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Published 2008-03-03 · Federal Register document E8-3930

Airworthiness Directives; Airbus Model A318, A319, A320, and A321 Series Airplanes

Publication summary

The FAA is correcting a typographical error in an existing airworthiness directive (AD) that was published in the Federal Register on December 10, 2007 (72 FR 69593). The error resulted in a potential for confusion regarding the applicability of the AD. This AD applies to certain Airbus Model A318, A319, A320, and A321 series airplanes. This AD requires inspections of the landing gear (LG) selector valve 40GA and the LG door selector valve 41GA, to identify a possible hydraulic leak. The corrective action includes replacing the LG selector valve 40GA and/or the LG door selector valve 41GA if necessary.

Why this record is shown

Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:26.953736+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2008-e9cf118935fdae82
Source row
results[86]
Raw source SHA-256
e9cf118935fdae82a000e2c01764c770bd79679c1dd4c2b00fdcd3b030f92fe5

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition
2007-25-12
Effective date printed in this edition
Unknown

This correction is a separate source edition; it is not counted as a new adopted rule.

No adopted-clause structure was recorded for this source edition. Read the complete text; no applicability conclusion has been inferred.

No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.

Find all recorded historical references to AD 2007-25-12 · 0 printed reference observations in this pinned collection.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.

Why these observations are shown

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: 6f06c133128616fb0fa35357e43903e824ebd5fcf6c6af846d692c90aa6a032e. Source manifest: 684cd31ead84eb14d6aebb2b53463b9d674f3e16dc6b6bc98118184b4e3a669b.

Official source · 2008-03-03

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 73, Number 42 (Monday, March 3, 2008)]
[Rules and Regulations]
[Pages 11346-11347]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: E8-3930]


=======================================================================
-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2007-29249; Directorate Identifier 2007-NM-112-AD; 
Amendment 39-15294; AD 2007-25-12]
RIN 2120-AA64


Airworthiness Directives; Airbus Model A318, A319, A320, and A321 
Series 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 December 10, 2007 (72 FR 69593). The error resulted in a potential 
for confusion regarding the applicability of the AD. This AD applies to 
certain Airbus Model A318, A319, A320, and A321 series airplanes. This 
AD requires inspections of the landing gear (LG) selector valve 40GA 
and the LG door selector valve 41GA, to identify a possible hydraulic 
leak. The corrective action includes replacing the LG selector valve 
40GA and/or the LG door selector valve 41GA if necessary.

DATES: Effective January 14, 2008.

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, FAA, Transport Airplane Directorate, 
1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425) 
227-2141; fax (425) 227-1149.

SUPPLEMENTARY INFORMATION: On November 21, 2007, the FAA issued AD 
2007-25-12, amendment 39-15294 (72 FR 69593, December 10, 2007), for 
certain Airbus Model A318, A319, A320, and A321 series airplanes. The 
AD requires inspections of the landing gear (LG) selector valve 40GA 
and the LG door selector valve 41GA, to identify a possible hydraulic 
leak. The corrective action includes replacing the LG selector valve 
40GA and/or the LG door selector valve 41GA if necessary.
    As published, the AD applies to airplanes identified in paragraphs 
(c)(1) ``and'' (c)(2) of this AD instead of those identified in 
paragraph (c)(1) ``or'' (c)(2) of this AD.
    This change is relieving in nature, and 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 January 14, 2008.


Sec.  39.13   [Corrected]

0
In the Federal Register of December 10, 2007, on page 69594, in the 
second column, paragraph (c) of AD 2007-25-12 is corrected to read as 
follows:
* * * * *
    (c) This AD applies to Airbus Model A318, A319, A320, and A321 
series airplanes, certificated in any category,

[[Page 11347]]

except those identified in paragraph (c)(1) or (c)(2) of this AD.
* * * * *

    Issued in Renton, Washington, on February 25, 2008.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. E8-3930 Filed 2-29-08; 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 2026-10-09T03:32:37.746832+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

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Source SHA-256
bf6b12e0b5e0435ac49c840f1eccf2ecf00d3e65829ff737007215a36c0dfcd7
Text SHA-256
6f06c133128616fb0fa35357e43903e824ebd5fcf6c6af846d692c90aa6a032e

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These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.

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