Fowler flap: split flap that slides backward flat, before hinging downward, thereby increasing first chord, then camber.[10] The flap may form part of the upper surface of the wing, like a plain flap, or it may not, like a split flap, but it must slide rearward before lowering. It may provide some slot effect, but this is not a defining feature of the type.[11] Invented by Harlan D. Fowler in 1924, and tested by Fred Weick at NACA in 1932. They were first used on the Martin 146 prototype in 1935, and in production on the 1937 Lockheed Electra,[12] and is still in widespread use on modern aircraft, often with multiple slots.