Airworthiness Directives; Airbus Model A340-200 and -300 Series Airplanes, 57125 [05-19556]

Download as PDF Federal Register / Vol. 70, No. 189 / Friday, September 30, 2005 / Rules and Regulations SUMMARY: The FAA is correcting a typographical error in an existing airworthiness directive (AD) that was published in the Federal Register on September 15, 2005 (70 FR 54474). The error resulted in an inadvertent reference to a nonexistent paragraph. This AD applies to certain Boeing Model 747–100, 747–100B, 747–100B SUD, 747–200B, 747–200C, 747–200F, 747–300, 747SR, and 747SP series airplanes. This AD requires repetitive detailed and ultrasonic inspections of the thrust links of the rear engine mounts for any crack or fracture and corrective actions if necessary. DATES: Effective September 30, 2005. 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–2005–22413; the directorate identifier for this docket is 2005–NM– 167–AD. FOR FURTHER INFORMATION CONTACT: Ivan Li, Aerospace Engineer, Airframe Branch, ANM–120S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue, SW., Renton, Washington 98055–4056; telephone (425) 917–6437; fax (425) 917–6590. SUPPLEMENTARY INFORMATION: On September 6, 2005, the FAA issued AD 2005–19–06, amendment 39–14271 (70 FR 54474, September 15, 2005), for certain Boeing Model 747–100, 747– 100B, 747–100B SUD, 747–200B, 747– 200C, 747–200F, 747–300, 747SR, and 747SP series airplanes; equipped with Pratt & Whitney JT9D–3 and –7 series engines, except JT9D–70 engines. The AD requires repetitive detailed and ultrasonic inspections of the thrust links of the rear engine mounts for any crack or fracture and corrective actions if necessary. As published, the requirements of paragraph (h)(1) of the AD inadvertently reference doing the repetitive replacements ‘‘* * * at the applicable compliance time specified in paragraph (h)(1)(i) or (h)(2)(ii) of this AD.’’ However, there is no paragraph (h)(2)(ii) in the AD. We have removed reference to paragraph (h)(2)(ii) and replaced it with the correct reference to paragraph (h)(1)(ii). VerDate Aug<31>2005 15:28 Sep 29, 2005 Jkt 205001 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 September 30, 2005. § 39.13 [Corrected] In the Federal Register of September 15, 2005, on page 54476, in the third column, paragraph (h)(1) of AD 2005– 19–06 is corrected to read as follows: * * * * * (1) Replace the cracked thrust link with a new or overhauled thrust link in accordance with Part 2 of the service bulletin; except as provided by paragraph (i) of this AD. Repeat the replacement at the applicable compliance time specified in paragraph (h)(1)(i) or (h)(1)(ii) of this AD. * * * * * I Issued in Renton, Washington, on September 26, 2005. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 05–19564 Filed 9–29–05; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2005–22405; Directorate Identifier 2002–NM–243–AD; Amendment 39–14269; AD 2005–19–04] RIN 2120–AA64 Airworthiness Directives; Airbus Model A340–200 and –300 Series Airplanes Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule; correction. AGENCY: SUMMARY: The FAA is correcting a typographical error in an existing airworthiness directive (AD) that was published in the Federal Register on September 14, 2005 (70 FR 54251). The error resulted in in an incorrect Docket No. This AD applies to certain Airbus Model A340–200 and –300 series airplanes. This AD requires revising the airplane flight manual to incorporate new procedures for the flightcrew to follow to correct miscalculation of the takeoff and accelerating or stopping distance of the airplane during a ferry flight under certain conditions. DATES: Effective September 29, 2005. ADDRESSES: The AD docket contains the proposed AD, comments, and any final PO 00000 Frm 00005 Fmt 4700 Sfmt 4700 57125 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–2005–22405; the directorate identifier for this docket is 2002–NM– 243–AD. Dan Rodina, Aerospace Engineer, International Branch, ANM–116, FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington 98055–4056; telephone (425) 227–2125; fax (425) 227–1149. FOR FURTHER INFORMATION CONTACT: On September 6, 2005, the FAA issued AD 2005–19–04, amendment 39–14269 (70 FR 54251, September 14, 2005), for certain Airbus Model A340–200 and –300 series airplanes. The AD requires revising the airplane flight manual to incorporate new procedures for the flightcrew to follow to correct miscalculation of the takeoff and accelerating or stopping distance of the airplane during a ferry flight under certain conditions. As published, that AD specifies an incorrect Docket No. (i.e., FAA–2005– 20405) throughout preamble and the regulatory text of the AD. The correct Docket No. is FAA–2005–22405. 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 September 29, 2005. SUPPLEMENTARY INFORMATION: § 39.13 [Corrected] I In the Federal Register of September 14, 2005, on page 54253, in the first column, paragraph 2. of PART 39— AIRWORTHINESS DIRECTIVES of AD 2005–19–04 is corrected to read as follows: * * * * * 2005–19–04 Airbus: Amendment 39–14269. Docket No. FAA–2005–22405; Directorate Identifier 2002–NM–243–AD. * * * * * Issued in Renton, Washington, on September 26, 2005. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 05–19556 Filed 9–29–05; 8:45 am] BILLING CODE 4910–13–P E:\FR\FM\30SER1.SGM 30SER1

Agencies

[Federal Register Volume 70, Number 189 (Friday, September 30, 2005)]
[Rules and Regulations]
[Page 57125]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-19556]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2005-22405; Directorate Identifier 2002-NM-243-AD; 
Amendment 39-14269; AD 2005-19-04]
RIN 2120-AA64


Airworthiness Directives; Airbus Model A340-200 and -300 Series 
Airplanes

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

ACTION: Final rule; correction.

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SUMMARY: The FAA is correcting a typographical error in an existing 
airworthiness directive (AD) that was published in the Federal Register 
on September 14, 2005 (70 FR 54251). The error resulted in in an 
incorrect Docket No. This AD applies to certain Airbus Model A340-200 
and -300 series airplanes. This AD requires revising the airplane 
flight manual to incorporate new procedures for the flightcrew to 
follow to correct miscalculation of the takeoff and accelerating or 
stopping distance of the airplane during a ferry flight under certain 
conditions.

DATES: Effective September 29, 2005.

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-2005-22405; the directorate 
identifier for this docket is 2002-NM-243-AD.

FOR FURTHER INFORMATION CONTACT: Dan Rodina, Aerospace Engineer, 
International Branch, ANM-116, FAA, Transport Airplane Directorate, 
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 
227-2125; fax (425) 227-1149.

SUPPLEMENTARY INFORMATION: On September 6, 2005, the FAA issued AD 
2005-19-04, amendment 39-14269 (70 FR 54251, September 14, 2005), for 
certain Airbus Model A340-200 and -300 series airplanes. The AD 
requires revising the airplane flight manual to incorporate new 
procedures for the flightcrew to follow to correct miscalculation of 
the takeoff and accelerating or stopping distance of the airplane 
during a ferry flight under certain conditions.
    As published, that AD specifies an incorrect Docket No. (i.e., FAA-
2005-20405) throughout preamble and the regulatory text of the AD. The 
correct Docket No. is FAA-2005-22405.
    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 September 29, 2005.


Sec.  39.13  [Corrected]

0
In the Federal Register of September 14, 2005, on page 54253, in the 
first column, paragraph 2. of PART 39--AIRWORTHINESS DIRECTIVES of AD 
2005-19-04 is corrected to read as follows:
* * * * *
2005-19-04 Airbus: Amendment 39-14269. Docket No. FAA-2005-22405; 
Directorate Identifier 2002-NM-243-AD.
* * * * *

    Issued in Renton, Washington, on September 26, 2005.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 05-19556 Filed 9-29-05; 8:45 am]
BILLING CODE 4910-13-P