Airworthiness Directives; Airbus Model A330, A340-200, and A340-300 Series Airplanes, 12119 [05-4824]
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Federal Register / Vol. 70, No. 47 / Friday, March 11, 2005 / Rules and Regulations
Material Incorporated by Reference
(j) You must use the applicable temporary
revision to the applicable Airbus airplane
flight manual specified in Table 3 of this AD
to perform the actions that are required by
this AD, unless the AD specifies otherwise.
The Director of the Federal Register approves
the incorporation by reference of those
documents in accordance with 5 U.S.C.
552(a) and 1 CFR part 51. For copies of the
service information, contact Airbus, 1 Rond
Point Maurice Bellonte, 31707 Blagnac
Cedex, France. For information on the
availability of this material at the National
Archives and Records Administration
(NARA), call (202) 741–6030, or go to http:/
/www.archives.gov/federal_register/
code_of_federal_regulations/
ibr_locations.html.
You may view the AD docket at the Docket
Management Facility, U.S. Department of
Transportation, 400 Seventh Street SW.,
room PL–401, Nassif Building, Washington,
DC.
TABLE 3.—MATERIAL INCORPORATED
BY REFERENCE
Airbus temporary
revision
6.01.03/08,
February
6.01.03/36,
February
dated
9, 2004.
dated
9, 2004.
AFM
A300–600 Flight Manual.
A310 Flight Manual.
Issued in Renton, Washington, on February
18, 2005.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 05–4070 Filed 3–10–05; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2003–NM–256–AD; Amendment
39–13968; AD 2005–03–12]
RIN 2120–AA64
Airworthiness Directives; Airbus Model
A330, A340–200, and A340–300 Series
Airplanes
Federal Aviation
Administration, DOT.
ACTION: Final rule; correction.
AGENCY:
17:11 Mar 10, 2005
Jkt 205001
DATES:
Effective March 21, 2005.
Tim
Backman, Aerospace Engineer,
International Branch, ANM–116, FAA,
Transport Airplane Directorate, 1601
Lind Avenue, SW., Renton, Washington
98055–4056; telephone (425) 227–2797;
fax (425) 227–1149.
SUPPLEMENTARY INFORMATION:
Airworthiness Directive (AD) 2005–03–
12, amendment 39–13968, applicable to
certain Airbus Model A330, A340–200,
and A340–300 series airplanes, was
published in the Federal Register on
February 14, 2005 (70 FR 7386). That
AD requires initial and repetitive
inspections of certain frame stiffeners to
detect cracking and replacement of any
cracked stiffener with a new, reinforced
stiffener. Replacement of the stiffener
constitutes terminating action for
certain inspections. That AD also
requires a one-time inspection of any
new, reinforced stiffener; and repair or
replacement of the new, reinforced
stiffener if any cracking is found during
the one-time inspection. That AD also
provides for an optional terminating
action for certain requirements of that
AD.
As published, that final rule
incorrectly specified the AD number in
a single location in the AD as ‘‘2005–
NM–03–12’’ instead of ‘‘2005–03–12.’’
Since no other part of the regulatory
information has been changed, the final
rule is not being republished in the
Federal Register.
The effective date of this AD remains
March 21, 2005.
FOR FURTHER INFORMATION CONTACT:
§ 39.13
SUMMARY: This document corrects a
typographical error that appeared in
airworthiness directive (AD) 2005–03–
12 that was published in the Federal
Register on February 14, 2005 (70 FR
7386). The typographical error resulted
in an incorrect AD number. This AD is
applicable to certain Airbus Model
A330, A340–200, and A340–300 series
VerDate jul<14>2003
airplanes. This AD requires initial and
repetitive inspections of certain frame
stiffeners to detect cracking and
replacement of any cracked stiffener
with a new, reinforced stiffener.
Replacement of the stiffener constitutes
terminating action for certain
inspections. This AD also requires a
one-time inspection of any new,
reinforced stiffener; and repair or
replacement of the new, reinforced
stiffener if any cracking is found during
the one-time inspection. This AD also
provides for an optional terminating
action for certain requirements of this
AD.
[Corrected]
I In the Federal Register of February 14,
2005, on page 7388, in the first column,
paragraph 2. of PART 39—
AIRWORTHINESS DIRECTIVES is
corrected to read as follows:
*
*
*
*
*
2005–03–12 Airbus: Amendment 39–13968.
Docket 2003–NM–256–AD.
*
PO 00000
*
Frm 00009
*
*
Fmt 4700
*
Sfmt 4700
12119
Issued in Renton, Washington, on February
28, 2005.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 05–4824 Filed 3–10–05; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2004–19446; Directorate
Identifier 2004–NM–130–AD; Amendment
39–13967; AD 2005–03–11]
RIN 2120–AA64
Airworthiness Directives; Boeing
Model 767–200 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
February 11, 2005 (70 FR 7174). The
error resulted in an incorrect AD
number. This AD applies to certain
Boeing Model 767 series airplanes. This
AD requires repetitive detailed and
eddy current inspections of the aft
pressure bulkhead for damage and
cracking, and repair if necessary. This
AD also requires one-time detailed and
high frequency eddy current inspections
of any ‘‘oil-can’’ located on the aft
pressure bulkhead, and related
corrective actions if necessary.
DATES: Effective March 18, 2005.
ADDRESSES: The AD docket contains the
proposed AD, comments, and any final
disposition. You can 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–2004–19446; the directorate
identifier for this docket is 2004–NM–
130–AD.
FOR FURTHER INFORMATION CONTACT:
Suzanne Masterson, Aerospace
Engineer, Airframe Branch, ANM–120S,
FAA, Seattle Aircraft Certification
Office, 1601 Lind Avenue, SW., Renton,
E:\FR\FM\11MRR1.SGM
11MRR1
]]>Agencies
[Federal Register Volume 70, Number 47 (Friday, March 11, 2005)]
[Rules and Regulations]
[Page 12119]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-4824]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2003-NM-256-AD; Amendment 39-13968; AD 2005-03-12]
RIN 2120-AA64
Airworthiness Directives; Airbus Model A330, A340-200, and A340-
300 Series Airplanes
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; correction.
-----------------------------------------------------------------------
SUMMARY: This document corrects a typographical error that appeared in
airworthiness directive (AD) 2005-03-12 that was published in the
Federal Register on February 14, 2005 (70 FR 7386). The typographical
error resulted in an incorrect AD number. This AD is applicable to
certain Airbus Model A330, A340-200, and A340-300 series airplanes.
This AD requires initial and repetitive inspections of certain frame
stiffeners to detect cracking and replacement of any cracked stiffener
with a new, reinforced stiffener. Replacement of the stiffener
constitutes terminating action for certain inspections. This AD also
requires a one-time inspection of any new, reinforced stiffener; and
repair or replacement of the new, reinforced stiffener if any cracking
is found during the one-time inspection. This AD also provides for an
optional terminating action for certain requirements of this AD.
DATES: Effective March 21, 2005.
FOR FURTHER INFORMATION CONTACT: Tim Backman, Aerospace Engineer,
International Branch, ANM-116, FAA, Transport Airplane Directorate,
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425)
227-2797; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION: Airworthiness Directive (AD) 2005-03-12,
amendment 39-13968, applicable to certain Airbus Model A330, A340-200,
and A340-300 series airplanes, was published in the Federal Register on
February 14, 2005 (70 FR 7386). That AD requires initial and repetitive
inspections of certain frame stiffeners to detect cracking and
replacement of any cracked stiffener with a new, reinforced stiffener.
Replacement of the stiffener constitutes terminating action for certain
inspections. That AD also requires a one-time inspection of any new,
reinforced stiffener; and repair or replacement of the new, reinforced
stiffener if any cracking is found during the one-time inspection. That
AD also provides for an optional terminating action for certain
requirements of that AD.
As published, that final rule incorrectly specified the AD number
in a single location in the AD as ``2005-NM-03-12'' instead of ``2005-
03-12.''
Since no other part of the regulatory information has been changed,
the final rule is not being republished in the Federal Register.
The effective date of this AD remains March 21, 2005.
Sec. 39.13 [Corrected]
0
In the Federal Register of February 14, 2005, on page 7388, in the
first column, paragraph 2. of PART 39--AIRWORTHINESS DIRECTIVES is
corrected to read as follows:
* * * * *
2005-03-12 Airbus: Amendment 39-13968. Docket 2003-NM-256-AD.
* * * * *
Issued in Renton, Washington, on February 28, 2005.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 05-4824 Filed 3-10-05; 8:45 am]
BILLING CODE 4910-13-P
