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MIL-F-26301 Flasher, Solid State, Aircraft Navigational Light, General Specification ForThis specification covers the general requirements for solid state aircraft flashers which are used for cycling aircraft position lights on and off. Flashers will have the load current controlled by a transistor, controlled rectifier, magnetic amplifier or equivalent device. Flashers have either single or dual output circuits.

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MIL-F-26301G
4.2.1 Sample size. Thirteen flashers shall be selected at random and subjected to first article testing as specified
4.2.2 Inspection routine. Sample flashers shall be subjected to the inspections specified in table II, in the order
shown. All flashers shall be subjected to group I inspection. Upon completion of group I inspection, the sample shall
be subdivided as specified in table II for groups II, III, IV, and V.
4.2.3 Failures. Failures in excess of the number allowed in table II shall be cause for refusal to grant first article
approval.
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