AD 2006-11-11

Recurring final rule
Data completeness: 90%

Airworthiness Directives; Boeing Model 757 Airplanes

AD Number
2006-11-11
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2005-23213
FR Citation
71 FR 30278

Applicability

TypeManufacturerModelDetails
aircraft Boeing 757 Airworthiness Directives; Boeing Model 757 Airplanes

Unsafe Condition

Fatigue cracking of principal structural elements (PSEs) could adversely affect the structural integrity of these airplanes.

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

Required Actions

Incorporate a new revision to the Airworthiness Limitations section of the Instructions of Continued Airworthiness to mandate certain repetitive inspections for fatigue cracking of PSEs.

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

Compliance Time

Within 12 months of effective date

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

Affected Aircraft

Boeing Model 757 series airplanes, including Model 757-200CB series airplanes.

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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