AD 2017-04-09

final rule
Data completeness: 70%

Airworthiness Directives; Airbus Airplanes

AD Number
2017-04-09
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2016-9305
FR Citation
82 FR 11304

Applicability

TypeManufacturerModelDetails
aircraft Airbus A330-243 Airworthiness Directives; Airbus Airplanes

Unsafe Condition

Cracking of air intake cowls, worn and detached attachment links, fractured thermal anti-ice (TAI) piccolo tubes, and loose or missing attachment rivets of the inner boundary angles (IBAs) and outer boundary angles (OBAs) of the forward bulkhead.

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

Required Actions

Inspect piccolo tubes and mount links, the aft side of the forward bulkhead, and OBAs; inspect certain areas of the forward bulkhead; inspect IBA and OBA attachment rivets; replace the engine air intake cowl assembly and repair pulled, loose, or missing rivets if necessary.

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

Compliance Time

Before further flight to within 100 flight cycles, depending on findings.

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.

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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.