AD 2000-08-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Raytheon | BAe 125-800A and BAe 125-800B | Airworthiness Directives; Raytheon Model BAe 125-800A and BAe 125-800B, Model Hawker 800, and Model Hawker 800XP Series Airplanes |
Unsafe Condition
The presence of unused (open) tooling holes on the firewalls of the left and right engine pylons could allow an engine fire to move to the fuselage and to the lines that carry flammable fluid located inboard of the firewall.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Fill the two unused tooling holes in the firewalls of the left and right engine pylons, as required by AD 96-24-16, within 6 months after January 27, 1997. Additionally, fill all unused tooling holes in the left and right engine pylon firewalls with firewall sealant, in accordance with Raytheon Service Bulletin SB.54-1-3815B, Revision 1, dated May 1998, within 6 months after the effective date of this AD.
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Compliance Time
Within 6 months after the effective date of this AD (May 31, 2000) for new requirements; within 6 months after January 27, 1997, for requirements of AD 96-24-16.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Raytheon Model BAe 125-800A and BAe 125-800B, Model Hawker 800, and Model Hawker 800XP series airplanes, as listed in Raytheon Service Bulletin SB.54-1-3815B, Revision 1, dated May 1998, certificated in any category.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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