AD 95-15-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | BAe.125 Series 1000A | Airworthiness Directives; Raytheon Model BAe 125-800A and -1000A Airplanes |
| aircraft | Textron Aviation Inc. | BAe.125 Series 800A | Airworthiness Directives; Raytheon Model BAe 125-800A and -1000A Airplanes |
Unsafe Condition
Corrosion of the wing leading edge skins at the interface with the TKS panels and stall vane spoilers could reduce structural integrity, adversely affecting flight characteristics.
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Required Actions
Inspect wing leading edge skins for corrosion, repair if necessary, and apply corrosion protection treatment. Conduct dye penetrant inspections, repair beyond limits, and perform stall warning system flight checks as per service bulletins.
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Compliance Time
Within 24 months since airplane manufacture or within 12 months after the effective date of this AD (August 23, 1995), whichever occurs later. Subsequent actions must be done prior to further flight after each preceding step.
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Affected Aircraft
Raytheon Model BAe 125-800A and -1000A airplanes listed in Service Bulletin S.B. 57-77, Revision 1.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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