AD 2005-18-11

final rule
Data completeness: 70%

Airworthiness Directives; Airbus Model A340-200 and A340-300 Series Airplanes

AD Number
2005-18-11
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2005-22291
FR Citation
70 FR 53051

Applicability

TypeManufacturerModelDetails
aircraft Airbus A340-200 and A340-300 Airworthiness Directives; Airbus Model A340-200 and A340-300 Series Airplanes

Unsafe Condition

Incorrect diameter of the spotfacings for two of the pylon-to-engine attachment bolts on the pyramid forward fitting, causing possible damage to the spotfacing area and cracking/wear of the pylon-to-engine attachment bolt, which could result in separation of an engine from the airplane.

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

Required Actions

Inspect for discrepancies of the spotfacing for the pylon-to-engine attachment bolts on the pyramid forward fitting of the engine pylon. Repair if necessary, including measuring and machining the spotfacing to the correct dimension and installing new bolts and washers.

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 A340-200 and A340-300 series airplanes manufactured in France and certificated for operation in the United States.

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.