AD 2005-22-10

final rule
Data completeness: 70%

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

AD Number
2005-22-10
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2002-NM-298-AD
FR Citation
70 FR 62232

Applicability

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

Unsafe Condition

Mis-rigged elevator servo-controls due to improperly installed tail cone triangles during production, which could result in low hinge moments and possible vibrations if combined with elevator freeplay.

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

Required Actions

Perform a detailed inspection to determine the position of each tail cone triangle. If the triangles are not in the correct position, rig the elevators in accordance with A320 AMM Task 27-34-00-820-003. Alternative methods of compliance (AMOC) may be requested.

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

Compliance Time

Within 800 flight hours after the effective date of this AD.

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Affected Aircraft

Airbus Model A320-111, -211, -212, -214, -231, -232, and -233 airplanes, 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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