|
|
SiteMap
|
You are here: home->ama->D01->D.8.0.5.3.A.1
8053
Metal fasteners used with carbon/graphite composite structures
| | A) may be constructed of any of the metals commonly used in aircraft fasteners. |
| | B) must be constructed of high strength aluminum-lithium alloy. |
| | C) must be constructed of material such as titanium or corrosion resistant steel. |
|
|
|
|
