AD 2017-05-06

final rule
Data completeness: 70%

Airworthiness Directives; The Boeing Company Airplanes

AD Number
2017-05-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2016-7423
FR Citation
82 FR 12410

Applicability

TypeManufacturerModelDetails
aircraft Boeing Company Airworthiness Directives; The Boeing Company Airplanes

Unsafe Condition

The frame-to-floor-beam joints and frames common to shear ties at certain locations of fuselage structure are subject to widespread fatigue damage (WFD).

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

Required Actions

Inspect for cracking of the frame inner chords and webs common to the floor beam joint and at frames common to the shear ties at certain sections on the left and right fuselage sides. Take corrective action 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 the AD, unless already done.

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Affected Aircraft

All The Boeing Company Model 767-200 and -300 series airplanes, certificated in any category. Installation of Supplemental Type Certificate (STC) ST01920SE does not affect applicability.

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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