Mooney M20C Weight and Balance Calculator
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
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.
Mooney M20C (S/N 2623 and up fuel configuration) specifications
| Specification | Value |
|---|---|
| Maximum takeoff weight | 2,575 lbs |
| Maximum landing weight | 2,575 lbs |
| Forward CG at 2,100 lbs or less | 42 in |
| Forward CG at 2,575 lbs | 46.5 in |
| Aft CG limit | 49 in |
| Usable fuel | 52 US gal |
| Fuel arm | 48.4 in |
Source: FAA Type Certificate Data Sheet 2A3.
Mooney M20C (S/N 2623 and up fuel configuration) CG limits
| Aircraft weight | Forward CG limit | Aft CG limit |
|---|---|---|
| 2,100 lbs | 42 in | 49 in |
| 2,575 lbs | 46.5 in | 49 in |
The calculator uses the published CG envelope points and linear interpolation between forward-limit breakpoints where applicable.
Mooney M20C (S/N 2623 and up fuel configuration) loading stations
| Station | Arm | Limit |
|---|---|---|
| Front seats | 36.5 to 44 | |
| Rear seats | 70 in | |
| Baggage | 93 in | 120 lbs |
| Aft baggage / hat rack | 114 in | 10 lbs |
Mooney M20C (S/N 2623 and up fuel configuration) fuel capacity
This calculator uses 52 US gallons of usable fuel at an arm of 48.4 inches.
Mooney M20C (S/N 2623 and up fuel configuration) baggage limits
Baggage is limited to 120 lbs and Aft baggage / hat rack is limited to 10 lbs
Normal category limits
The CG envelope on this page is for the normal category.
About this Mooney M20C (S/N 2623 and up fuel configuration) configuration
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.
Related aircraft
Mooney M20G, Mooney M20E, Mooney M20F (2740 lb configuration)
Mooney M20C (S/N 2623 and up fuel configuration) FAQ
What maximum takeoff weight does this Mooney M20C (S/N 2623 and up fuel configuration) calculator use?
This calculator uses a maximum takeoff weight of 2,575 lb for the configuration identified on this page.
How much usable fuel is represented for the Mooney M20C (S/N 2623 and up fuel configuration)?
This page uses up to 52 US gal of usable fuel at an arm of 48.4 in.
What baggage limit is represented for the Mooney M20C (S/N 2623 and up fuel configuration)?
Baggage is limited to 120 lb on this page.
Source and applicability
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.
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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