am looking for a document which would give an overview of this subject. We have E & F Safety Circuit/interlocks, some appear to have a Converter Loop ( ie Converter generates the 28 VDC) while others rely on the 28 VDC being generated at the Aircraft.
Now with the Split "F" there is a new approach.
Is there any consensus in the Aviation Industry as to which Interlock approach is better?
Now with the Split "F" there is a new approach.
Is there any consensus in the Aviation Industry as to which Interlock approach is better?
