AD 2000-26-10
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 could adversely affect the structural integrity of these airplanes.
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Required Actions
Revise the Airworthiness Limitations Section (ALS) of the Instructions for Continued Airworthiness by incorporating Section 05-00-00, dated August 15, 1997, of the British Aerospace ATP Aircraft Maintenance Manual (AMM), dated October 15, 1999, into the ALS. No alternative inspections or inspection intervals may be approved for the structural elements specified in the revised ALS.
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Compliance Time
Within 30 days after the effective date of this AD.
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Affected Aircraft
All BAe Systems (Operations) Limited Model ATP airplanes, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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