AD 2006-18-10

final rule
Data completeness: 70%

Airworthiness Directives; Airbus Model A340-541 and -642 Airplanes

AD Number
2006-18-10
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2006-25722
FR Citation
71 FR 52410

Applicability

TypeManufacturerModelDetails
aircraft Airbus A340-541 and -642 Airworthiness Directives; Airbus Model A340-541 and -642 Airplanes

Unsafe Condition

Failure of the anti-stall valve on the hydraulic pump of the ram air turbine (RAT) due to poor installation of the anti-stall valve sleeve, causing a shift in the anti-stall speed setting and leading to inability to supply adequate pressure to activate the RAT.

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

Required Actions

Inspect the anti-stall valve sleeve of the RAT for proper installation. Determine the part number of the modification plate on the hydraulic pump of the RAT. Perform follow-on corrective actions, including reworking the anti-stall valve or replacing the RAT with a new one, and conducting an operational test of the new RAT if necessary.

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

Compliance Time

Before further flight

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

Affected Aircraft

Airbus Model A340-541 and -642 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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