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.
Why this record is shown
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
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Find all recorded historical references to AD 2006-12-08 · 0 printed reference observations in this pinned collection.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: 6dbfdf5f62809b7cd13ee6d63cdd09ef6548a0675f1edae5f52e129d5f4b1e30. Source manifest: 73bb3a5d10fef26868a37932696fe8f555e287f6d64b34f2da5e582b5acf4ff8.
Official source · 2006-06-28
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 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]
-----------------------------------------------------------------------
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
Why this text is shown
The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T03:45:22.035940+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.
Open the captured official edition
- Source SHA-256
- d4d05fc882e1b77192ac3dd2f876426e7fb8e142bc5f62a006a2dc5e6c0446dc
- Text SHA-256
- 6dbfdf5f62809b7cd13ee6d63cdd09ef6548a0675f1edae5f52e129d5f4b1e30
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.