AD 2011-22-02

final rule
Data completeness: 70%

Airworthiness Directives; Airbus Airplanes

AD Number
2011-22-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2011-0255
FR Citation
76 FR 65936

Applicability

TypeManufacturerModelDetails
aircraft Airbus A310 Airworthiness Directives; Airbus Airplanes
aircraft Aviat Various Airworthiness Directives; Airbus Airplanes

Unsafe Condition

Wire damages at the pylon/wing interface due to installation quality issues and lack of information in installation drawings and job cards. Low Pressure Valve (LPV) wires were not segregated by design, leading to potential wire chafing that could impact fire protection and detection systems, and may induce dormant failures on LPV preventing its closure in case of fire upstream the High Pressure Valve (HPV).

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

Required Actions

Inspect wires for damage at the pylon/wing interface and repair if necessary. Incorporate Modification 13541 in accordance with Airbus Service Bulletin A310-24-2106, Revision 1.

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

Compliance Time

Within 30 months of the effective date (November 29, 2011).

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

Affected Aircraft

Airbus Model A310 series airplanes; Model A300 B4-600, B4-600R, and F4-600R series airplanes; and Model C4-605R variant F airplanes (collectively called A300-600 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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