AD 2017-18-05

Recurring final rule
Data completeness: 70%

Airworthiness Directives; The Boeing Company Airplanes

AD Number
2017-18-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2017-0559
FR Citation
82 FR 41331

Applicability

TypeManufacturerModelDetails
aircraft Boeing Company Airworthiness Directives; The Boeing Company Airplanes

Unsafe Condition

Cracking in the fuse pin of the wing landing gear beam end fitting, which could lead to a broken fuse pin and subsequent damage to the surrounding structure, including flight control cables and hydraulic systems.

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

Required Actions

Repetitive replacement or inspection of certain fuse pins, and applicable on-condition actions to detect and correct cracking in the fuse pins.

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

The Boeing Company Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SR, and 747SP airplanes, certificated in any category.

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

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