AD 2012-22-12

final rule
Data completeness: 70%

Airworthiness Directives; Airbus Airplanes

AD Number
2012-22-12
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2012-0428
FR Citation
77 FR 67263

Applicability

TypeManufacturerModelDetails
aircraft Airbus A330-243 Airworthiness Directives; Airbus Airplanes
engine Rolls-Royce Trent Airworthiness Directives; Airbus Airplanes

Unsafe Condition

Cracking of air intake cowls, worn and detached attachment links, and fractured thermal anti-ice (TAI) piccolo tubes on Rolls-Royce Trent engines. Forward bulkhead damage in conjunction with a broken piccolo tube could lead to degraded structural integrity of the engine nose cowl and potential in-flight detachment of the outer barrel.

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

Required Actions

Inspect piccolo tubes, piccolo tube mount links, the aft side of the forward bulkhead, and outer boundary angles (OBA) for cracks, fractures, and broken links. Perform corrective actions if necessary, including replacing the affected engine air intake cowl with a new or serviceable cowl.

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

All Airbus Model A330-243, -243F, -341, -342, and -343 airplanes equipped with Rolls-Royce Trent engines.

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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