AD 2005-15-02

final rule
Data completeness: 70%

Airworthiness Directives; Airbus Model A320-111 Airplanes and Model A320-200 Series Airplanes

AD Number
2005-15-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2005-20500
FR Citation
70 FR 41946

Applicability

TypeManufacturerModelDetails
aircraft Airbus A320-111 Airworthiness Directives; Airbus Model A320-111 Airplanes and Model A320-200 Series Airplanes

Unsafe Condition

Reports of unsuccessful in-flight ram air turbine (RAT) tests during which a deployed RAT failed to pressurize the blue hydraulic circuit of the RAT system.

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

Required Actions

Bleed accumulated air from, or perform a ground functional test of, the RAT system; modify and reidentify the airborne ground check module of the RAT system; and replace the RAT reducer assembly if applicable.

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

Compliance Time

Within 3 days or 20 flight hours after the effective date of this AD, whichever occurs first, for certain maintenance actions. Within 35 months after the effective date of this AD for AGCM and reducer replacement.

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

Affected Aircraft

Airbus Model A320-111 airplanes and Model A320-200 series airplanes, certificated in any category; equipped with Hamilton Sundstrand airborne ground check module (AGCM) having part number 769104, 769105, or 769106 installed; except those airplanes on which Airbus Modification 27189 has been done in production and on which Airbus Modification 28413 has not been done.

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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