AD 2006-20-02

final rule
Data completeness: 80%

Airworthiness Directives; Boeing Model 747 Airplanes

AD Number
2006-20-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2006-24865
FR Citation
71 FR 56861

Applicability

TypeManufacturerModelDetails
aircraft Boeing 747 Airworthiness Directives; Boeing Model 747 Airplanes

Unsafe Condition

Cracking discovered in a skin lap joint that was previously inspected using the eddy current method, which could lead to disbonding and subsequent cracking of the skin panels, potentially causing rapid decompression of the airplane.

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

Required Actions

Inspect the bonded skin panels in section 41 of the fuselage for disbonding, corrosion, and cracking at the longitudinal rows of fasteners. Repair any detected issues. Perform new inspections for airplanes that may have Alodine-coated rivets installed.

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

Compliance Time

Within a specified timeframe (not explicitly stated in the provided text).

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Affected Aircraft

Boeing Model 747 airplanes, including those with Alodine-coated rivets installed.

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

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