11. Wings were fitted with split flaps . 12. Crashes this date on landing approach at Edwards AFB, California, when split flap condition occurs. 13. The NG4 is a conventionally laid out split flaps fill the trailing edges inboard of the ailerons. 14. The outer panels carry some Split flaps with an area of run under the trailing edge from aileron to aileron. 15. The wing and fuselage structures were of a conventional metal design, having a single vertical tail with two split flaps . 16. Thirteen Series II variants were built with split flaps and the Series III ( 19-built ) was similar but had detailed improvements. 17. The design was performed by Yves Gardan, a onetime employee of French aeronautical company flaps that replaced the split flaps of the Minicab. 18. The light alloy split flaps at the trailing edge of the wing were also pneumatically operated via a finger lever on the instrument panel. 19. The wing had a rectangular centre section with tapered outer panels, the latter with split flaps on the inboard trailing edges and ailerons outboard. 20. The aircraft was fitted with various devices to increase lift; slotted flaps and slotted ailerons and, on the low wing sponsons, split flaps .
