AD 2006-22-15

Recurring final rule
Data completeness: 80%

Airworthiness Directives; Boeing Model 747 Airplanes

AD Number
2006-22-15
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2006-23921
FR Citation
71 FR 64884

Applicability

TypeManufacturerModelDetails
aircraft Boeing 747 Airworthiness Directives; Boeing Model 747 Airplanes

Unsafe Condition

Fatigue cracks in the top and side panel webs and stiffeners of the nose wheel well (NWW), which could compromise the structural integrity of the NWW and could lead to the rapid decompression of the airplane.

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

Required Actions

Replace the NWW side and top panels with new panels, which terminates the repetitive inspections. Reduce the interval for certain repetitive inspections and remove a certain optional inspection.

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

Compliance Time

Within 57 months of the effective date (December 11, 2006).

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

Affected Aircraft

All Boeing Model 747 series airplanes.

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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