AD 2017-02-04

final rule
Data completeness: 70%

Airworthiness Directives; The Boeing Company Airplanes

AD Number
2017-02-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2016-7261
FR Citation
82 FR 9489

Applicability

TypeManufacturerModelDetails
aircraft Boeing Company Airworthiness Directives; The Boeing Company Airplanes

Unsafe Condition

Cracking in the aluminum strut side skin and corrosion resistant steel (CRES) outer spring beam support fitting could result in the failure of the outer spring beam support fitting, which could cause separation of a strut and engine from the airplane during flight.

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

Required Actions

Inspect for cracking in the strut side skin using repetitive high frequency eddy current (HFEC) inspections. Perform an open-hole HFEC inspection for cracking. Take applicable related investigative and corrective actions. Install fastener modifications as specified.

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

Compliance Time

Within 500 flight cycles

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Affected Aircraft

The Boeing Company Model 747-200B, 747-300, 747-400, 747-400D, and 747-400F 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

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