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Published 2006-06-28 · Federal Register document 06-5739

Airworthiness Directives; Goodrich Evacuation Systems Approved Under Technical Standard Order (TSO) TSO-C69b and Installed on Airbus Model A330-200 and -300 Series Airplanes, Model A340-200 and -300 Series Airplanes, and Model A340-541 and -642 Airplanes

Publication summary

The FAA is correcting an inadvertent error in an existing airworthiness directive (AD) that was published in the Federal Register on June 12, 2006 (71 FR 33606). The error resulted in an incorrect reference to the airplane manufacturer instead of the TSO holder. This AD applies to Goodrich evacuation systems approved under TSO-C69b and installed on certain Airbus Model A330-200 and -300 series airplanes, Model A340-200 and -300 series airplanes, and Model A340-541 and -642 airplanes. This AD requires inspecting to determine the part number of the pressure relief valves on the affected Goodrich evacuation systems, and corrective action if necessary.

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Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:20.745856+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2006-8d787f8b35bc8016
Source row
results[238]
Raw source SHA-256
8d787f8b35bc80165a417cea66de09cd32a1700face13759db364c607e405963

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition
2006-12-08
Effective date printed in this edition
Unknown

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Find all recorded historical references to AD 2006-12-08 · 0 printed reference observations in this pinned collection.

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Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 6dbfdf5f62809b7cd13ee6d63cdd09ef6548a0675f1edae5f52e129d5f4b1e30. Source manifest: 73bb3a5d10fef26868a37932696fe8f555e287f6d64b34f2da5e582b5acf4ff8.

Official source · 2006-06-28

Publication text

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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 71, Number 124 (Wednesday, June 28, 2006)]
[Rules and Regulations]
[Page 36674]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 06-5739]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2006-23890; Directorate Identifier 2005-NM-229-AD; 
Amendment 39-14633; AD 2006-12-08]
RIN 2120-AA64


Airworthiness Directives; Goodrich Evacuation Systems Approved 
Under Technical Standard Order (TSO) TSO-C69b and Installed on Airbus 
Model A330-200 and -300 Series Airplanes, Model A340-200 and -300 
Series Airplanes, and Model A340-541 and -642 Airplanes

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

ACTION: Final rule; correction.

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

SUMMARY: The FAA is correcting an inadvertent error in an existing 
airworthiness directive (AD) that was published in the Federal Register 
on June 12, 2006 (71 FR 33606). The error resulted in an incorrect 
reference to the airplane manufacturer instead of the TSO holder. This 
AD applies to Goodrich evacuation systems approved under TSO-C69b and 
installed on certain Airbus Model A330-200 and -300 series airplanes, 
Model A340-200 and -300 series airplanes, and Model A340-541 and -642 
airplanes. This AD requires inspecting to determine the part number of 
the pressure relief valves on the affected Goodrich evacuation systems, 
and corrective action if necessary.

DATES: Effective July 17, 2006.

ADDRESSES: The AD docket contains the proposed AD, comments, and any 
final disposition. You may examine the AD docket on the Internet at 
http://dms.dot.gov, or in person at the Docket Management Facility 
office between 9 a.m. and 5 p.m., Monday through Friday, except Federal 
holidays. The Docket Management Facility office (telephone (800) 647-
5227) is located on the plaza level of the Nassif Building at the U.S. 
Department of Transportation, 400 Seventh Street, SW., Room PL-401, 
Washington, DC. This docket number is FAA-2006-23890; the directorate 
identifier for this docket is 2005-NM-229-AD.

FOR FURTHER INFORMATION CONTACT: Tracy Ton, Aerospace Engineer, Cabin 
Safety/Mechanical and Environmental Systems Branch, ANM-150L, FAA, Los 
Angeles Aircraft Certification Office, 3960 Paramount Boulevard, 
Lakewood, California 90712-4137; telephone (562) 627-5352; fax (562) 
627-5210.

SUPPLEMENTARY INFORMATION: On May 31, 2006, the FAA issued AD 2006-12-
08, amendment 39-14633 (71 FR 33606, June 12, 2006), for Goodrich 
evacuation systems approved under TSO-C69b and installed on certain 
Airbus Model A330-200 and -300 series airplanes, Model A340-200 and -
300 series airplanes, and Model A340-541 and -642 airplanes. The AD 
requires inspecting to determine the part number of the pressure relief 
valves on the affected Goodrich evacuation systems, and corrective 
action if necessary.
    As published, the final rule identifies an incorrect reference to 
the airplane manufacturer (Airbus) in the regulatory text of the AD. 
The correct reference is Goodrich (formerly BF Goodrich).
    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 July 17, 2006.


Sec.  39.13  [Corrected]

0
In the Federal Register of June 12, 2006, on page 33607, in the second 
column, paragraph 2 of PART 39--AIRWORTHINESS DIRECTIVES of AD 2006-12-
08 is corrected to read as follows:
* * * * *
0
2. The Federal Aviation Administration (FAA) amends Sec.  39.13 by 
adding the following new airworthiness directive (AD):

2006-12-08 Goodrich (Formerly BF Goodrich): Amendment 39-14633. 
Docket No. FAA-2006-23890; Directorate Identifier 2005-NM-229-AD.
* * * * *

    Issued in Renton, Washington, on June 20, 2006.
Kalene C. Yanamura,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 06-5739 Filed 6-27-06; 8:45 am]
BILLING CODE 4910-13-P


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Text SHA-256
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