AD 2005-18-10

final rule
Data completeness: 70%

Airworthiness Directives; Boeing Model 777-200 and -300 Series Airplanes

AD Number
2005-18-10
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2005-20475
FR Citation
70 FR 54242

Applicability

TypeManufacturerModelDetails
aircraft Boeing 777-200 and -300 Airworthiness Directives; Boeing Model 777-200 and -300 Series Airplanes

Unsafe Condition

Cracking of the aluminum splice plates under the floor panels in the cabin aisle, which could lead to loss of the capability of the cabin floor and seat track structure to support the airplane interior inertia loads under emergency landing conditions.

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

Required Actions

Modify the splice plate assemblies installed under the floor panels at the forward and aft edges of the cabin aisle.

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

Compliance Time

Within 60 months of the effective date.

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

Affected Aircraft

Boeing Model 777-200 and -300 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

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

View Official Source ↗ Find More ADs for Boeing 777-200 and -300

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