AD 2015-23-08

Recurring final rule
Data completeness: 70%

Airworthiness Directives; The Boeing Company Airplanes

AD Number
2015-23-08
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2014-0346
FR Citation
80 FR 73949

Applicability

TypeManufacturerModelDetails
aircraft Boeing Company Airworthiness Directives; The Boeing Company Airplanes

Unsafe Condition

Cracks in fuselage frames and a missing strap not installed on a fuselage frame during production can result in severed frames. Multiple adjacent severed frames, or the combination of a severed frame and fuselage skin chemical mill cracks, can lead to uncontrolled decompression of the airplane.

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

Required Actions

Inspect to determine if the strap adjacent to a certain stringer is installed, and repair if missing. Perform repetitive inspections of the frame for cracking or a severed frame web. Conduct related investigative and corrective actions if necessary. Optional actions are provided to terminate certain repetitive inspections.

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

Compliance Time

Within 12 months of the effective date (January 4, 2016)

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Affected Aircraft

The Boeing Company Model 737-100, -200, -200C, -300, -400, and -500 series 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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