AD 2017-07-03

final rule
Data completeness: 70%

Airworthiness Directives; Airbus Airplanes

AD Number
2017-07-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2017-0245
FR Citation
82 FR 17749

Applicability

TypeManufacturerModelDetails
aircraft Airbus A330-243 Airworthiness Directives; Airbus Airplanes

Unsafe Condition

Cracks can develop on the ripple damper of the hydraulic pressure tube assembly, which could lead to hydraulic leakage and consequent loss of the green hydraulic system. Reports of failure of the ripple damper also prompted this AD.

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

Required Actions

Inspect to determine the part number of the hydraulic pressure tube assembly installed on each engine. Replace affected parts with serviceable parts within specified compliance times, as detailed in the AD. Perform repetitive replacements of serviceable parts before they exceed 800 total flight cycles since first installation.

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

Compliance Time

Within 15 days after April 17, 2017, inspect to determine part numbers. Replace affected parts within 25 flight cycles after April 17, 2017, or before exceeding 800 total flight cycles, depending on flight cycle accumulation.

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

Affected Aircraft

Airbus Model A330-243, -243F, -341, -342, and -343 airplanes, all manufacturer serial numbers, 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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