AD 2023-19-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Aviat | Various | Airworthiness Directives; British Aerospace (Operations) Limited and British Aerospace Regional Aircraft Airplanes |
Unsafe Condition
Corrosion on the rudder tab hinges, fuselage skin beneath the marker beacon antenna external doubler, and fuselage skin beneath the static vent external doubler, which could lead to reduced structural integrity and consequent loss of control.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Revise the Airworthiness Limitations Section (ALS) of the existing Instructions for Continued Airworthiness (ICA) to incorporate new inspections for corrosion on the rudder tab hinges, fuselage skin beneath the marker beacon antenna external doubler, and fuselage skin beneath the static vent external doubler. Depending on inspection results, perform applicable corrective actions.
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Compliance Time
Within 12 months after the effective date of this AD, or at the compliance times specified in BAE Systems CPCP Manual JS/CPCP/01, Revision 9, whichever occurs later.
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Affected Aircraft
British Aerospace Regional Aircraft Jetstream Series 3101 and Jetstream Model 3201 airplanes.
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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