AD 2007-11-13
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | McDonnell Douglas | 717-200 | Airworthiness Directives; McDonnell Douglas Model 717-200 Airplanes |
Unsafe Condition
Fatigue cracking of certain principal structural elements (PSEs), which could adversely affect the structural integrity of the airplane.
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Required Actions
Revise the Airworthiness Limitations Section (ALS) of the Instructions for Continued Airworthiness to incorporate reduced initial inspection and repeat inspection intervals for certain PSEs, in accordance with Boeing Report No. MDC-96K9063, Revision 5, dated February 2006.
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Compliance Time
Within 180 days after the effective date of this AD.
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Affected Aircraft
All McDonnell Douglas Model 717-200 airplanes, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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