Airworthiness Directives; Airbus Model A319-100, A320-200, A321-100, and A321-200 Series Airplanes

[Federal Register Volume 75, Number 106 (Thursday, June 3, 2010)]
[Rules and Regulations]
[Pages 31282-31283]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2010-13231]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2005-22919; Directorate Identifier 2005-NM-087-AD; 
Amendment 39-14582; AD 2006-09-11]
RIN 2120-AA64


Airworthiness Directives; Airbus Model A319-100, A320-200, A321-
100, and A321-200 Series Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

ACTION: Final rule; correction.

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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.


Sec.  39.13  [Corrected]

    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:
* * * * *

[[Page 31283]]

    (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.
[FR Doc. 2010-13231 Filed 6-2-10; 8:45 am]
BILLING CODE 4910-13-P

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