AD 2003-17-01

final rule
Data completeness: 70%

Airworthiness Directives; McDonnell Douglas Model 717-200 Airplanes

AD Number
2003-17-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2001-NM-325-AD
FR Citation
68 FR 49686

Applicability

TypeManufacturerModelDetails
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.

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

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.

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

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 6, 2026

Rights: U.S. Government Public Domain

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