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