AD 2017-06-07

final rule
Data completeness: 70%

Airworthiness Directives; Airbus Airplanes

AD Number
2017-06-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2016-8851
FR Citation
82 FR 17107

Applicability

TypeManufacturerModelDetails
aircraft Airbus A330-200 Freighter Airworthiness Directives; Airbus Airplanes

Unsafe Condition

Nonconforming aluminum alloy was used to manufacture several structural parts on the inboard flap, which could result in reduced structural integrity of the airplane.

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

Required Actions

Identify potentially affected inboard flap parts, perform a one-time eddy current inspection to determine material composition, and replace parts with serviceable ones if nonconforming material is found.

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

Compliance Time

Within 30 days after performing the eddy current inspection, unless extended with approval from the FAA, EASA, or Airbus's EASA Design Organization Approval (DOA).

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Affected Aircraft

All Airbus Model A330-200 Freighter, -200, and -300 series airplanes; and Airbus Model A340-200, -300, -500, and -600 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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