YimKing
Aerospace
- Mar 31, 2004
- 1
I have an electrical part used in the aircraft (all weather and atmospheric condition). The part consists of (1) anodized Al 6061-T6 (2) anodized Al 2024-T3 (3) Cad plated CR steel. The anodizing is per MIL-A-8625 Type II. All the surfaces described above will be in contact with electroless nickel plated Copper (used as a ground strap). Will there be long term corrosion problem at each interface?