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When selecting hardware for attaching bonding connections to an aircraft structure, which of the following should be considered?
| 1. |
Mechanical strength. |
| 2. |
Allowable power loss. |
| 3. |
Ease of installation. |
| 4. |
Permissible voltage drop. |
| 5. |
Amount of current to be carried. |
| 6. |
Type of load (continuous or intermittent). |
| * | A) 1, 3, 5. |
| | B) 4, 5, 6. |
| | C) 1, 2, 3. |
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