AD Amdt-39-9840

final rule
Data completeness: 70%

Airworthiness Directives; Raytheon Model BAe 125-800A, Model Hawker 800, and Model Hawker 800XP Series Airplanes

AD Number
Amdt-39-9840
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. 96-NM-136-AD
FR Citation
61 FR 66878

Applicability

TypeManufacturerModelDetails
aircraft Raytheon BAe 125-800A Airworthiness Directives; Raytheon Model BAe 125-800A, Model Hawker 800, and Model Hawker 800XP Series Airplanes

Unsafe Condition

The two tooling holes on the firewalls of the left and right engine pylons were not sealed during production, allowing an engine fire to move to the fuselage and flammable fluid carrying lines located inboard of the firewalls.

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 engine pylon firewalls with sealant per Raytheon Service Bulletin SB.54-1-3815B. Compliance must be completed within six months after the effective date of this AD.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within six months after January 27, 1997

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Raytheon Model BAe 125-800A, Model Hawker 800 (including Special Variants C29A, U125, U125A), and Model Hawker 800XP series airplanes where Service Bulletin SB.54-1-3815B or production equivalent has not been installed.

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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.