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AD FAA-2009-0789

Airworthiness Directives; Airbus Model A300 B2-1C, B2-203, B2K-3C, B4-103, B4-203, B4-2C Airplanes; Model A310 Series Airplanes; and Model A300 B4-601, B4-603, B4-605R, B4-620, B4-622, and B4-622R Airplanes

Summary

The FAA is correcting a typographical error in an existing airworthiness directive (AD) that was published in the Federal Register on March 11, 2010. The error resulted in an imprecise compliance time in a table. This AD applies to certain Airbus Model A300 B2-1C, B2-203, B2K-3C, B4-103, B4-203, B4-2C airplanes; Model A310 series airplanes; and Model A300 B4-601, B4-603, B4-605R, B4-620, B4-622, and B4-622R airplanes. This AD requires repetitive inspections to detect cracks of the pylon side panels (upper section) at rib 8; and corrective actions if necessary.

Directive Details

AD Number

FAA-2009-0789

Document Number

2010-9521

Type

Rule

Publication Date

May 4, 2010

Effective Date

May 4, 2010

Affected Manufacturer

Airbus Model A300 B2-1C, B2-203, B2K-3C, B4-103, B4-203, B4-2C

Criticality

routine

Emergency

No

Docket ID

Docket No. FAA-2009-0789

Official Documents

View all ADs for Airbus Model A300 B2-1C, B2-203, B2K-3C, B4-103, B4-203, B4-2C →

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