AD 2017-24-03

final rule
Data completeness: 70%

Airworthiness Directives; Airbus Airplanes

AD Number
2017-24-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2017-0690
FR Citation
82 FR 56167

Applicability

TypeManufacturerModelDetails
aircraft Airbus A319-115 Airworthiness Directives; Airbus Airplanes

Unsafe Condition

Absence of cadmium plating on the rod end threads of tie rod assemblies, which could lead to galvanic corrosion and potential rod end failure, loss of a MLG door, and injury to persons on the ground.

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

Required Actions

Inspect tie rod assemblies installed on the hinged fairing assembly of the main landing gear (MLG). Replace affected tie rod assemblies 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 A319-115, A319-132, A320-214, A320-232, A321-211, A321-213, and A321-231 airplanes, as identified in Airbus Service Bulletin A320-52-1167.

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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