WBcalc > Mooney > Mooney M20C (S/N 2623 and up fuel configuration)
This calculator represents the M20C using the 52 US gal wing-tank configuration applicable to serial number 2623 and up. Enter the current basic empty weight and arm from the certified weight and balance record for the individual aircraft.
Maximum takeoff weight: 2,575 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 | 2,575 lbs |
| Maximum landing weight represented | 2,575 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 at centerline of nose gear support bolts |
| Weight | Forward CG | Aft CG |
|---|---|---|
| 2,100 lbs or less | 42 in | 49 in |
| 2,575 lbs | 46.5 in | 49 in |
Where a published limit changes between points, WBcalc uses straight-line interpolation between those points.
| Station | Arm | Limit |
|---|---|---|
| Front seats | 36.5 to 44 in — enter actual position | |
| Rear seats | 70 in | |
| Baggage | 93 in | 120 lbs |
| Aft baggage / hat rack | 114 in | 10 lbs |
M20C using the 52 US gal wing-tank configuration applicable to serial number 2623 and up. TCDS capacity excludes the separately specified unusable fuel included in certified empty weight.
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 M20C (S/N 2623 and up fuel configuration) configuration identified in FAA Type Certificate Data Sheet 2A3. The calculator uses a maximum takeoff weight of 2,575 lb and 52 US gal of usable fuel.
The reference datum for the loading arms on this page is Fuselage station 0.00 at centerline of nose gear support bolts.
Need help with the terminology? Read the aircraft weight and balance guide or the CG envelope guide.
Mooney M20G, Mooney M20E, Mooney M20F (2740 lb configuration)
This calculator uses a maximum takeoff weight of 2,575 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.