Back to publication catalog

Published 2012-04-23 · Federal Register document 2012-9576

Airworthiness Directives; Airbus Airplanes

Publication summary

The FAA is correcting an airworthiness directive (AD) that published in the Federal Register. That AD applies to all Airbus Model A300 B4-600, B4-600R, and F4-600R series airplanes, Model A300 C4-605R Variant F airplanes (collectively called A300-600 series airplanes), and Model A310 series airplanes. The agency docket number specified throughout the final rule is incorrect. This document corrects that error. In all other respects, the original document remains the same.

Why this record is shown

Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:39.502075+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2012-08bffa249ae9a205
Source row
results[126]
Raw source SHA-256
08bffa249ae9a2053bbfc0d74663d089914e83fb91f9bc4c8409ea28239f6875

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition
2012-06-02
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Find all recorded historical references to AD 2012-06-02 · 0 printed reference observations in this pinned collection.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: 68660e373055fedd73a92a3c62c81c90df5e1a6c2893569ddab3ac3fdda9290c. Source manifest: b5add215dde273c853235e78e063f0039682b9f90b78b333d6905853163fb48d.

Official source · 2012-04-23

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 77, Number 78 (Monday, April 23, 2012)]
[Rules and Regulations]
[Page 24137]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2012-9576]



========================================================================
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 
week.

========================================================================


Federal Register / Vol. 77, No. 78 / Monday, April 23, 2012 / Rules 
and Regulations

[[Page 24137]]



DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2011-1324; Directorate Identifier 2011-NM-104-AD; 
Amendment 39-16983; AD 2012-06-02]
RIN 2120-AA64


Airworthiness Directives; Airbus Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; correction.

-----------------------------------------------------------------------

SUMMARY: The FAA is correcting an airworthiness directive (AD) that 
published in the Federal Register. That AD applies to all Airbus Model 
A300 B4-600, B4-600R, and F4-600R series airplanes, Model A300 C4-605R 
Variant F airplanes (collectively called A300-600 series airplanes), 
and Model A310 series airplanes. The agency docket number specified 
throughout the final rule is incorrect. This document corrects that 
error. In all other respects, the original document remains the same.

DATES: This final rule is effective April 25, 2012.

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 (phone: 800-647-5527) is 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: Dan Rodina, Aerospace Engineer, 
International Branch, ANM-116, Transport Airplane Directorate, FAA, 
1601 Lind Avenue SW., Renton, Washington 98057-3356; telephone (425) 
227-2125; fax (425) 227-1149.

SUPPLEMENTARY INFORMATION: Airworthiness Directive (AD) 2012-06-02, 
Amendment 39-16983 (77 FR 16430, March 21, 2012), currently requires 
replacing a certain aluminum high pressure pipe with a new corrosion 
resistant stainless steel pipe, for all Airbus Model A300 B4-600, B4-
600R, and F4-600R series airplanes, Model A300 C4-605R Variant F 
airplanes (collectively called A300-600 series airplanes), and Model 
A310 series airplanes.
    As published, the agency docket number specified throughout the AD 
is incorrect.
    No other part of the preamble or regulatory information has been 
changed; therefore, only the changed portion of the final rule is being 
published in the Federal Register.
    The effective date of this AD remains April 25, 2012.

Correction of Non-Regulatory Text

    In the Federal Register of March 21, 2012, AD 2012-06-02, Amendment 
39-16983 (77 FR 16430), is corrected as follows:
    On page 16430, in the second column, change the docket number to 
read as follows:

    ``[Docket No. FAA-2011-1324; Directorate Identifier 2011-NM-104-
AD; Amendment 39-16983; AD 2012-06-02]''

Correction of Regulatory Text


Sec.  39.13  [Corrected]

0
In the Federal Register of March 21, 2012, AD 2012-06-02, Amendment 39-
16983 (77 FR 16430), on page 16431, in the third column, the product 
identification line of AD 2012-06-02 is corrected to read as follows:
* * * * *
2012-06-02 Airbus: Amendment 39-16983, Docket No. FAA-2011-1324; 
Directorate Identifier 2011-NM-104-AD.
* * * * *

    Issued in Renton, Washington, on April 13, 2012.
John P. Piccola,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2012-9576 Filed 4-20-12; 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 2026-10-09T03:03:07.533599+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

Open the captured official edition

Source SHA-256
c2cf9405faa84db47f4b2dd6f1df61fb8932392f62b23c3e43532d934acb47e5
Text SHA-256
68660e373055fedd73a92a3c62c81c90df5e1a6c2893569ddab3ac3fdda9290c

Return to the full metadata catalog · Search complete publication text · Explore retained publication text and evidence

Coverage and limits

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.

The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.