AD 2006-06-11

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Boeing Model 747-100B SUD, 747-200B, 747-300, 747-400, and 747-400D Series Airplanes

AD Number
2006-06-11
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2005-22383
FR Citation
71 FR 14367

Applicability

TypeManufacturerModelDetails
aircraft Boeing 747-100B SUD Airworthiness Directives; Boeing Model 747-100B SUD, 747-200B, 747-300, 747-400, and 747-400D Series Airplanes

Unsafe Condition

Cracking or discrepancies of the fasteners in the tension ties, shear webs, and frames at body stations 1120 through 1220, 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

Repetitively inspect for cracking or discrepancies of the fasteners in the tension ties, shear webs, and frames at body stations 1120 through 1220. Perform related investigative and corrective actions if necessary.

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

Compliance Time

Within the compliance times specified in Boeing Alert Service Bulletin 747-53A2507, except as provided by paragraphs (f)(1), (f)(2), and (f)(3) of this AD.

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

Affected Aircraft

Boeing Model 747-100B SUD, 747-200B, 747-300, 747-400, and 747-400D series airplanes; and Model 747-200B series airplanes having a stretched upper deck.

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.