# 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
> **Rule** · Final rule; correction. · Published 2010-05-04 · Effective 2010-05-04 · 75 FR 23572
## Document
- **Document number:** 2010-9521
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule; correction.
- **Citation:** 75 FR 23572
- **Publication date:** 2010-05-04
- **Effective date:** 2010-05-04
- **FAA docket:** Docket No. FAA-2009-0789
## Abstract

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.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2010/05/04/2010-9521/airworthiness-directives-airbus-model-a300-b2-1c-b2-203-b2k-3c-b4-103-b4-203-b4-2c-airplanes-model)
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