AD 2013-25-08

Recurring final rule
Data completeness: 90%

Airworthiness Directives; Airbus Airplanes

AD Number
2013-25-08
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2013-0365
FR Citation
78 FR 78694

Applicability

TypeManufacturerModelDetails
aircraft Airbus A330-200 and -300 Airworthiness Directives; Airbus Airplanes

Unsafe Condition

Loosening of check valves, Part Number (P/N) CAR401, which could result in hydraulic leaks, possibly leading to the loss of all three hydraulic systems and consequent loss of control of the airplane.

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

Required Actions

Inspect check valves P/N CAR401 for lock wire presence and integrity, traces of seepage or black deposits, proper torque, and alignment of the check valve and manifold. Install new lock wire and take corrective actions if needed. Revise the torque values for check valve tightening and implement a repetitive inspection program for certain check valves in the hydraulic systems on airplanes that have had a specific modification during production or in-service.

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

Compliance Time

Within 1,000 flight hours after the effective date of this AD.

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Affected Aircraft

Airbus Model A330-200 and -300 series airplanes, and Model A340-200 and -300 series airplanes equipped with check valves P/N CAR401 installed in production through Airbus modification 54491, or installed in service through Airbus Service Bulletin (SB) A330-29-3101 or Airbus SB A340-29-4078.

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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