Published 2009-05-06 · Federal Register document E9-10421
Airworthiness Directives; Airbus Model A318, A319, A320, and A321 Airplanes
Publication summary
The FAA is correcting a typographical error in an existing airworthiness directive (AD) that was published in the Federal Register on March 24, 2009 (74 FR 12247). The error resulted in publication of an incorrect AD number. This AD applies to certain Airbus Model A318, A319, A320, and A321 airplanes. This AD requires the installation of improved cockpit door latch/striker assemblies.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:30.011257+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2009-cb57e588bd107238
- Source row
- results[116]
- Raw source SHA-256
- cb57e588bd10723805ef0ea28ddc0685de14711012023c7e7d12178879efaeed
Correction notice · separate source edition
Recorded publication clauses
- AD identifier printed in this edition
- 2009-06-22
- Effective date printed in this edition
- Unknown
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Find all recorded historical references to AD 2009-06-22 · 0 printed reference observations in this pinned collection.
These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.
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They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.
Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 899982adb80168b35714c96c63f5a28a7fdfe3e1cc614ec422bd1bc12dd027cc. Source manifest: 3020edc9cb1d20f5dd24acf1da6f0976b0a0dc74d56ecde7ece0be19938196a8.
Official source · 2009-05-06
Publication text
This is the complete recorded text of this dated publication.
Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.
Read the complete official publication text
[Federal Register Volume 74, Number 86 (Wednesday, May 6, 2009)]
[Rules and Regulations]
[Page 20867]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: E9-10421]
========================================================================
Rules and Regulations
Federal Register
________________________________________________________________________
This section of the FEDERAL REGISTER contains regulatory documents
having general applicability and legal effect, most of which are keyed
to and codified in the Code of Federal Regulations, which is published
under 50 titles pursuant to 44 U.S.C. 1510.
The Code of Federal Regulations is sold by the Superintendent of Documents.
Prices of new books are listed in the first FEDERAL REGISTER issue of each
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Federal Register / Vol. 74, No. 86 / Wednesday, May 6, 2009 / Rules
and Regulations
[[Page 20867]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2008-1327; Directorate Identifier 2008-NM-161-AD;
Amendment 39-15859; AD 2009-06-22]
RIN 2120-AA64
Airworthiness Directives; Airbus Model A318, A319, A320, and A321
Airplanes
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 March 24, 2009 (74 FR 12247). The error resulted in publication of
an incorrect AD number. This AD applies to certain Airbus Model A318,
A319, A320, and A321 airplanes. This AD requires the installation of
improved cockpit door latch/striker assemblies.
DATES: Effective April 28, 2009.
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 March 12, 2009, the FAA issued AD 2009-
06-22, amendment 39-15859 (74 FR 12247, March 24, 2009), for certain
Airbus Model A318, A319, A320, and A321 airplanes. The AD requires the
installation of improved cockpit door latch/striker assemblies.
As published, that final rule incorrectly specified the AD number
in a single location in the AD as ``2009-09-22'' instead of ``2009-06-
22.''
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 April 28, 2009.
Sec. 39.13 [Corrected]
0
In the Federal Register of March 24, 2009, on page 12249, in the first
column, paragraph 2. of PART 39--AIRWORTHINESS DIRECTIVES is corrected
to read as follows:
* * * * *
2009-06-22 Airbus: Amendment 39-15859. Docket No. FAA-2008-1327;
Directorate Identifier 2008-NM-161-AD.
* * * * *
Issued in Renton, Washington, on April 27, 2009.
Stephen P. Boyd,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E9-10421 Filed 5-5-09; 8:45 am]
BILLING CODE 4910-13-P
Why this text is shown
The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T03:24:07.017072+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.
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- Source SHA-256
- 0a20f5a630935064e52c37f4b18dd615406d7f5332688d399db3e29ed0932214
- Text SHA-256
- 899982adb80168b35714c96c63f5a28a7fdfe3e1cc614ec422bd1bc12dd027cc
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