Airworthiness Directives; Boeing Model 767-200 and -300 Series Airplanes, 12119-12120 [05-4825]
Download as PDF
<![CDATA[
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
12120
Federal Register / Vol. 70, No. 47 / Friday, March 11, 2005 / Rules and Regulations
Washington 98055–4056; telephone
(425) 917–6441; fax (425) 917–6590.
SUPPLEMENTARY INFORMATION: On
January 31, 2005, the FAA issued AD
2005–03–11, amendment 39–13967 (70
FR 7174, February 11, 2005), for certain
Boeing Model 767 series airplanes. The
AD requires repetitive detailed and
eddy current inspections of the aft
pressure bulkhead for damage and
cracking, and repair if necessary. The
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.
As published, that final rule
incorrectly specified the AD number in
a single location in the AD as ‘‘2005–
NM–03–11’’ instead of ‘‘2005–03–11.’’
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
March 18, 2005.
§ 39.13
[Corrected]
In the Federal Register of February 11,
2005, on page 7175, in the first column,
paragraph 2. of PART 39—
AIRWORTHINESS DIRECTIVES is
corrected to read as follows:
*
*
*
*
*
I
2005–03–11 Boeing: Amendment 39–13967.
Docket No. FAA–2004–19446;
Directorate Identifier 2004–NM–130–AD.
*
*
*
*
*
Issued in Renton, Washington, on February
28, 2005.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 05–4825 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–2004–19530; Directorate
Identifier 2002–NM–274–AD; Amendment
39–14008; AD 2005–05–19]
RIN 2120–AA64
Airworthiness Directives; Boeing
Model 727 Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
SUMMARY: The FAA is superseding an
existing airworthiness directive (AD),
VerDate jul<14>2003
17:11 Mar 10, 2005
Jkt 205001
which applies to certain Boeing Model
727 airplanes. That AD currently
requires repetitive detailed inspections
to detect cracking, corrosion, and
existing stop-drilled repairs of cracking
in the upper chord of the rear spar of the
wing; and repair if necessary. This new
AD requires new repetitive inspections
to detect cracks, corrosion, minor
surface defects, and existing stop-drilled
repairs of cracks in the upper and lower
chords of the front and rear spars of the
wing; and repair if necessary. This AD
is prompted by our determination that
further rulemaking action is necessary
to require additional actions specified in
the referenced service bulletin. We are
issuing this AD to prevent structural
failure of the wing and fuel leaks in the
airplane due to stress corrosion cracking
of the wing spar chords.
DATES: This AD becomes effective April
15, 2005.
On December 18, 2002 (67 FR 71808,
December 3, 2002), the Director of the
Federal Register approved the
incorporation by reference of Boeing
Alert Service Bulletin 727–57A0145,
Revision 2, dated October 24, 2002.
ADDRESSES: For service information
identified in this AD, contact Boeing
Commercial Airplanes, P.O. Box 3707,
Seattle, Washington 98124–2207.
Docket: 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–2004–19530; the directorate
identifier for this docket is 2002–NM–
274–AD.
FOR FURTHER INFORMATION CONTACT:
Daniel F. Kutz, Aerospace Engineer,
Airframe Branch, ANM–120S, FAA,
Seattle Aircraft Certification Office,
1601 Lind Avenue, SW., Renton,
Washington 98055–4056; telephone
(425) 917–6456; fax (425) 917–6590.
SUPPLEMENTARY INFORMATION: The FAA
proposed to amend part 39 of the
Federal Aviation Regulations (14 CFR
Part 39) with an AD to supersede AD
2002–24–05, amendment 39–12970 (67
FR 71808, December 3, 2002). The
existing AD applies to certain Boeing
Model 727 airplanes. The proposed AD
was published in the Federal Register
on November 5, 2004 (69 FR 64506), to
PO 00000
Frm 00010
Fmt 4700
Sfmt 4700
require new repetitive inspections to
detect cracks, corrosion, minor surface
defects, and existing stop-drilled repairs
of cracks in the upper and lower chords
of the front and rear spars of the wing;
and repair if necessary.
Comments
We provided the public the
opportunity to participate in the
development of this AD. We have
considered the comment that has been
submitted on the proposed AD. The
commenter supports the proposed AD.
Explanation of Change to Model
Designation
We have revised the subject heading
of the existing AD to identify model
designations as published in the most
recent type certificate data sheet for the
affected models.
Changes to Delegation Authority
Boeing has received a Delegation
Option Authorization (DOA). We have
revised this final rule to delegate the
authority to approve an alternative
method of compliance for any repair
required by this AD to the Authorized
Representative for the Boeing DOA
Organization rather than the Designated
Engineering Representative (DER).
Conclusion
We have carefully reviewed the
available data, including the comment
that has been submitted, and
determined that air safety and the
public interest require adopting the AD
with the change described previously.
We have determined that this change
will neither increase the economic
burden on any operator nor increase the
scope of the AD.
Costs of Compliance
There are about 1,426 airplanes of the
affected design in the worldwide fleet.
This AD will affect about 946 airplanes
of U.S. registry.
For Group 1 airplanes identified in
the service bulletin, the actions (Part 1
of the Accomplishment Instructions of
the service bulletin) that are required by
AD 2002–24–05 and retained in this AD
take about 8 work hours per airplane, at
an average labor rate of $65 per work
hour. Based on these figures, the
estimated cost of the currently required
actions is $520 per airplane.
The following table provides the
estimated costs for U.S. operators to
comply with the new actions required
by this AD. The average labor rate is $65
per work hour.
E:\FR\FM\11MRR1.SGM
11MRR1
]]>Agencies
[Federal Register Volume 70, Number 47 (Friday, March 11, 2005)]
[Rules and Regulations]
[Pages 12119-12120]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-4825]
-----------------------------------------------------------------------
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
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 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,
[[Page 12120]]
Washington 98055-4056; telephone (425) 917-6441; fax (425) 917-6590.
SUPPLEMENTARY INFORMATION: On January 31, 2005, the FAA issued AD 2005-
03-11, amendment 39-13967 (70 FR 7174, February 11, 2005), for certain
Boeing Model 767 series airplanes. The AD requires repetitive detailed
and eddy current inspections of the aft pressure bulkhead for damage
and cracking, and repair if necessary. The 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.
As published, that final rule incorrectly specified the AD number
in a single location in the AD as ``2005-NM-03-11'' instead of ``2005-
03-11.''
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 March 18, 2005.
Sec. 39.13 [Corrected]
0
In the Federal Register of February 11, 2005, on page 7175, in the
first column, paragraph 2. of PART 39--AIRWORTHINESS DIRECTIVES is
corrected to read as follows:
* * * * *
2005-03-11 Boeing: Amendment 39-13967. Docket No. FAA-2004-19446;
Directorate Identifier 2004-NM-130-AD.
* * * * *
Issued in Renton, Washington, on February 28, 2005.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 05-4825 Filed 3-10-05; 8:45 am]
BILLING CODE 4910-13-P
