Lateral Tip-over Angle

See Graphic

For an aircraft with tricycle gears, the lateral tip-over angle should not be larger than 55 degrees when the aircraft center of gravity is at its most forward position.

For a taildragger aircraft , the lateral tip-over angle should not be larger than 55 degrees when the aircraft center of gravity is at its most aft position.

Note: The calculation uses the current C.G. location for the flight condition. The flight condition C.G. location may be changed in the Flight Condition Dialog Box.