This calculator represents the M20G normal-category configuration represented by FAA TCDS 2A3. Enter the current basic empty weight and arm from the certified weight and balance record for the individual aircraft.
Maximum takeoff weight: 2,525 lbs. Usable fuel represented: 52 US gal. Fuel arm: 48.4 in.
Data source: FAA Type Certificate Data Sheet 2A3. How WBcalc sources aircraft data
| Specification | Value |
|---|---|
| Maximum takeoff weight | 2,525 lbs |
| Maximum landing weight represented | 2,525 lbs |
| Usable fuel represented | 52 US gal |
| Fuel arm | 48.4 in |
| Fuel density used by calculator | 6 lbs/US gal |
| Reference datum | Fuselage station 0.00, 5.00 in aft of centerline of nose gear support bolts |
| Weight | Forward CG | Aft CG |
|---|---|---|
| 2,113 lbs or less | 40.5 in | 50.1 in |
| 2,470 lbs | 41.8 in | 50.1 in |
| 2,525 lbs | 42.5 in | 50.1 in |
Where a published limit changes between points, WBcalc uses straight-line interpolation between those points.
| Station | Arm | Limit |
|---|---|---|
| Front seats | 31.5 to 39 in — enter actual position | |
| Rear seats | 70.7 to 75.2 in — enter actual position | |
| Baggage | 95.5 in | 120 lbs |
| Aft baggage / hat rack | 119 in | 10 lbs |
M20G normal-category configuration represented by FAA TCDS 2A3. Fuel capacity is 52 US gal at +48.4 in.
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 Mooney M20G configuration identified in FAA Type Certificate Data Sheet 2A3. The calculator uses a maximum takeoff weight of 2,525 lb and 52 US gal of usable fuel.
The reference datum for the loading arms on this page is Fuselage station 0.00, 5.00 in aft of centerline of nose gear support bolts.
Need help with the terminology? Read the aircraft weight and balance guide or the CG envelope guide.
Mooney M20C (S/N 2623 and up fuel configuration), Mooney M20E, Mooney M20F (2740 lb configuration)
This calculator uses a maximum takeoff weight of 2,525 lb for the configuration identified on this page.
This page uses up to 52 US gal of usable fuel at an arm of 48.4 in.
Baggage is limited to 120 lb on this page.
Source: FAA Type Certificate Data Sheet 2A3. Check the current POH or AFM, aircraft weight and balance record, equipment list and applicable supplements for the individual aircraft.