AD 2015-21-08

Recurring final rule
Data completeness: 70%

Airworthiness Directives; The Boeing Company Airplanes

AD Number
2015-21-08
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2015-4205
FR Citation
80 FR 65921

Applicability

TypeManufacturerModelDetails
aircraft Boeing Company Airworthiness Directives; The Boeing Company Airplanes

Unsafe Condition

Cracking in the inspar upper skin and rear spar upper chord could result in the inability of the structure to carry limit load, or result in a fuel leak.

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

Required Actions

Repetitive eddy current inspections for any cracking in the inspar upper skin, and related investigative and corrective actions if necessary.

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

Compliance Time

Before further flight

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

Affected Aircraft

The Boeing Company Model 737-100, -200, -200C, -300, -400, and -500 series airplanes, excluding Group 1, configuration 1 airplanes that have already undergone the high frequency eddy current open-hole inspection per Boeing Special Attention Service Bulletin 737-57-1318.

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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