USACompositeGuy
Aerospace
- Aug 12, 2003
- 35
I am currently working a repair of an elongated fastener hole on the flange of a Duct assembly. The duct material is 0.063" thick 321 Annealed CRES per MIL-S-6721, Comp T1. The repair is to fusion weld the surfaces using AMS 5689 filler. I am unsure if it is possible to not perform a post weld stress relief in this application.
Any thoughts/experience on the topic would be helpful.
Any thoughts/experience on the topic would be helpful.