This calculator is specifically scoped to the DA20/100 Rotax 912 S3 configuration represented by the cited flight manual.
Source and applicability
Source: Diamond DA20/100 Flight Manual, Doc. 202-100 / DA202-100, Rotax 912 S3 configuration. Verify the current approved AFM, aircraft weight and balance record, equipment 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.
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