[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]
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