Internal Corrosion Protection


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I will probably have more hours into my RV-9A than many other builders because of the multi-step corrosion prevention treatments that I have decided to use. Many builders will claim that I have gone overboard and they may be correct. However, I am going through this effort for five reasons:
  1. Peace of mind.
  2. PPG recommends etching and applying a chromate conversion coating (Alodine or Iridite) for maximum primer adhesion and corrosion resistance. (See note about PPG's FaxBack service below for a copy of their tech bulletin on metal treatments.)
  3. A MIL-P-23377F Type I Class 1 primer must pass a 1000 hour salt spray test with no adhesion loss, blisters or corrosion WITHOUT A TOPCOAT! (This requires proper surface preparation before priming including either Alodine, Iridite or anodizing.)
  4. A local RV-6QB builder and EAA Flight Advisor gave me his extra copy of AC 43-4A "Corrosion Control for Aircraft". The glossy, color photographs of corrosion problems found on internal aircraft structures is enough to scare anyone into taking extra precautions to prevent corrosion.
  5. Peace of mind.

I try to have all parts completely ready to assemble before beginning the preparation for priming. This means all holes match-drilled, holes and edges deburred, and holes dimpled or countersunk as required.


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Updated 7/6/00