Cessna C-172SP - N2407N
Equipment: G1000/WAAS, KAP 140 Dual AXIS TIS
| Year | 2007 | Rate | $169/hr |
| Vr (rotation) | 55 | Vs1 (stall clean) | 48 |
| Vx (best angle of climb) | 62 | Vso (stall dirty) | 40 |
| Vy (best rate of climb) | 74 |
| |
| Va (design maneuvering) | 105 |
| |
| Vfe (max flap extended) | 85 |
| |
| Vno (max structural cruising) | 129 |
| |
| Vne (never exceed) | 163 |
| |
Weight and Balance
Replace sample weights with your actual weights, then click on the "Calculate" button to see the
new takeoff C.G. Important: Pilots should always calculate the Weight and Balance on the ramp prior to
takeoff using the latest data from the POH, and taking into account all circumstances including the
difference between takeoff and landing fuel quantity and weight.