AD 2006-25-05

Recurring final rule
Data completeness: 80%

Airworthiness Directives; Boeing Model 777 Airplanes

AD Number
2006-25-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2006-23817
FR Citation
71 FR 70860

Applicability

TypeManufacturerModelDetails
aircraft Boeing 777 Airworthiness Directives; Boeing Model 777 Airplanes

Unsafe Condition

Corrosion or missing corrosion inhibiting compound (CIC) of the fuselage skin under the forward and aft wing-to-body fairings, which could result in rapid decompression of the airplane.

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

Required Actions

Inspect for corrosion or missing CIC of the fuselage skin under the forward and aft wing-to-body fairings for certain airplanes, or the fuselage skin under the forward wing-to-body fairings only for other airplanes; take corrective action if necessary. Optionally, perform a preventive modification of the fairing areas to terminate repetitive inspections.

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

Boeing Model 777 airplanes, as specified in the referenced service bulletin.

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

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

View Official Source ↗ Find More ADs for Boeing 777

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