slotted aileron

It had unusually short and broad slotted ailerons which reached behind the trailing edge.

Initially it had slotted ailerons on all span, later shortened.

The slotted ailerons could be drooped together to function as flaps.

The outer flaps acted as slotted ailerons for roll control.

Slotted ailerons were fitted to the outer wing sections.

Slotted ailerons occupy the outer 45% of the trailing edge; there are no flaps.

The slotted ailerons, which filled about half the span, were ply skinned but with an outer fabric covering.

The outer panels carried slotted ailerons and the centre section pneumatically operated split flaps.

There were fabric over ply covered wooden slotted ailerons which occupied all the trailing edge of the outer panels.

Narrow chord slotted ailerons occupied the outer two-thirds of the span and the rest fitted with similar flaps.

Their trailing edges carry slotted ailerons and slotted flaps.

There are full span, fixed slots on the leading edges and wooden, slotted ailerons and flaps.

It uses slotted ailerons.

The canvas-sheathed slotted ailerons are aerodynamically-compensated, differentially displaced 30 upward and 18 downward.

It has a parallel chord, square tipped wing with a full-span combination of slotted ailerons and flaps.

The outer panels were straight tapered, with short span, slotted ailerons that were fabric over ply covered.

Their trailing edges carried slotted flaps inboard; slotted ailerons filled the rest of the span.

The Kometa-Standard had mass-balanced, slotted ailerons and spoilers at 60% chord which opened above and below the wing.

The inner wing sections, fitted with slotted flaps on the trailing edges had constant chord but further out the wings tapered, with slotted ailerons.

The cantilever wing incorporates nearly full-span automatic leading edge slats, wide-chord slotted ailerons, and wide-span Fowler-type trailing edge flaps.

Four section Handley-Page automatic slats were fitted to the entire leading edges out board of the engine nacelles and differential slotted ailerons at the trailing edges.

The aircraft was fitted with various devices to increase lift; slotted flaps and slotted ailerons and, on the low wing sponsons, split flaps.

The wing was built in three separable parts for ease of transport, with a rectangular centre section and slightly straight tapered outer panels with rounded tips, carrying slotted ailerons.

The Lycoming 0-360-A engine of 180 h.p. driving a McCauley v.p. propeller giving it ample power; and slotted ailerons and balanced tail controls providing good handling.

The Handley Page H.P.20 was an experimental monoplane modification of a de Havilland DH.9A, built to study controllable slots and slotted ailerons as high lift devices.