AD 2006-18-09
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | BAE | Systems (Operations) Limited Model ATP | Airworthiness Directives; BAE Systems (Operations) Limited Model ATP Airplanes |
Unsafe Condition
Fatigue cracking of certain structural elements, which could result in reduced structural integrity of the airplane and consequent rapid decompression of the airplane.
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Required Actions
Revise the Airworthiness Limitations Section (ALS) of the Instructions for Continued Airworthiness (ICA) to include new and revised inspections of the fuselage as specified in the service bulletin ATP-51-002.
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Compliance Time
Before further flight
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Affected Aircraft
BAE Systems (Operations) Limited Model ATP airplanes.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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