fjcobo
Newbie
- Apr 1, 2014
- 2
Hi all,
I’m working in the installation of a external doubler on a pressurized fuselage (for an antenna installation). I have suddenly realized today, in the installation drawing, that the doubler is covering partially four existing rivets (between stringers and skin).
So the result is that, there are four rivets which head is partially hidden by the doubler (about 50%) and not possible to do a fully visual inspection on them.
Does anybody know if this installation is acceptable and it could be enough to include these four rivets in the ultrasounds/Eddy current inspection planned for the doubler fasteners and antenna hole? (this inspection is issued from the damage tolerance analysis).
Or it should be necessary to trim the doubler flange in order to keep clear an visible the rivets heads?
Thanks in advance
I’m working in the installation of a external doubler on a pressurized fuselage (for an antenna installation). I have suddenly realized today, in the installation drawing, that the doubler is covering partially four existing rivets (between stringers and skin).
So the result is that, there are four rivets which head is partially hidden by the doubler (about 50%) and not possible to do a fully visual inspection on them.
Does anybody know if this installation is acceptable and it could be enough to include these four rivets in the ultrasounds/Eddy current inspection planned for the doubler fasteners and antenna hole? (this inspection is issued from the damage tolerance analysis).
Or it should be necessary to trim the doubler flange in order to keep clear an visible the rivets heads?
Thanks in advance