ingenieroe
Aerospace
- Jul 17, 2025
- 1
I am designing an external doubler for an antenna in an unpressurized section of fuselage. I am struggling to find good resources on the matter. I am using AC43.13 as the main driver at the moment but I need more guidance.
At the moment I have the plate bonded to a single panel using a perimeter of rivets following edge distance, rivet pitch, and plate thickness as described by 43.13
I am considering having the doubler span more than one panel/bay because of grounding plane requirements and the single panel where the antenna could be is asymmetrical. However, from what I have read, this approach can increase the complexity of the design process due to the way the load is distributed. I'd like to know more about this.
What kind of testing/verification is required for a modification of this nature?
Any advice or pointers would be very helpful and appreciated.
At the moment I have the plate bonded to a single panel using a perimeter of rivets following edge distance, rivet pitch, and plate thickness as described by 43.13
I am considering having the doubler span more than one panel/bay because of grounding plane requirements and the single panel where the antenna could be is asymmetrical. However, from what I have read, this approach can increase the complexity of the design process due to the way the load is distributed. I'd like to know more about this.
What kind of testing/verification is required for a modification of this nature?
Any advice or pointers would be very helpful and appreciated.