AD 2007-11-13

final rule
Data completeness: 80%

Airworthiness Directives; McDonnell Douglas Model 717-200 Airplanes

AD Number
2007-11-13
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2007-27338
FR Citation
72 FR 29237

Applicability

TypeManufacturerModelDetails
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.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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