Summary
This document proposes the supersedure of an existing airworthiness directive (AD), applicable to certain Raytheon Model BAe 125-800A, Model Hawker 800, and Model Hawker 800XP series airplanes, that currently requires the filling of two tooling holes on the firewalls of the left and right engine pylons with firewall sealant. This action would require the sealing of all unused (open) tooling holes on the firewalls of the left and right engine pylons, and would expand the applicability to include additional airplanes. This proposal is prompted by reports of additional unused (open) tooling holes, found at locations other than those currently addressed. The actions specified by the proposed AD are intended to prevent an engine fire from moving to the fuselage and to the lines that carry flammable fluid that are located inboard of the firewall.