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, 36674 [06-5739]

Download as PDF 36674 Federal Register / Vol. 71, No. 124 / Wednesday, June 28, 2006 / Rules and Regulations Material Incorporated by Reference DEPARTMENT OF TRANSPORTATION (l) You must use PATS Aircraft Service Bulletin SA979NE–28–SB–28_IR, dated April 3, 2006, and the applicable PATS Aircraft supplement to the Boeing 757–200 Airplane Flight Manual identified in Table 2 of this AD, as applicable, to perform the actions that are required by this AD, unless the AD specifies otherwise. 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 TABLE 2.—AIRPLANE FLIGHT MANUAL Airworthiness Directives; Goodrich SUPPLEMENTS FOR INCORPORATION Evacuation Systems Approved Under Technical Standard Order (TSO) TSO– BY REFERENCE PATS Aircraft airplane flight manual supplement— Dated— 142 143 144 145 146 May May May May May 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 ............................ ............................ ............................ ............................ ............................ 31, 31, 31, 31, 31, 2006. 2006. 2006. 2006. 2006. Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule; correction. AGENCY: The Director of the Federal Register approved the incorporation by reference of these documents in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Contact PATS Aircraft, LLC, Product Support, 21652 Nanticoke Avenue, Georgetown, DE 19947, for a copy of this service information. You may review copies at the Docket Management Facility, U.S. Department of Transportation, 400 Seventh Street, SW., Room PL–401, Nassif Building, Washington, DC; on the Internet at https://dms.dot.gov; or at the National Archives and Records Administration (NARA). For information on the availability of this material at the NARA, call (202) 741–6030, or go to https:// www.archives.gov/federal_register/ code_of_federal_regulations/ ibr_locations.html. Issued in Renton, Washington, on June 15, 2006. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 06–5702 Filed 6–27–06; 8:45 am] mstockstill on PROD1PC61 with RULES BILLING CODE 4910–13–P VerDate Aug<31>2005 16:22 Jun 27, 2006 Jkt 208001 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 https:// 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. PO 00000 Frm 00014 Fmt 4700 Sfmt 4700 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. SUPPLEMENTARY INFORMATION: § 39.13 [Corrected] 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: * * * * * I 2. The Federal Aviation Administration (FAA) amends § 39.13 by adding the following new airworthiness directive (AD): I 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 DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 97 [Docket No. 30500 Amdt. No. 3172] Standard Instrument Approach Procedures, Weather Takeoff Minimums; Miscellaneous Amendments Federal Aviation Administration (FAA), DOT. ACTION: Final rule. AGENCY: E:\FR\FM\28JNR1.SGM 28JNR1

Agencies

[Federal Register Volume 71, Number 124 (Wednesday, June 28, 2006)]
[Rules and Regulations]
[Page 36674]
From the Federal Register Online via the Government Printing 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 
https://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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