I am pretty new to the Herc, But not aviation, and navigating through manuals.
A question has come up about resealing at the firewall (to do with turbine overheat system) with a sealant I connot find the spec on and a reference to a Lockheed process bulletin G-550 I am not able to find. Is there some one out there that know where to find out about this process?
Cheers,