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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
TABLE II. First article inspection.
Number of
Inspection
Requirement
Test
Number of
allowable
paragraph
paragraph
sample flashers
to be inspected
failures
Group I
Visual and mechanical
examination (external)
and 3.19
All flashers in
1
sample
(13 total 1/ )
Flash characteristics
Voltage drop
Group II
High and low temperature
soak and operation.
3
1
Vibration
Immersion
Group III
Shock
Altitude
Humidity
3
1
Salt fog
Sand and dust
(when specified)
Group IV
Electromagnetic interference
2
0
Transient voltage
Group V
Life
0
4
1/ One additional flasher is included in the sample to allow for the one defective flasher allowed for group I.
7



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