Airworthiness Directives; ATR Model ATR42-500 Airplanes, 6594-6595 [E8-2004]
Download as PDF
6594
Federal Register / Vol. 73, No. 24 / Tuesday, February 5, 2008 / Rules and Regulations
information on the availability of this
material at NARA, call 202–741–6030, or go
to: https://www.archives.gov/federal_register/
code_of_federal_regulations/
ibr_locations.html.
Issued in Kansas City, Missouri, on January
23, 2008.
John Colomy,
Acting Manager, Small Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E8–1829 Filed 2–4–08; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2008–0121; Directorate
Identifier 2007–NM–277–AD; Amendment
39–15363; AD 2008–03–13]
RIN 2120–AA64
Airworthiness Directives; ATR Model
ATR42–500 Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; request for
comments.
rmajette on PROD1PC64 with RULES
AGENCY:
SUMMARY: The FAA is adopting a new
airworthiness directive (AD) for certain
ATR Model ATR42–500 series
airplanes. This AD requires removing
metallized polyethylene terephtalate
(MPET) insulation blankets installed on
the left and the right sides of the
airplane over frame 24 between stringers
5 and 14. This AD results from reports
indicating that burnt spots were found
on the MPET insulation blankets
installed over frame 24. The actions
specified by this AD are intended to
ensure that MPET insulation blankets
are removed over frame 24. Such MPET
insulation blankets, if not removed,
could propagate a small fire that is the
result of an electrical arc and could lead
to a much larger fire.
DATES: This AD becomes effective
February 20, 2008.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in the AD
as of February 20, 2008.
We must receive comments on this
AD by March 6, 2008.
ADDRESSES: You may send comments by
any of the following methods:
• Federal eRulemaking Portal: Go to
https://www.regulations.gov. Follow the
instructions for submitting comments.
• Fax: 202–493–2251.
• Mail: U.S. Department of
Transportation, Docket Operations, M–
VerDate Aug<31>2005
15:28 Feb 04, 2008
Jkt 214001
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue, SE.,
Washington, DC 20590.
• Hand Delivery: U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue, SE.,
Washington, DC 20590, between 9 a.m.
and 5 p.m., Monday through Friday,
except Federal holidays.
For service information identified in
this AD, contact ATR, 316 Route de
Bayonne, 31060 Toulouse, Cedex 03,
France.
Examining the AD Docket
You may examine the AD docket on
the Internet at https://
www.regulations.gov; or in person at the
Docket Management Facility between 9
a.m. and 5 p.m., Monday through
Friday, except Federal holidays. The AD
docket contains this AD, the regulatory
evaluation, any comments received, and
other information. The street address for
the Docket Office (telephone 800–647–
5527) is in the ADDRESSES section.
Comments will be available in the AD
docket shortly after receipt.
FOR FURTHER INFORMATION CONTACT: Tom
Rodriguez, Aerospace Engineer,
International Branch, ANM–116,
Transport Airplane Directorate, FAA,
1601 Lind Avenue, SW., Renton,
Washington 98057–3356; telephone
(425) 227–1137; fax (425) 227–1149.
SUPPLEMENTARY INFORMATION:
Discussion
The European Aviation Safety Agency
(EASA), which is the Technical Agent
for the Member States of the European
Community, notified us that an unsafe
condition may exist on certain ATR
Model ATR42–500 series airplanes. The
EASA advises that there have been
reports of two in-service aircraft where
burnt spots were found on the
insulation blankets installed over frame
24. Investigations concluded that due to
the presence of the bleed air duct,
installation of the thermal-acoustical
insulation blankets having a metallized
polyethylene terephtalate (MPET) made
the covering (also known as Mylar TM) at
this location unsafe. Such MPET
insulation blankets, if not removed,
could propagate a small fire that is the
result of an electrical arc and could lead
to a much larger fire. This action is
intended to address the identified
unsafe condition.
Relevant Service Information
ATR has issued Service Bulletin
ATR42–25–0155, dated April 10, 2007.
The service bulletin describes
procedures for removing the MPET
insulation blankets installed on the left
PO 00000
Frm 00018
Fmt 4700
Sfmt 4700
and the right sides of the airplane over
frame 24 between stringers 5 and 14.
Accomplishing the actions specified in
the service information is intended to
adequately address the unsafe
condition. The EASA mandated the
service information and issued
emergency airworthiness directive
2007–0106–E, dated April 18, 2007, to
ensure the continued airworthiness of
these airplanes in the European Union.
FAA’s Determination and Requirements
of This AD
These airplanes are manufactured in
France and are 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. As described
in FAA Order 8100.14A, ‘‘Interim
Procedures for Working with the
European Community on Airworthiness
Certification and Continued
Airworthiness,’’ dated August 12, 2005,
the EASA has kept the FAA informed of
the situation described above. We have
examined the EASA’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
ensure that MPET insulation blankets
are removed over frame 24. Such MPET
insulation blankets, if not removed,
could propagate a small fire that is the
result of an electrical arc and could lead
to a much larger fire. 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 action would take about 6
work hours per airplane, at an average
labor rate of $80 per work hour. Based
on these figures, the estimated cost of
the AD would be $480 per airplane.
FAA’s Determination of the Effective
Date
No airplane affected by this AD is
currently on the U.S. Register.
E:\FR\FM\05FER1.SGM
05FER1
Federal Register / Vol. 73, No. 24 / Tuesday, February 5, 2008 / Rules and Regulations
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 affecting flight safety, and
we did not provide you with notice and
an opportunity to provide your
comments before it becomes effective.
However, we invite you to send any
written data, views, or arguments about
this AD. Send your comments to an
address listed under the ADDRESSES
section. Include ‘‘Docket No. FAA–
2008–0121; Directorate Identifier 2007–
NM–277–AD’’ at the beginning of your
comments. We specifically invite
comments on the overall regulatory,
economic, environmental, and energy
aspects of this AD. We will consider all
comments received by the closing date
and may amend this AD because of
those comments.
We will post all comments we
receive, without change, to https://
www.regulations.gov, including any
personal information you provide. We
will also post a report summarizing each
substantive verbal contact we receive
about this AD.
Authority for This Rulemaking
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
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.
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.
§ 39.13
2. The Federal Aviation
Administration (FAA) amends § 39.13
by adding the following new
airworthiness directive (AD):
I
2008–03–13 ATR—GIE Avions de
´
Transport Regional (Formerly
Aerospatiale): Amendment 39–15363.
Docket No. FAA–2008–0121; Directorate
Identifier 2007–NM–277–AD.
Effective Date
(a) This AD becomes effective February 20,
2008.
Affected ADs
(b) None.
rmajette on PROD1PC64 with RULES
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
Unsafe Condition
(d) This AD results from reports indicating
that burnt spots were found on the metallized
polyethylene terephtalate (MPET) insulation
blankets installed over frame 24. We are
issuing this AD to ensure that MPET
insulation blankets are removed over frame
15:28 Feb 04, 2008
Jkt 214001
PO 00000
Frm 00019
Fmt 4700
24. Such MPET insulation blankets, if not
removed, could propagate a small fire that is
the result of an electrical arc and could lead
to a much larger fire.
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.
Removal of Installation Blankets
(f) Within 15 days after the effective date
of this AD, remove the MPET insulation
blankets installed on the left and the right
sides of the airplane over frame 24 between
stringers 5 and 14, in accordance with the
Accomplishment Instructions of ATR Service
Bulletin ATR42–25–0155, dated April 10,
2007.
Alternative Methods of Compliance
(AMOCs)
(g)(1) 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.
(2) To request a different method of
compliance or a different compliance time
for this AD, follow the procedures in 14 CFR
39.19. Before using any approved AMOC on
any airplane to which the AMOC applies,
notify your appropriate principal inspector
(PI) in the FAA Flight Standards District
Office (FSDO), or lacking a PI, your local
FSDO.
Related Information
[Amended]
Applicability
(c) This AD applies to ATR Model ATR42–
500 series airplanes, certificated in any
category; except for airplanes modified in
accordance with ATR modification numbers
05117, 05322, and 05791, or ATR Service
Bulletin ATR42–25–1034, dated January 24,
2002.
VerDate Aug<31>2005
6595
Sfmt 4700
(h) EASA emergency airworthiness
directive 2007–0106–E, dated April 18, 2007,
also addresses the subject of this AD.
Material Incorporated by Reference
(i) You must use ATR Service Bulletin
ATR42–25–0155, dated April 10, 2007, 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 ATR, 316 Route de Bayonne,
31060 Toulouse, Cedex 03, France, for a copy
of this service information. You may review
copies at the FAA, Transport Airplane
Directorate, 1601 Lind Avenue SW., Renton,
Washington; or at the National Archives and
Records Administration (NARA).
For information on the availability of this
material at NARA, call 202–741–6030, or go
to: https://www.archives.gov/federal-register/
cfr/ibr-locations.html.
Issued in Renton, Washington, on January
24, 2008.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E8–2004 Filed 2–4–08; 8:45 am]
BILLING CODE 4910–13–P
E:\FR\FM\05FER1.SGM
05FER1
Agencies
[Federal Register Volume 73, Number 24 (Tuesday, February 5, 2008)]
[Rules and Regulations]
[Pages 6594-6595]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E8-2004]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2008-0121; Directorate Identifier 2007-NM-277-AD;
Amendment 39-15363; AD 2008-03-13]
RIN 2120-AA64
Airworthiness Directives; ATR Model ATR42-500 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
certain ATR Model ATR42-500 series airplanes. This AD requires removing
metallized polyethylene terephtalate (MPET) insulation blankets
installed on the left and the right sides of the airplane over frame 24
between stringers 5 and 14. This AD results from reports indicating
that burnt spots were found on the MPET insulation blankets installed
over frame 24. The actions specified by this AD are intended to ensure
that MPET insulation blankets are removed over frame 24. Such MPET
insulation blankets, if not removed, could propagate a small fire that
is the result of an electrical arc and could lead to a much larger
fire.
DATES: This AD becomes effective February 20, 2008.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in the AD as of February 20,
2008.
We must receive comments on this AD by March 6, 2008.
ADDRESSES: You may send comments by any of the following methods:
Federal eRulemaking Portal: Go to https://
www.regulations.gov. Follow the instructions for submitting comments.
Fax: 202-493-2251.
Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue, SE., Washington, DC 20590.
Hand Delivery: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue, SE., Washington, DC 20590, between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays.
For service information identified in this AD, contact ATR, 316
Route de Bayonne, 31060 Toulouse, Cedex 03, France.
Examining the AD Docket
You may examine the AD docket on the Internet at https://
www.regulations.gov; or in person at the Docket Management Facility
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The AD docket contains this AD, the regulatory evaluation,
any comments received, and other information. The street address for
the Docket Office (telephone 800-647-5527) is in the ADDRESSES section.
Comments will be available in the AD docket shortly after receipt.
FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aerospace Engineer,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425)
227-1137; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION:
Discussion
The European Aviation Safety Agency (EASA), which is the Technical
Agent for the Member States of the European Community, notified us that
an unsafe condition may exist on certain ATR Model ATR42-500 series
airplanes. The EASA advises that there have been reports of two in-
service aircraft where burnt spots were found on the insulation
blankets installed over frame 24. Investigations concluded that due to
the presence of the bleed air duct, installation of the thermal-
acoustical insulation blankets having a metallized polyethylene
terephtalate (MPET) made the covering (also known as Mylar \TM\) at
this location unsafe. Such MPET insulation blankets, if not removed,
could propagate a small fire that is the result of an electrical arc
and could lead to a much larger fire. This action is intended to
address the identified unsafe condition.
Relevant Service Information
ATR has issued Service Bulletin ATR42-25-0155, dated April 10,
2007. The service bulletin describes procedures for removing the MPET
insulation blankets installed on the left and the right sides of the
airplane over frame 24 between stringers 5 and 14. Accomplishing the
actions specified in the service information is intended to adequately
address the unsafe condition. The EASA mandated the service information
and issued emergency airworthiness directive 2007-0106-E, dated April
18, 2007, to ensure the continued airworthiness of these airplanes in
the European Union.
FAA's Determination and Requirements of This AD
These airplanes are manufactured in France and are 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. As described in FAA
Order 8100.14A, ``Interim Procedures for Working with the European
Community on Airworthiness Certification and Continued Airworthiness,''
dated August 12, 2005, the EASA has kept the FAA informed of the
situation described above. We have examined the EASA'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 ensure that MPET insulation
blankets are removed over frame 24. Such MPET insulation blankets, if
not removed, could propagate a small fire that is the result of an
electrical arc and could lead to a much larger fire. 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 action would take about 6 work hours per
airplane, at an average labor rate of $80 per work hour. Based on these
figures, the estimated cost of the AD would be $480 per airplane.
FAA's Determination of the Effective Date
No airplane affected by this AD is currently on the U.S. Register.
[[Page 6595]]
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 affecting flight
safety, and we did not provide you with notice and an opportunity to
provide your comments before it becomes effective. However, we invite
you to send any written data, views, or arguments about this AD. Send
your comments to an address listed under the ADDRESSES section. Include
``Docket No. FAA-2008-0121; Directorate Identifier 2007-NM-277-AD'' at
the beginning of your comments. We specifically invite comments on the
overall regulatory, economic, environmental, and energy aspects of this
AD. We will consider all comments received by the closing date and may
amend this AD because of those comments.
We will post all comments we receive, without change, to https://
www.regulations.gov, including any personal information you provide. We
will also post a report summarizing each substantive verbal contact we
receive about this AD.
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
0
Accordingly, under the authority delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
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]
0
2. The Federal Aviation Administration (FAA) amends Sec. 39.13 by
adding the following new airworthiness directive (AD):
2008-03-13 ATR--GIE Avions de Transport R[eacute]gional (Formerly
Aerospatiale): Amendment 39-15363. Docket No. FAA-2008-0121;
Directorate Identifier 2007-NM-277-AD.
Effective Date
(a) This AD becomes effective February 20, 2008.
Affected ADs
(b) None.
Applicability
(c) This AD applies to ATR Model ATR42-500 series airplanes,
certificated in any category; except for airplanes modified in
accordance with ATR modification numbers 05117, 05322, and 05791, or
ATR Service Bulletin ATR42-25-1034, dated January 24, 2002.
Unsafe Condition
(d) This AD results from reports indicating that burnt spots
were found on the metallized polyethylene terephtalate (MPET)
insulation blankets installed over frame 24. We are issuing this AD
to ensure that MPET insulation blankets are removed over frame 24.
Such MPET insulation blankets, if not removed, could propagate a
small fire that is the result of an electrical arc and could lead to
a much larger fire.
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.
Removal of Installation Blankets
(f) Within 15 days after the effective date of this AD, remove
the MPET insulation blankets installed on the left and the right
sides of the airplane over frame 24 between stringers 5 and 14, in
accordance with the Accomplishment Instructions of ATR Service
Bulletin ATR42-25-0155, dated April 10, 2007.
Alternative Methods of Compliance (AMOCs)
(g)(1) 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.
(2) To request a different method of compliance or a different
compliance time for this AD, follow the procedures in 14 CFR 39.19.
Before using any approved AMOC on any airplane to which the AMOC
applies, notify your appropriate principal inspector (PI) in the FAA
Flight Standards District Office (FSDO), or lacking a PI, your local
FSDO.
Related Information
(h) EASA emergency airworthiness directive 2007-0106-E, dated
April 18, 2007, also addresses the subject of this AD.
Material Incorporated by Reference
(i) You must use ATR Service Bulletin ATR42-25-0155, dated April
10, 2007, 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 ATR, 316
Route de Bayonne, 31060 Toulouse, Cedex 03, France, for a copy of
this service information. You may review copies at the FAA,
Transport Airplane Directorate, 1601 Lind Avenue SW., Renton,
Washington; or at the National Archives and Records Administration
(NARA).
For information on the availability of this material at NARA,
call 202-741-6030, or go to: https://www.archives.gov/federal-
register/cfr/ibr-locations.html.
Issued in Renton, Washington, on January 24, 2008.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E8-2004 Filed 2-4-08; 8:45 am]
BILLING CODE 4910-13-P