# [Corrected]
**AGENCY:**
Federal Aviation Administration (FAA), Department of Transportation (DOT).
**ACTION:**
Final rule; correction.
**SUMMARY:**
The FAA is correcting a typographical error in an existing airworthiness directive (AD) that was published in the *Federal Register* on May 12, 2006. The error resulted in an incorrect component maintenance manual number. This AD applies to certain Airbus Model A319-100, A320-200, A321-100, and A321-200 series airplanes. This AD requires repetitive inspections for corrosion in the inside and outside lower walls of each type A, D, E, and F lavatory wall that has at least one wall-mounted cabin attendant seat, and related investigative and corrective actions if necessary.
**DATES:**
This correction is effective June 3, 2010. The effective date of AD 2006-09-11 remains June 16, 2006.
**ADDRESSES:**
You may examine the AD docket on the Internet at *http://www.regulations.gov* ; or in person at the Docket Management Facility between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this AD, the regulatory evaluation, any comments received, and other information. The address for the Docket Office (telephone 800-647-5527) is the Document Management Facility, U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC 20590.
**FOR FURTHER INFORMATION CONTACT:**
Tim Dulin, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425) 227-2141; fax (425) 227-1149.
**SUPPLEMENTARY INFORMATION:**
On April 26, 2006, the FAA issued AD 2006-09-11, Amendment 39-14582 (71 FR 27595, May 12, 2006), for certain Airbus Model A319-100, A320-200, A321-100, and A321-200 series airplanes. The AD requires repetitive inspections for corrosion in the inside and outside lower walls of each type A, D, E, and F lavatory wall that has at least one wall-mounted cabin attendant seat, and related investigative and corrective actions if necessary.
As published, paragraphs (h)(1)(iii) and (h)(2)(ii) of the AD specifies in error Airbus Component Maintenance Manual Lavatory E 25-41-52. Airbus Component Maintenance Manual Lavatory E 25-41-52 does not exist. The correct Airbus Component Maintenance Manual Lavatory E is 25-43-52.
No other part of the regulatory information has been changed; therefore, the final rule is not republished in the *Federal Register.*
The effective date of this AD remains June 16, 2006.
**14 CFR Part 39**
§ 39.13
In the *Federal Register* of May 12, 2006, on page 27597, in the third column, paragraph (h)(1)(iii) of AD 2006-09-11 is corrected to read as follows:
(iii) Airbus CMM Lavatory E 25-43-52.
In the *Federal Register* of May 12, 2006, on page 27597, in the third column, paragraph (h)(2)(ii) of AD 2006-09-11 is corrected to read as follows:
(ii) For lavatories D and E: Airbus Service Bulletin A320-25-1365, dated February 18, 2005, references Airbus CMM Lavatory D 25-43-51; and Airbus CMM Lavatory E 25-43-52, as applicable, as an additional source of guidance for doing the replacement.
Issued in Renton, Washington, on May 25, 2010.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification Service.