1964 Mooney M20E
Weight & Balance

1964 Mooney M20E

Super 21 · Complex / HP

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Empty WeightARM 47.2"
1,640 lbs
PilotARM 40.2"
lbs
Front PassengerARM 40.2"
lbs
Rear Left PassengerARM 70.7"
lbs
Rear Right PassengerARM 70.7"
lbs
Baggage AreaARM 93"
lbs
Hat RackARM 114"
lbs
Wing Tanks (gal)ARM 48.4"
312 lbs

Trip Calculator

0 NMMax ≈ 739 NM800 NM
Time

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Fuel Used

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Remaining

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Within Limits

Aircraft is within weight and CG envelope

Gross Weight

2,122 lbs

+453 lbs remaining

CG Location

46.82"

Limits: 42.2" – 49.0"

Total Moment

99.3k

in·lbs

% Max Gross

82.4%

Max: 2,575 lbs

CG Envelope

Fwd: 42.0"–46.5"Aft: 49.0"
40.0"42.0"44.0"46.0"48.0"51.0"CG Station (inches aft of datum)1,500 lbs1,700 lbs1,900 lbs2,100 lbs2,300 lbs2,500 lbs2,700 lbsMax GWBEW
EnvelopeTakeoff CG

For reference only. Verify all weight and balance calculations against your aircraft's actual POH and current equipment list before flight. Pilot in command is responsible for ensuring the aircraft is loaded within limits.

FLT Plan

FLT Plan

Educational & Training Use Only

For educational and training purposes only. This application is not approved for operational flight planning and must not be used for actual navigation or flight decisions. Information shown here may be incomplete, delayed, or inaccurate.

Always use current FAA-approved charts, official weather briefings, aircraft documentation, and your instructor's guidance. The pilot in command is responsible for all flight decisions.

By continuing you acknowledge that this tool is for learning and simulation only and agree not to rely on it for real-world flight operations.