Landing light fault annunciator

Communications: electrical – Condition responsive indicating system – Specific condition

Reexamination Certificate

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Details

C340S642000, C340S643000, C340S945000

Reexamination Certificate

active

11049957

ABSTRACT:
A helicopter of the type having an electrical system, a landing light, a master switch and a power supply of between about 18-32 V for operating the electrical system when the master switch is in an on position also includes a landing light fault detector. The landing light fault detector includes a light switch for turning the landing lights on and off and circuit means for detecting a fault in the landing light and for providing a signal indicative of a fault whether or not the light switch is in an on or off position.

REFERENCES:
patent: 3671955 (1972-06-01), Malekzadeh
patent: 4195802 (1980-04-01), Gilson et al.
patent: 5173685 (1992-12-01), Nimmo

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