Automatic notes can be added to calculated variables and automatic date + initials can be added to input variables.

A list of all notes and a list of all locked variables can be exported.

The aerodynamic center can be plotted with the C.G. location.

A module for airfoil aerodynamic characteristics has been added where airfoil aerodynamic data can be entered and saved.

The power and thrust required is now calculated for each climb, cruise and loiter flight segment in the mission profile.

Propeller, engine and nacelle data has been made more specific per engine.

The engine location can now be defined as inside or outside of the fuselage.

The landing gear can now be defined to a specific nacelle/tailboom.

The landing gear X, Y and Z coordinates are flight condition dependent.

The landing gear has been made more specific per gear instead of landing gear class (e.g. main, nose).

The landing gear can be immersed in the propeller slipstream.

Dorsal fins can be added in a v-tail configuration.

A module for wind tunnel drag trendline has been added based on wind tunnel data.

Asymmetric thrust is automatically calculated based on the engine operating condition.

Airplane can now be trimmed with canard, flying wings and for 3-surface configurations.

Expansion of the help system.

60+ Aircraft Examples: Single Engine and Twin Engine Aircraft; Business Jets; Commercial Transport Jets; Military Trainer, Military Fighter, Military Bomber and Military Transport Aircraft; Experimental Aircraft; UAVs; Gliders; Other Aircraft