Mooney M20F Weight and Balance Calculator
This calculator represents the M20F 2740 lb maximum-weight configuration; approved 2900 lb configurations are not represented. Enter the current basic empty weight and arm from the certified weight and balance record for the individual aircraft.
Maximum takeoff weight: 2,740 lbs. Usable fuel represented: 64 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 M20F (2740 lb configuration) specifications
| Specification | Value |
|---|---|
| Maximum takeoff weight | 2,740 lbs |
| Maximum landing weight | 2,740 lbs |
| Forward CG at 2,250 lbs or less | 41 in |
| Forward CG at 2,470 lbs | 41.8 in |
| Forward CG at 2,740 lbs | 45 in |
| Aft CG limit | 50.1 in |
| Usable fuel | 64 US gal |
| Fuel arm | 48.4 in |
Source: FAA Type Certificate Data Sheet 2A3.
Mooney M20F (2740 lb configuration) CG limits
| Aircraft weight | Forward CG limit | Aft CG limit |
|---|---|---|
| 2,250 lbs | 41 in | 50.1 in |
| 2,470 lbs | 41.8 in | 50.1 in |
| 2,740 lbs | 45 in | 50.1 in |
The calculator uses the published CG envelope points and linear interpolation between forward-limit breakpoints where applicable.
Mooney M20F (2740 lb configuration) loading stations
| Station | Arm | Limit |
|---|---|---|
| Front seats | 31.5 to 39 | |
| Rear seats | 70.7 to 75.2 | |
| Baggage | 95.5 in | 120 lbs |
| Aft baggage / hat rack | 119 in | 10 lbs |
Mooney M20F (2740 lb configuration) fuel capacity
This calculator uses 64 US gallons of usable fuel at an arm of 48.4 inches.
Mooney M20F (2740 lb 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 M20F (2740 lb configuration) configuration
This page represents the normal-category Mooney M20F (2740 lb configuration) configuration identified in FAA Type Certificate Data Sheet 2A3. The calculator uses a maximum takeoff weight of 2,740 lb and 64 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.
Related aircraft
Mooney M20C (S/N 2623 and up fuel configuration), Mooney M20G, Mooney M20E
Mooney M20F (2740 lb configuration) FAQ
What maximum takeoff weight does this Mooney M20F (2740 lb configuration) calculator use?
This calculator uses a maximum takeoff weight of 2,740 lb for the configuration identified on this page.
How much usable fuel is represented for the Mooney M20F (2740 lb configuration)?
This page uses up to 64 US gal of usable fuel at an arm of 48.4 in.
What baggage limit is represented for the Mooney M20F (2740 lb 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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