Airworthiness Directives; British Aerospace Model HS 748 Airplanes, 55234-55236 [05-18521]
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55234
Federal Register / Vol. 70, No. 182 / Wednesday, September 21, 2005 / Rules and Regulations
Material Incorporated by Reference
(i) You must use Airbus Service Bulletin
A320–28–1067, Revision 02, dated January
27, 1997, to perform the actions that are
required by this AD, unless the AD specifies
otherwise. The Director of the Federal
Register approved the incorporation by
reference of this document in accordance
with 5 U.S.C. 552(a) and 1 CFR part 51.
Contact Airbus, 1 Rond Point Maurice
Bellonte, 31707 Blagnac Cedex, France, 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 tohttps://www.archives.gov/
federal_register/code_of_federal_regulations/
ibr_locations.html.
Unsafe Condition
(d) This AD results from fuel system
reviews conducted by the manufacturer. We
are issuing this AD to prevent an ignition
source for fuel vapor in the wing, which
could result in fire or explosion in the
adjacent wing fuel tank.
[Docket No. FAA–2005–22453; Directorate
Identifier 2002–NM–139–AD; Amendment
39–14278; AD 2005–19–13]
of a certain publication listed in the AD
as of October 6, 2005.
We must receive comments on this
AD by November 21, 2005.
ADDRESSES: Use one of the following
addresses to submit comments on this
AD.
• DOT Docket Web site: Go to
https://dms.dot.gov and follow the
instructions for sending your comments
electronically.
• Government-wide rulemaking Web
site: Go to https://www.regulations.gov
and follow the instructions for sending
your comments electronically.
• Mail: Docket Management Facility;
U.S. Department of Transportation, 400
Seventh Street SW., Nassif Building,
Room PL–401, Washington, DC 20590.
• Fax: (202) 493–2251.
• Hand Delivery: Room PL–401 on
the plaza level of the Nassif Building,
400 Seventh Street SW., Washington,
DC, between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
Contact British Aerospace Regional
Aircraft American Support, 13850
Mclearen Road, Herndon, Virginia
20171, for service information identified
in this AD.
FOR FURTHER INFORMATION CONTACT:
Todd Thompson, Aerospace Engineer,
International Branch, ANM–116, FAA,
Transport Airplane Directorate, 1601
Lind Avenue, SW., Renton, Washington
98055–4056; telephone (425) 227–1175;
fax (425) 227–1149.
SUPPLEMENTARY INFORMATION:
RIN 2120–AA64
Discussion
Airworthiness Directives; British
Aerospace Model HS 748 Airplanes
Compliance
(e) You are responsible for having the
actions required by this AD performed within
the compliance times specified, unless the
actions have already been done.
AGENCY:
The Civil Aviation Authority (CAA),
which is the airworthiness authority for
the United Kingdom, notified us that an
unsafe condition may exist on all British
Aerospace Model HS 748 Airplanes.
The CAA advises that failure to follow
the airplane’s maintenance manual
instructions for installing the nose
landing gear (NLG) could result in
incorrect assembly of the NLG. Incorrect
assembly may result in the pintle pin
being unlocked, so that it is free to
migrate from its support housing. It is
possible to install the pintle pin in an
incorrect configuration without any
knowledge or suspicion that the pin was
installed incorrectly. Incorrect assembly
of the pin, if not corrected, could result
in jamming or collapse of the NLG,
which could result in damage to the
airplane structure or injury to
passengers or crew.
Adoption of the Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
I
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
I
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The Federal Aviation
Administration (FAA) amends § 39.13
by adding the following new
airworthiness directive (AD):
I
2005–19–16 Airbus: Amendment 39–14281.
Docket No. FAA–2005–21861;
Directorate Identifier 2005–NM–093–AD.
Effective Date
(a) This AD becomes effective October 26,
2005.
Affected ADs
(b) None.
BILLING CODE 4910–13–P
Applicability
(c) This AD applies to Airbus Model A320–
111, –211, –212, –214, –231, –232, and –233
airplanes, certificated in any category; except
those airplanes on which Airbus
Modification 25513 has been accomplished
in production.
Installation of Bonding Strips
(f) Within 56 months after the effective
date of this AD, install a bonding strip
between each of the two water scavenge jet
pumps of the center fuel tank and the rear
spar in section 21, in accordance with the
Accomplishment Instructions of Airbus
Service Bulletin A320–28–1067, Revision 02,
dated January 27, 1997.
Alternative Methods of Compliance
(AMOCs)
(g) The Manager, International Branch,
ANM–116, Transport Airplane Directorate,
FAA, has the authority to approve AMOCs
for this AD, if requested in accordance with
the procedures found in 14 CFR 39.19.
Related Information
(h) French airworthiness directive F–2005–
056, dated April 13, 2005, also addresses the
subject of this AD.
VerDate Aug<31>2005
Issued in Renton, Washington, on
September 9, 2005.
Kalene C. Yanamura,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. 05–18520 Filed 9–20–05; 8:45 am]
14:27 Sep 20, 2005
Jkt 205001
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; request for
comments.
SUMMARY: The FAA is adopting a new
airworthiness directive (AD) for all
British Aerospace Model HS 748
airplanes. This AD requires modifying
the undercarriage of the nose landing
gear (NLG). This AD results from a
report that pintle pins could be installed
in an incorrect manner during
maintenance without maintenance
personnel being aware (or having
feedback) that the pin was installed
incorrectly. We are issuing this AD to
prevent jamming or collapse of the NLG,
which could result in damage to the
airplane structure or injury to
passengers or crew.
DATES: Effective October 6, 2005.
The Director of the Federal Register
approved the incorporation by reference
PO 00000
Frm 00010
Fmt 4700
Sfmt 4700
Relevant Service Information
British Aerospace has issued BAE
Systems (Operations) Limited Service
Bulletin HS748–32–104, dated April 9,
2002. The service bulletin describes
E:\FR\FM\21SER1.SGM
21SER1
Federal Register / Vol. 70, No. 182 / Wednesday, September 21, 2005 / Rules and Regulations
procedures for modifying the NLG
undercarriage. Modifying the NLG
undercarriage involves installing an
additional baulking device by installing
a location pin, lanyard, and a NLG that
has had the actions of Dowty Service
Bulletin 32–108E done on it.
Accomplishing the actions specified in
the service information is intended to
adequately address the unsafe
condition. The CAA issued British
airworthiness directive 003–04–2002, to
ensure the continued airworthiness of
these airplanes in the United Kingdom.
FAA’s Determination and Requirements
of This AD
This airplane model is manufactured
in the United Kingdom and is type
certificated for operation in the United
States under the provisions of section
21.29 of the Federal Aviation
Regulations (14 CFR 21.29) and the
applicable bilateral airworthiness
agreement. Pursuant to this bilateral
airworthiness agreement, the CAA has
kept the FAA informed of the situation
described above. We have examined the
CAA’s findings, evaluated all pertinent
information, and determined that we
need to issue an AD for products of this
type design that are certificated for
operation in the United States.
Therefore, we are issuing this AD to
prevent jamming or collapse of the NLG,
which could result in damage to the
airplane structure or injury to
passengers or crew. This AD requires
accomplishing the actions specified in
the service information described
previously.
Costs of Compliance
None of the airplanes affected by this
action are on the U.S. Register. All
airplanes affected by this AD are
currently operated by non-U.S.
operators under foreign registry;
therefore, they are not directly affected
by this AD action. However, we
consider this AD necessary to ensure
that the unsafe condition is addressed if
any affected airplane is imported and
placed on the U.S. Register in the future.
If an affected airplane is imported and
placed on the U.S. Register in the future,
the required actions would take about
20 work hours per airplane, at an
average labor rate of $65 per work hour.
Based on these figures, the estimated
cost of the AD would be $1,300 per
airplane.
FAA’s Determination of the Effective
Date
No airplane affected by this AD is
currently on the U.S. Register.
Therefore, providing notice and
opportunity for public comment is
VerDate Aug<31>2005
14:27 Sep 20, 2005
Jkt 205001
unnecessary before this AD is issued,
and this AD may be made effective in
less than 30 days after it is published in
the Federal Register.
Comments Invited
This AD is a final rule that involves
requirements that affect flight safety and
was not preceded by notice and an
opportunity for public comment;
however, we invite you to submit any
relevant written data, views, or
arguments regarding this AD. Send your
comments to the address listed under
the ADDRESSES section. Include ‘‘Docket
No. FAA–2005–22453; Directorate
Identifier 2002–NM–139–AD’’ at the
beginning of your comments. We
specifically invite comments on the
overall regulatory, economic,
environmental, and energy aspects of
the AD that might suggest a need to
modify it.
We will post all comments we
receive, without change, to https://
dms.dot.gov, including any personal
information you provide. We will also
post a report summarizing each
substantive verbal contact with FAA
personnel concerning this AD. Using the
search function of that Web site, anyone
can find and read the comments in any
of our dockets, including the name of
the individual who sent the comment
(or signed the comment on behalf of an
association, business, labor union, etc.).
You may review the DOT’s complete
Privacy Act Statement in the Federal
Register published on April 11, 2000
(65 FR 19477–78), or you may visit
https://dms.dot.gov.
55235
‘‘General requirements.’’ Under that
section, Congress charges the FAA with
promoting safe flight of civil aircraft in
air commerce by prescribing regulations
for practices, methods, and procedures
the Administrator finds necessary for
safety in air commerce. This regulation
is within the scope of that authority
because it addresses an unsafe condition
that is likely to exist or develop on
products identified in this rulemaking
action.
Regulatory Findings
We have determined that this AD will
not have federalism implications under
Executive Order 13132. This AD will
not have a substantial direct effect on
the States, on the relationship between
the National Government and the States,
or on the distribution of power and
responsibilities among the various
levels of government.
For the reasons discussed above, I
certify that the regulation:
1. Is not a ‘‘significant regulatory
action’’ under Executive Order 12866;
2. Is not a ‘‘significant rule’’ under the
DOT Regulatory Policies and Procedures
(44 FR 11034, February 26, 1979); and
3. Will not have a significant
economic impact, positive or negative,
on a substantial number of small entities
under the criteria of the Regulatory
Flexibility Act.
We prepared a regulatory evaluation
of the estimated costs to comply with
this AD and placed it in the AD docket.
See the ADDRESSES section for a location
to examine the regulatory evaluation.
List of Subjects in 14 CFR Part 39
Examining the Docket
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 DOT
street address stated in the ADDRESSES
section. Comments will be available in
the AD docket shortly after the Docket
Management System receives them.
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
Authority for This Rulemaking
Title 49 of the United States Code
specifies the FAA’s authority to issue
rules on aviation safety. Subtitle I,
section 106, describes the authority of
the FAA Administrator. Subtitle VII,
Aviation Programs, describes in more
detail the scope of the Agency’s
authority.
We are issuing this rulemaking under
the authority described in subtitle VII,
part A, subpart III, section 44701,
Authority: 49 U.S.C. 106(g), 40113, 44701.
PO 00000
Frm 00011
Fmt 4700
Sfmt 4700
Adoption of the Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
I
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
I
§ 39.13
[Amended]
2. The Federal Aviation
Administration (FAA) amends § 39.13
by adding the following new
airworthiness directive (AD):
I
2005–19–13 BAE Systems (Operations)
Limited (Formerly British Aerospace
Regional Aircraft): Amendment 39–
14278. Docket No. FAA–2005–22453;
Directorate Identifier 2002–NM–139–AD.
E:\FR\FM\21SER1.SGM
21SER1
55236
Federal Register / Vol. 70, No. 182 / Wednesday, September 21, 2005 / Rules and Regulations
Effective Date
Issued in Renton, Washington, on
September 9, 2005.
Kalene C. Yanamura,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. 05–18521 Filed 9–20–05; 8:45 am]
(a) This AD becomes effective October 6,
2005.
Affected ADs
(b) None.
Applicability
BILLING CODE 4910–13–P
(c) This AD applies to all BAE Systems
(Operations) Limited Model HS 748 series 2A
and series 2B airplanes, certificated in any
category.
DEPARTMENT OF TRANSPORTATION
Unsafe Condition
(d) This AD results from a report that
pintle pins could be installed in an incorrect
manner during maintenance without
maintenance personnel being aware (or
having feedback) that the pin was installed
incorrectly. The FAA is issuing this AD to
prevent jamming or collapse of the nose
landing gear (NLG), which could result in
damage to the airplane structure or injury to
passengers or crew.
Compliance
(e) You are responsible for having the
actions required by this AD performed within
the compliance times specified, unless the
actions have already been done.
Modifying the Undercarriage of the Nose
Landing Gear
(f) Within 64 months after the effective
date of this AD, modify the undercarriage of
the NLG in accordance with the
Accomplishment Instructions of BAE
Systems (Operations) Limited Service
Bulletin HS748–32–104, dated April 9, 2002.
Alternative Methods of Compliance
(AMOCs)
(g) The Manager, International Branch,
ANM–116, Transport Airplane Directorate,
FAA, has the authority to approve AMOCs
for this AD, if requested in accordance with
the procedures found in 14 CFR 39.19.
Related Information
(h) British airworthiness directive 003–04–
2002 also addresses the subject of this AD.
Material Incorporated by Reference
(i) You must use BAE Systems (Operations)
Limited Service Bulletin HS748–32–104,
dated April 9, 2002, to perform the actions
that are required by this AD, unless the AD
specifies otherwise. The Director of the
Federal Register approved the incorporation
by reference of this document in accordance
with 5 U.S.C. 552(a) and 1 CFR part 51.
Contact British Aerospace Regional Aircraft
American Support, 13850 Mclearen Road,
Herndon, Virginia 20171, 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.
VerDate Aug<31>2005
14:27 Sep 20, 2005
Jkt 205001
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2005–22452; Directorate
Identifier 2001–NM–336–AD; Amendment
39–14277; AD 2005–19–12]
RIN 2120–AA64
Airworthiness Directives; Airbus Model
A330–301, –321, –322, –341, and –342
Airplanes; and Model A340–200 and
A340–300 Series Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; request for
comments.
AGENCY:
SUMMARY: The FAA is adopting a new
airworthiness directive (AD) for certain
Airbus Model A330–301, –321, –322,
–341, and –342 airplanes; and Model
A340–200 and A340–300 series
airplanes. This AD requires repetitive
inspections for cracks of the inboard
lower flange and radius of the left- and
right-hand outboard floor beams at
frame (FR) 48, and related investigative
and corrective actions if necessary. This
AD also provides an optional
terminating action for the repetitive
inspections. This AD results from
reports that cracks were found during
fatigue tests at the attachment between
the canted lower flange of the floor
beam and the pressure diaphragm in
front of FR48 on both left- and righthand floor beams; and that an additional
crack was found in the flange radius of
the floor beam. We are issuing this AD
to detect and correct such cracking,
which could propagate and result in
reduced structural integrity of the
fuselage.
Effective October 6, 2005.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in the AD
as of October 6, 2005.
We must receive comments on this
AD by November 21, 2005.
ADDRESSES: Use one of the following
addresses to submit comments on this
AD.
• DOT Docket Web site: Go to https://
dms.dot.gov and follow the instructions
DATES:
PO 00000
Frm 00012
Fmt 4700
Sfmt 4700
for sending your comments
electronically.
• Government-wide rulemaking Web
site: Go to https://www.regulations.gov
and follow the instructions for sending
your comments electronically.
• Mail: Docket Management Facility;
U.S. Department of Transportation, 400
Seventh Street SW., Nassif Building,
Room PL–401, Washington, DC 20590.
• Fax: (202) 493–2251.
• Hand Delivery: Room PL–401 on
the plaza level of the Nassif Building,
400 Seventh Street SW., Washington,
DC, between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
Contact Airbus, 1 Rond Point Maurice
Bellonte, 31707 Blagnac Cedex, France,
for service information identified in this
AD.
You may examine the contents of the
AD docket on the Internet at https://
dms.dot.gov, or in person at the Docket
Management Facility, U.S. Department
of Transportation, 400 Seventh Street
SW., Room PL–401, Washington, DC.
This docket number is FAA–2005–
22452; the directorate identifier for this
docket is 2001–NM–336–AD.
FOR FURTHER INFORMATION CONTACT: Tim
Backman, Aerospace Engineer, ANM–
116, International Branch, FAA,
Transport Airplane Directorate, 1601
Lind Avenue, SW., Renton, Washington
98055–4056; telephone (425) 227–2797;
fax (425) 227–1149.
SUPPLEMENTARY INFORMATION:
Comments Invited
Although this is a final rule that was
not preceded by notice and an
opportunity for public comment, we
invite you to submit any relevant
written data, views, or arguments
regarding this AD. Include ‘‘Docket No.
FAA–2005–22452; Directorate Identifier
2001–NM–336–AD’’ at the beginning of
your comments. We specifically invite
comments on the overall regulatory,
economic, environmental, and energy
aspects of the AD. We will consider all
comments received by the closing date
and may amend the AD in light of those
comments.
We will post all comments we
receive, without change, to https://
dms.dot.gov, including any personal
information you provide. We will also
post a report summarizing each
substantive verbal contact with FAA
personnel concerning this AD. Using the
search function of that Web site, anyone
can find and read the comments in any
of our dockets, including the name of
the individual who sent the comment
(or signed the comment on behalf of an
association, business, labor union, etc.).
You may review the DOT’s complete
E:\FR\FM\21SER1.SGM
21SER1
Agencies
[Federal Register Volume 70, Number 182 (Wednesday, September 21, 2005)]
[Rules and Regulations]
[Pages 55234-55236]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-18521]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-22453; Directorate Identifier 2002-NM-139-AD;
Amendment 39-14278; AD 2005-19-13]
RIN 2120-AA64
Airworthiness Directives; British Aerospace Model HS 748
Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; request for comments.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all
British Aerospace Model HS 748 airplanes. This AD requires modifying
the undercarriage of the nose landing gear (NLG). This AD results from
a report that pintle pins could be installed in an incorrect manner
during maintenance without maintenance personnel being aware (or having
feedback) that the pin was installed incorrectly. We are issuing this
AD to prevent jamming or collapse of the NLG, which could result in
damage to the airplane structure or injury to passengers or crew.
DATES: Effective October 6, 2005.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in the AD as of October 6,
2005.
We must receive comments on this AD by November 21, 2005.
ADDRESSES: Use one of the following addresses to submit comments on
this AD.
DOT Docket Web site: Go to https://dms.dot.gov and follow
the instructions for sending your comments electronically.
Government-wide rulemaking Web site: Go to https://
www.regulations.gov and follow the instructions for sending your
comments electronically.
Mail: Docket Management Facility; U.S. Department of
Transportation, 400 Seventh Street SW., Nassif Building, Room PL-401,
Washington, DC 20590.
Fax: (202) 493-2251.
Hand Delivery: Room PL-401 on the plaza level of the
Nassif Building, 400 Seventh Street SW., Washington, DC, between 9 a.m.
and 5 p.m., Monday through Friday, except Federal holidays.
Contact British Aerospace Regional Aircraft American Support, 13850
Mclearen Road, Herndon, Virginia 20171, for service information
identified in this AD.
FOR FURTHER INFORMATION CONTACT: Todd Thompson, Aerospace Engineer,
International Branch, ANM-116, FAA, Transport Airplane Directorate,
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425)
227-1175; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION:
Discussion
The Civil Aviation Authority (CAA), which is the airworthiness
authority for the United Kingdom, notified us that an unsafe condition
may exist on all British Aerospace Model HS 748 Airplanes. The CAA
advises that failure to follow the airplane's maintenance manual
instructions for installing the nose landing gear (NLG) could result in
incorrect assembly of the NLG. Incorrect assembly may result in the
pintle pin being unlocked, so that it is free to migrate from its
support housing. It is possible to install the pintle pin in an
incorrect configuration without any knowledge or suspicion that the pin
was installed incorrectly. Incorrect assembly of the pin, if not
corrected, could result in jamming or collapse of the NLG, which could
result in damage to the airplane structure or injury to passengers or
crew.
Relevant Service Information
British Aerospace has issued BAE Systems (Operations) Limited
Service Bulletin HS748-32-104, dated April 9, 2002. The service
bulletin describes
[[Page 55235]]
procedures for modifying the NLG undercarriage. Modifying the NLG
undercarriage involves installing an additional baulking device by
installing a location pin, lanyard, and a NLG that has had the actions
of Dowty Service Bulletin 32-108E done on it. Accomplishing the actions
specified in the service information is intended to adequately address
the unsafe condition. The CAA issued British airworthiness directive
003-04-2002, to ensure the continued airworthiness of these airplanes
in the United Kingdom.
FAA's Determination and Requirements of This AD
This airplane model is manufactured in the United Kingdom and is
type certificated for operation in the United States under the
provisions of section 21.29 of the Federal Aviation Regulations (14 CFR
21.29) and the applicable bilateral airworthiness agreement. Pursuant
to this bilateral airworthiness agreement, the CAA has kept the FAA
informed of the situation described above. We have examined the CAA's
findings, evaluated all pertinent information, and determined that we
need to issue an AD for products of this type design that are
certificated for operation in the United States.
Therefore, we are issuing this AD to prevent jamming or collapse of
the NLG, which could result in damage to the airplane structure or
injury to passengers or crew. This AD requires accomplishing the
actions specified in the service information described previously.
Costs of Compliance
None of the airplanes affected by this action are on the U.S.
Register. All airplanes affected by this AD are currently operated by
non-U.S. operators under foreign registry; therefore, they are not
directly affected by this AD action. However, we consider this AD
necessary to ensure that the unsafe condition is addressed if any
affected airplane is imported and placed on the U.S. Register in the
future.
If an affected airplane is imported and placed on the U.S. Register
in the future, the required actions would take about 20 work hours per
airplane, at an average labor rate of $65 per work hour. Based on these
figures, the estimated cost of the AD would be $1,300 per airplane.
FAA's Determination of the Effective Date
No airplane affected by this AD is currently on the U.S. Register.
Therefore, providing notice and opportunity for public comment is
unnecessary before this AD is issued, and this AD may be made effective
in less than 30 days after it is published in the Federal Register.
Comments Invited
This AD is a final rule that involves requirements that affect
flight safety and was not preceded by notice and an opportunity for
public comment; however, we invite you to submit any relevant written
data, views, or arguments regarding this AD. Send your comments to the
address listed under the ADDRESSES section. Include ``Docket No. FAA-
2005-22453; Directorate Identifier 2002-NM-139-AD'' at the beginning of
your comments. We specifically invite comments on the overall
regulatory, economic, environmental, and energy aspects of the AD that
might suggest a need to modify it.
We will post all comments we receive, without change, to https://
dms.dot.gov, including any personal information you provide. We will
also post a report summarizing each substantive verbal contact with FAA
personnel concerning this AD. Using the search function of that Web
site, anyone can find and read the comments in any of our dockets,
including the name of the individual who sent the comment (or signed
the comment on behalf of an association, business, labor union, etc.).
You may review the DOT's complete Privacy Act Statement in the Federal
Register published on April 11, 2000 (65 FR 19477-78), or you may visit
https://dms.dot.gov.
Examining the Docket
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 DOT
street address stated in the ADDRESSES section. Comments will be
available in the AD docket shortly after the Docket Management System
receives them.
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. Subtitle VII, Aviation Programs,
describes in more detail the scope of the Agency's authority.
We are issuing this rulemaking under the authority described in
subtitle VII, part A, subpart III, section 44701, ``General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.
Regulatory Findings
We have determined that this AD will not have federalism
implications under Executive Order 13132. This AD will not have a
substantial direct effect on the States, on the relationship between
the National Government and the States, or on the distribution of power
and responsibilities among the various levels of government.
For the reasons discussed above, I certify that the regulation:
1. Is not a ``significant regulatory action'' under Executive Order
12866;
2. Is not a ``significant rule'' under the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979); and
3. Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
We prepared a regulatory evaluation of the estimated costs to
comply with this AD and placed it in the AD docket. See the ADDRESSES
section for a location to examine the regulatory evaluation.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
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Accordingly, under the authority delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
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1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
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2. The Federal Aviation Administration (FAA) amends Sec. 39.13 by
adding the following new airworthiness directive (AD):
2005-19-13 BAE Systems (Operations) Limited (Formerly British
Aerospace Regional Aircraft): Amendment 39-14278. Docket No. FAA-
2005-22453; Directorate Identifier 2002-NM-139-AD.
[[Page 55236]]
Effective Date
(a) This AD becomes effective October 6, 2005.
Affected ADs
(b) None.
Applicability
(c) This AD applies to all BAE Systems (Operations) Limited
Model HS 748 series 2A and series 2B airplanes, certificated in any
category.
Unsafe Condition
(d) This AD results from a report that pintle pins could be
installed in an incorrect manner during maintenance without
maintenance personnel being aware (or having feedback) that the pin
was installed incorrectly. The FAA is issuing this AD to prevent
jamming or collapse of the nose landing gear (NLG), which could
result in damage to the airplane structure or injury to passengers
or crew.
Compliance
(e) You are responsible for having the actions required by this
AD performed within the compliance times specified, unless the
actions have already been done.
Modifying the Undercarriage of the Nose Landing Gear
(f) Within 64 months after the effective date of this AD, modify
the undercarriage of the NLG in accordance with the Accomplishment
Instructions of BAE Systems (Operations) Limited Service Bulletin
HS748-32-104, dated April 9, 2002.
Alternative Methods of Compliance (AMOCs)
(g) The Manager, International Branch, ANM-116, Transport
Airplane Directorate, FAA, has the authority to approve AMOCs for
this AD, if requested in accordance with the procedures found in 14
CFR 39.19.
Related Information
(h) British airworthiness directive 003-04-2002 also addresses
the subject of this AD.
Material Incorporated by Reference
(i) You must use BAE Systems (Operations) Limited Service
Bulletin HS748-32-104, dated April 9, 2002, to perform the actions
that are required by this AD, unless the AD specifies otherwise. The
Director of the Federal Register approved the incorporation by
reference of this document in accordance with 5 U.S.C. 552(a) and 1
CFR part 51. Contact British Aerospace Regional Aircraft American
Support, 13850 Mclearen Road, Herndon, Virginia 20171, 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 September 9, 2005.
Kalene C. Yanamura,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 05-18521 Filed 9-20-05; 8:45 am]
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