AD 2007-15-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | BAE | Systems (Operations) Limited Model ATP | Airworthiness Directives; BAE Systems (Operations) Limited Model ATP Airplanes |
Unsafe Condition
Failure to adopt the latest revision of Chapter 5 of the AMM could result in fatigue cracking of certain structural elements remaining undetected, which could result in reduced structural integrity of the airplane and consequent rapid decompression of the airplane.
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 Instructions for Continued Airworthiness (ICA) to include new and revised inspections of the fuselage, engine, horizontal stabilizer, and wing bottom surface. Accomplish the new inspections and replacement actions as specified in the revised sections of the AMM.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the compliance times specified in the revised sections of the AMM.
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Affected Aircraft
All 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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