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