AD 2012-02-17

Recurring final rule
Data completeness: 70%

Airworthiness Directives; The Boeing Company Airplanes

AD Number
2012-02-17
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2010-0030
FR Citation
77 FR 12170

Applicability

TypeManufacturerModelDetails
aircraft Boeing Company Airworthiness Directives; The Boeing Company Airplanes

Unsafe Condition

Cracking in the front spar lower chord at the fastener locations common to the side link support fitting at wing station (WS) 292, which could grow and result in structural failure of the spar.

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

Required Actions

Conduct repetitive inspections for corrosion and cracking in the front spar lower chord at the specified fastener locations. Take corrective actions if necessary, including repair or replacement as per Boeing Special Attention Service Bulletin 757-57-0065, Revision 1, dated August 1, 2011.

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

Compliance Time

Within 50 flight hours after the effective date of the AD.

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

Affected Aircraft

All Model 757 airplanes manufactured by The Boeing Company.

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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.