AD 2015-23-05

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Airbus Airplanes

AD Number
2015-23-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2014-1043
FR Citation
80 FR 72569

Applicability

TypeManufacturerModelDetails
aircraft Airbus A330-200 Airworthiness Directives; Airbus Airplanes

Unsafe Condition

Cracked support strut body ends at a certain frame location of the trimmable horizontal stabilizer (THS), which could lead to the loss of all four THS support struts, making the remaining structure unable to carry limit loads, resulting in the loss of the horizontal tail plane.

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

Required Actions

Inspect for cracking of the strut ends of the THS support located at a certain frame in the tail cone, and replace if necessary. Reinstall or install reinforcing clamps on certain strut ends.

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

Compliance Time

Within 12 months of effective date

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Affected Aircraft

All Airbus Model A330-200, A330-200 Freighter, A330-300 series airplanes; and Model A340-200 and A340-300 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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