What is the primary function of bonding in aircraft electrical systems?

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Multiple Choice

What is the primary function of bonding in aircraft electrical systems?

Explanation:
Bonding is about making all conductive parts that could come into contact or influence each other sit at the same electrical potential. By tying metal surfaces—airframe sections, fuel tanks, panels, and equipment grounds—together with a low-impedance path, any tendency for those parts to develop different voltages is minimized. This prevents arcing or spark hazards between nearby parts, reduces shock risk when a person could touch different pieces at once, and helps keep electrical noise and interference from one component to another. Grounding, on the other hand, provides a reference point and a fault return path for the system, which is a separate function from bonding. Bonding is not about shielding insulation or treating grounding as the same thing, so the primary job of bonding is the low-impedance equalization of potentials across conductive parts.

Bonding is about making all conductive parts that could come into contact or influence each other sit at the same electrical potential. By tying metal surfaces—airframe sections, fuel tanks, panels, and equipment grounds—together with a low-impedance path, any tendency for those parts to develop different voltages is minimized. This prevents arcing or spark hazards between nearby parts, reduces shock risk when a person could touch different pieces at once, and helps keep electrical noise and interference from one component to another.

Grounding, on the other hand, provides a reference point and a fault return path for the system, which is a separate function from bonding. Bonding is not about shielding insulation or treating grounding as the same thing, so the primary job of bonding is the low-impedance equalization of potentials across conductive parts.

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