AD 2003-17-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | McDonnell Douglas | 717-200 | Airworthiness Directives; McDonnell Douglas Model 717-200 Airplanes |
Unsafe Condition
Fatigue cracking of certain safe-life structure and 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 of the Instructions for Continued Airworthiness in accordance with Boeing Report No. MDC-96K9063, Revision 3, dated August 2002. Ensure compliance with new removal limits for certain components of the flap system and reduced inspection intervals for fatigue cracking of certain PSEs.
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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 6, 2026
Rights: U.S. Government Public Domain
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