Development of the Highlander with leading edge slats and robust landing gear.

Without hydraulic pressure, the left wing leading edge slats retracted due to the force of the air moving over the wings.

Combat manoeuvrability was improved with the addition of automatic leading edge slats.

This arrangement is known as leading edge slats.

Both wings carried ailerons and the upper planes had leading edge slats.

Automatic leading edge slats were mounted on the outer panels.

The wing had leading edge slats along two-thirds of its length.

The addition of leading edge slats and large compound flaps to the wings has largely resolved the issue.

With the nose up or in a turn, the stalls whipped into spins when the automatic leading edge slats opened.

As 200 T but with leading edge slats.