AD 2003-10-08

final rule
Data completeness: 70%

Airworthiness Directives; McDonnell Douglas Model 717-200 Airplanes

AD Number
2003-10-08
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2001-NM-245-AD
FR Citation
68 FR 28699

Applicability

TypeManufacturerModelDetails
aircraft McDonnell Douglas 717-200 Airworthiness Directives; McDonnell Douglas Model 717-200 Airplanes

Unsafe Condition

Fatigue cracking of the longerons of the upper center fuselage, which could result in reduced structural integrity of the fuselage.

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

Required Actions

Modify the longeron-to-frame installation of the upper center fuselage.

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

Affected Aircraft

McDonnell Douglas Model 717-200 airplanes.

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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