N8077X Weight and Balance Calculator
To create a weight and balance table for N8077X, a Cessna 172, I’ll use the information provided in the search results to construct a comprehensive table. Here’s the weight and balance table for N8077X:
| Item | Weight (lbs) | Arm (inches) | Moment (in-lbs) |
|---|---|---|---|
| Empty Weight | 1,500 | 39.0 | 58,500 |
| Pilot + Copilot | 340 | 37.0 | 12,580 |
| Rear Passengers | 350 | 73.0 | 25,550 |
| Fuel (40 gal) | 240 | 48.0 | 11,520 |
| Baggage Area 1 | 80 | 95.0 | 7,600 |
| Baggage Area 2 | 0 | 123.0 | 0 |
| Total | 2,510 | 46.1 | 115,750 |
Additional information for N8077X:
- Maximum Takeoff Weight: 2,550 lbs2
- Acceptable CG Range: 35.0 – 47.3 inches2
- Fuel Weight: 6.01 lbs/gal (US)2
- Useful Load: 1,050 lbs (2,550 – 1,500)
- Maximum Landing Weight: 2,550 lbs2
- Oil Weight: 1.86 lbs/qt (US)2
- Baggage Area 1 + 2 Maximum: 120 lbs4
- Baggage Area 2 Maximum: 50 lbs4
To use this table:
- Verify the actual empty weight and arm for N8077X, as these can vary between individual aircraft.
- Fill in the actual weights for pilot, passengers, fuel, and baggage.
- Calculate the moments by multiplying weight by arm.
- Sum up the weights and moments.
- Calculate the Center of Gravity (CG) by dividing total moment by total weight.
- Ensure the total weight is below the maximum takeoff weight of 2,550 lbs.
- Confirm that the calculated CG falls within the acceptable range of 35.0 – 47.3 inches.
Remember, as the pilot in command, you are responsible for ensuring the accuracy of weight and balance calculations before each flight.