Airworthiness Directives; Gulfstream Aerospace LP Model Galaxy Airplanes and Model Gulfstream 200 Airplanes, 49170-49172 [E7-16655]
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<![CDATA[
49170
Federal Register / Vol. 72, No. 166 / Tuesday, August 28, 2007 / Rules and Regulations
ladders, or platforms may be required to gain
proximity to the area being checked.’’
DEPARTMENT OF TRANSPORTATION
Note 2: Boeing Alert Service Bulletin 737–
25A1363, Revision 2, dated May 2, 2006,
refers to IPECO Service Bulletin A001–25–47,
Issue 2, dated July 31, 2002, as an additional
source of service information for
accomplishment of the inspection and
rework required by paragraphs (f) and (f)(3)
of this AD, respectively.
(g) Actions done before the effective date
of this AD in accordance with Boeing Alert
Service Bulletin 737–25A1363, dated
November 5, 1998; or Revision 1, dated
March 28, 2002, is acceptable for compliance
with the corresponding action specified in
this AD.
Federal Aviation Administration
Alternative Methods of Compliance
(AMOCs)
(h)(1) The Manager, Seattle Aircraft
Certification Office (ACO), 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.
Material Incorporated by Reference
(i) You must use Boeing Alert Service
Bulletin 737–25A1363, Revision 2, dated
May 2, 2006, 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 Boeing Commercial Airplanes, P.O.
Box 3707, Seattle, Washington 98124–2207,
for a copy of this service information. You
may review copies at the FAA, Transport
Airplane Directorate, 1601 Lind Avenue,
S.W., 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/federalregister/cfr/ibr-locations.html.
Issued in Renton, Washington, on August
17, 2007.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E7–16909 Filed 8–27–07; 8:45 am]
pwalker on PROD1PC71 with NOTICES
16:51 Aug 27, 2007
[Docket No. FAA–2007–28353; Directorate
Identifier 2007–NM–065–AD; Amendment
39–15174; AD 2007–17–16]
RIN 2120–AA64
Airworthiness Directives; Gulfstream
Aerospace LP Model Galaxy Airplanes
and Model Gulfstream 200 Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
SUMMARY: We are adopting a new
airworthiness directive (AD) for the
products listed above. This AD results
from mandatory continuing
airworthiness information (MCAI)
originated by an aviation authority of
another country to identify and correct
an unsafe condition on an aviation
product. The MCAI describes the unsafe
condition as:
During the manufacturing process of the
Poppet Covers of the Pressurization Safety
Valves, burrs that could damage the Valve
Diaphragms were not removed. The damage
may eventually cause faulty operation of the
relief valves resulting in an unsafe condition
when combined with additional failures. The
serial numbers of the defective valves and the
affected aircraft were identified.
The unsafe condition is damage and
subsequent failure of the safety relief
valves, which could result in rapid
decompression of the airplane. We are
issuing this AD to require actions to
correct the unsafe condition on these
products.
This AD becomes effective
October 2, 2007.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of October 2, 2007.
ADDRESSES: You may examine the AD
docket on the Internet at https://
dms.dot.gov or in person at the U.S.
Department of Transportation, Docket
Operations, M–30, West Building
Ground Floor, Room W12–140, 1200
New Jersey Avenue SE., Washington,
DC.
DATES:
FOR FURTHER INFORMATION CONTACT:
Mike Borfitz, Aerospace Engineer,
International Branch, ANM–116, FAA,
Transport Airplane Directorate, 1601
Lind Avenue SW., Renton, Washington
98057–3356; telephone (425) 227–2677;
fax (425) 227–1149.
SUPPLEMENTARY INFORMATION:
BILLING CODE 4910–13–P
VerDate Aug<31>2005
14 CFR Part 39
Jkt 211001
PO 00000
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Fmt 4700
Sfmt 4700
Discussion
We issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would
apply to the specified products. That
NPRM was published in the Federal
Register on June 6, 2007 (72 FR 31204).
That NPRM proposed to correct an
unsafe condition for the specified
products. The MCAI states:
During the manufacturing process of the
Poppet Covers of the Pressurization Safety
Valves, burrs that could damage the Valve
Diaphragms were not removed. The damage
may eventually cause faulty operation of the
relief valves resulting in an unsafe condition
when combined with additional failures. The
serial numbers of the defective valves and the
affected aircraft were identified.
The unsafe condition is damage and
subsequent failure of the safety relief
valves, which could result in rapid
decompression of the airplane. The
corrective action includes replacing the
pressurization safety valve, part number
103842–3. You may obtain further
information by examining the MCAI in
the AD docket.
Comments
We gave the public the opportunity to
participate in developing this AD. We
received no comments on the NPRM or
on the determination of the cost to the
public.
Conclusion
We reviewed the available data and
determined that air safety and the
public interest require adopting the AD
as proposed.
Differences Between This AD and the
MCAI or Service Information
We have reviewed the MCAI and
related service information and, in
general, agree with their substance. But
we might have found it necessary to use
different words from those in the MCAI
to ensure the AD is clear for U.S.
operators and is enforceable. In making
these changes, we do not intend to differ
substantively from the information
provided in the MCAI and related
service information.
We might also have required different
actions in this AD from those in the
MCAI in order to follow our FAA
policies. Any such differences are
highlighted in a NOTE within the AD.
Costs of Compliance
Based on the service information, we
estimate that this AD affects about 7
products of U.S. registry. We also
estimate that it takes about 10 workhours per product to comply with the
basic requirements of this AD. The
E:\FR\FM\28AUR1.SGM
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Federal Register / Vol. 72, No. 166 / Tuesday, August 28, 2007 / Rules and Regulations
average labor rate is $80 per work-hour.
Required parts cost about $0 per
product. Where the service information
lists required parts costs that are
covered under warranty, we have
assumed that there will be no charge for
these costs. As we do not control
warranty coverage for affected parties,
some parties may incur costs higher
than estimated here. Based on these
figures, we estimate the cost of the AD
on U.S. operators to be $5,600, or $800
per product.
pwalker on PROD1PC71 with NOTICES
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 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 this AD:
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.
Examining the AD Docket
You may examine the AD docket on
the Internet at https://dms.dot.gov; or in
person at the Docket Operations office
VerDate Aug<31>2005
16:51 Aug 27, 2007
Jkt 211001
49171
replacing the pressurization safety valve, part
number 103842–3.
between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
The AD docket contains the NPRM, the
regulatory evaluation, any comments
received, and other information. The
street address for the Docket Operations
office (telephone (800) 647–5527) is in
the ADDRESSES section. Comments will
be available in the AD docket shortly
after receipt.
Actions and Compliance
(f) Unless already done, do the following
actions. Within 500 flight hours or 12 months
after the effective date of this AD, whichever
occurs first: Replace the pressurization safety
valve, part number 103842–3, according to
Gulfstream Service Bulletin 200–21–308,
dated February 23, 2007.
List of Subjects in 14 CFR Part 39
FAA AD Differences
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
Note: This AD differs from the MCAI and/
or service information as follows: No
differences.
Adoption of the Amendment
Other FAA AD Provisions
(g) The following provisions also apply to
this AD:
(1) Alternative Methods of Compliance
(AMOCs): The Manager, International
Branch, ANM–116, Transport Airplane
Directorate, FAA, has the authority to
approve AMOCs for this AD, if requested
using the procedures found in 14 CFR 39.19.
Send information to ATTN: Mike Borfitz,
Aerospace Engineer, International Branch,
ANM–116, Transport Airplane Directorate,
FAA, 1601 Lind Avenue SW., Renton,
Washington 98057–3356; telephone (425)
227–2677; fax (425) 227–1149. 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.
(2) Airworthy Product: For any requirement
in this AD to obtain corrective actions from
a manufacturer or other source, use these
actions if they are FAA-approved. Corrective
actions are considered FAA-approved if they
are approved by the State of Design Authority
(or their delegated agent). You are required
to assure the product is airworthy before it
is returned to service.
(3) Reporting Requirements: For any
reporting requirement in this AD, under the
provisions of the Paperwork Reduction Act,
the Office of Management and Budget (OMB)
has approved the information collection
requirements and has assigned OMB Control
Number 2120–0056.
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 FAA amends § 39.13 by adding
the following new AD:
I
2007–17–16 Gulfstream Aerospace LP
(Formerly Israel Aircraft Industries,
Ltd.): Amendment 39–15174. Docket No.
FAA–2007–28353; Directorate Identifier
2007–NM–065–AD.
Effective Date
(a) This airworthiness directive (AD)
becomes effective October 2, 2007.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Gulfstream Model
Galaxy airplanes and Model Gulfstream 200
airplanes, serial numbers 101 through 104,
109, 110, and 118, certificated in any
category.
Subject
(d) Air Transport Association (ATA) of
America Code 21: Air Conditioning.
Reason
(e) The mandatory continuing
airworthiness information (MCAI) states:
During the manufacturing process of the
Poppet Covers of the Pressurization Safety
Valves, burrs that could damage the Valve
Diaphragms were not removed. The damage
may eventually cause faulty operation of the
relief valves resulting in an unsafe condition
when combined with additional failures. The
serial numbers of the defective valves and the
affected aircraft were identified.
The unsafe condition is damage and
subsequent failure of the safety relief valves,
which could result in rapid decompression of
the airplane. The corrective action includes
PO 00000
Frm 00045
Fmt 4700
Sfmt 4700
Related Information
(h) Refer to MCAI Israeli Airworthiness
Directive 21–07–01–01, dated February 20,
2007; and Gulfstream Service Bulletin 200–
21–308, dated February 23, 2007; and
Honeywell Service Bulletin 103842–21–4126,
dated December 5, 2006; for related
information.
Material Incorporated by Reference
(i) You must use Gulfstream Service
Bulletin 200–21–308, dated February 23,
2007, to do the actions required by this AD,
unless the AD specifies otherwise.
(1) The Director of the Federal Register
approved the incorporation by reference of
this service information under 5 U.S.C.
552(a) and 1 CFR part 51.
(2) For service information identified in
this AD, contact Gulfstream Aerospace
Corporation, P.O. Box 2206, Mail Station D–
25, Savannah, Georgia 31402–2206.
E:\FR\FM\28AUR1.SGM
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49172
Federal Register / Vol. 72, No. 166 / Tuesday, August 28, 2007 / Rules and Regulations
(3) 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/ibrlocations.html.
Issued in Renton, Washington, on August
14, 2007.
Stephen P. Boyd,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. E7–16655 Filed 8–27–07; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2007–28436 Directorate
Identifier 2007–CE–055–AD; Amendment
39–15178; AD 2007–17–20]
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final Rule.
AGENCY:
To prevent cracks developing in the aileron
spar adjacent to the inboard hinge attachment
* * *
pwalker on PROD1PC71 with NOTICES
To prevent cracks developing in the aileron
spar adjacent to the inboard hinge attachment
accomplish the following:
Remove both ailerons, inspect and modify
the aileron spar at the inboard hinge
attachment point in accordance with Pacific
Aerospace Ltd Service Bulletin PACSB/XL/
027.
Conclusion
SUMMARY: We are adopting a new
airworthiness directive (AD) for the
products listed above. This AD results
from mandatory continuing
airworthiness information (MCAI)
issued by an aviation authority of
another country to identify and correct
an unsafe condition on an aviation
product. The MCAI describes the unsafe
condition as:
We are issuing this AD to require
actions to correct the unsafe condition
on these products.
DATES: This AD becomes effective
October 2, 2007.
On October 2, 2007, the Director of
the Federal Register approved the
incorporation by reference of certain
publications listed in this AD.
ADDRESSES: You may examine the AD
docket on the Internet at https://
dms.dot.gov or in person at Document
Management Facility, U.S. Department
of Transportation, Docket Operations,
M–30, West Building Ground Floor,
Room W12–140, 1200 New Jersey
Avenue, SE., Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT: Karl
Schletzbaum, Aerospace Engineer, FAA,
Jkt 211001
We issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would
apply to the specified products. That
NPRM was published in the Federal
Register on July 6, 2007 (72 FR 36905).
That NPRM proposed to correct an
unsafe condition for the specified
products. The MCAI states:
We gave the public the opportunity to
participate in developing this AD. We
received no comments on the NPRM or
on the determination of the cost to the
public.
Airworthiness Directives; Pacific
Aerospace Limited Model 750XL
Airplanes
16:51 Aug 27, 2007
Discussion
Comments
RIN 2120–AA64
VerDate Aug<31>2005
Small Airplane Directorate, 901 Locust,
Room 301, Kansas City, Missouri 64106;
telephone: (816) 329–4146; fax: (816)
329–4090.
SUPPLEMENTARY INFORMATION:
We reviewed the available data and
determined that air safety and the
public interest require adopting the AD
as proposed.
Differences Between this AD and the
MCAI or Service Information
We have reviewed the MCAI and
related service information and, in
general, agree with their substance. But
we might have found it necessary to use
different words from those in the MCAI
to ensure the AD is clear for U.S.
operators and is enforceable. In making
these changes, we do not intend to differ
substantively from the information
provided in the MCAI and related
service information.
We might also have required different
actions in this AD from those in the
MCAI in order to follow FAA policies.
Any such differences are highlighted in
a NOTE within the AD.
Costs of Compliance
We estimate that this AD will affect 7
products of U.S. registry. We also
estimate that it will take about 6 workhours per product to comply with basic
requirements of this AD. The average
labor rate is $80 per work-hour.
Required parts will cost about $864 per
product.
Based on these figures, we estimate
the cost of this AD to the U.S. operators
to be $9,408 or $1,344 per product.
PO 00000
Frm 00046
Fmt 4700
Sfmt 4700
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 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 this AD:
(1) Is not a ‘‘significant regulatory
action’’ under Executive Order 12866;
(2) Is not a ‘‘significant rule’’ under
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.
Examining the AD Docket
You may examine the AD docket on
the Internet at https://dms.dot.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 the
NPRM, 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.
E:\FR\FM\28AUR1.SGM
28AUR1
]]>Agencies
[Federal Register Volume 72, Number 166 (Tuesday, August 28, 2007)]
[Rules and Regulations]
[Pages 49170-49172]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E7-16655]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2007-28353; Directorate Identifier 2007-NM-065-AD;
Amendment 39-15174; AD 2007-17-16]
RIN 2120-AA64
Airworthiness Directives; Gulfstream Aerospace LP Model Galaxy
Airplanes and Model Gulfstream 200 Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for the
products listed above. This AD results from mandatory continuing
airworthiness information (MCAI) originated by an aviation authority of
another country to identify and correct an unsafe condition on an
aviation product. The MCAI describes the unsafe condition as:
During the manufacturing process of the Poppet Covers of the
Pressurization Safety Valves, burrs that could damage the Valve
Diaphragms were not removed. The damage may eventually cause faulty
operation of the relief valves resulting in an unsafe condition when
combined with additional failures. The serial numbers of the
defective valves and the affected aircraft were identified.
The unsafe condition is damage and subsequent failure of the safety
relief valves, which could result in rapid decompression of the
airplane. We are issuing this AD to require actions to correct the
unsafe condition on these products.
DATES: This AD becomes effective October 2, 2007.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of October 2,
2007.
ADDRESSES: You may examine the AD docket on the Internet at https://
dms.dot.gov or in person at the U.S. Department of Transportation,
Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200
New Jersey Avenue SE., Washington, DC.
FOR FURTHER INFORMATION CONTACT: Mike Borfitz, Aerospace Engineer,
International Branch, ANM-116, FAA, Transport Airplane Directorate,
1601 Lind Avenue SW., Renton, Washington 98057-3356; telephone (425)
227-2677; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would apply to the specified products.
That NPRM was published in the Federal Register on June 6, 2007 (72 FR
31204). That NPRM proposed to correct an unsafe condition for the
specified products. The MCAI states:
During the manufacturing process of the Poppet Covers of the
Pressurization Safety Valves, burrs that could damage the Valve
Diaphragms were not removed. The damage may eventually cause faulty
operation of the relief valves resulting in an unsafe condition when
combined with additional failures. The serial numbers of the
defective valves and the affected aircraft were identified.
The unsafe condition is damage and subsequent failure of the safety
relief valves, which could result in rapid decompression of the
airplane. The corrective action includes replacing the pressurization
safety valve, part number 103842-3. You may obtain further information
by examining the MCAI in the AD docket.
Comments
We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM or on the determination of
the cost to the public.
Conclusion
We reviewed the available data and determined that air safety and
the public interest require adopting the AD as proposed.
Differences Between This AD and the MCAI or Service Information
We have reviewed the MCAI and related service information and, in
general, agree with their substance. But we might have found it
necessary to use different words from those in the MCAI to ensure the
AD is clear for U.S. operators and is enforceable. In making these
changes, we do not intend to differ substantively from the information
provided in the MCAI and related service information.
We might also have required different actions in this AD from those
in the MCAI in order to follow our FAA policies. Any such differences
are highlighted in a NOTE within the AD.
Costs of Compliance
Based on the service information, we estimate that this AD affects
about 7 products of U.S. registry. We also estimate that it takes about
10 work-hours per product to comply with the basic requirements of this
AD. The
[[Page 49171]]
average labor rate is $80 per work-hour. Required parts cost about $0
per product. Where the service information lists required parts costs
that are covered under warranty, we have assumed that there will be no
charge for these costs. As we do not control warranty coverage for
affected parties, some parties may incur costs higher than estimated
here. Based on these figures, we estimate the cost of the AD on U.S.
operators to be $5,600, or $800 per product.
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 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 this AD:
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.
Examining the AD Docket
You may examine the AD docket on the Internet at https://
dms.dot.gov; or in person at the Docket Operations office between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD
docket contains the NPRM, the regulatory evaluation, any comments
received, and other information. The street address for the Docket
Operations office (telephone (800) 647-5527) is in the ADDRESSES
section. Comments will be available in the AD docket shortly after
receipt.
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 FAA amends Sec. 39.13 by adding the following new AD:
2007-17-16 Gulfstream Aerospace LP (Formerly Israel Aircraft
Industries, Ltd.): Amendment 39-15174. Docket No. FAA-2007-28353;
Directorate Identifier 2007-NM-065-AD.
Effective Date
(a) This airworthiness directive (AD) becomes effective October
2, 2007.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Gulfstream Model Galaxy airplanes and
Model Gulfstream 200 airplanes, serial numbers 101 through 104, 109,
110, and 118, certificated in any category.
Subject
(d) Air Transport Association (ATA) of America Code 21: Air
Conditioning.
Reason
(e) The mandatory continuing airworthiness information (MCAI)
states:
During the manufacturing process of the Poppet Covers of the
Pressurization Safety Valves, burrs that could damage the Valve
Diaphragms were not removed. The damage may eventually cause faulty
operation of the relief valves resulting in an unsafe condition when
combined with additional failures. The serial numbers of the
defective valves and the affected aircraft were identified.
The unsafe condition is damage and subsequent failure of the safety
relief valves, which could result in rapid decompression of the
airplane. The corrective action includes replacing the
pressurization safety valve, part number 103842-3.
Actions and Compliance
(f) Unless already done, do the following actions. Within 500
flight hours or 12 months after the effective date of this AD,
whichever occurs first: Replace the pressurization safety valve,
part number 103842-3, according to Gulfstream Service Bulletin 200-
21-308, dated February 23, 2007.
FAA AD Differences
Note: This AD differs from the MCAI and/ or service information
as follows: No differences.
Other FAA AD Provisions
(g) The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
has the authority to approve AMOCs for this AD, if requested using
the procedures found in 14 CFR 39.19. Send information to ATTN: Mike
Borfitz, Aerospace Engineer, International Branch, ANM-116,
Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton,
Washington 98057-3356; telephone (425) 227-2677; fax (425) 227-1149.
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.
(2) Airworthy Product: For any requirement in this AD to obtain
corrective actions from a manufacturer or other source, use these
actions if they are FAA-approved. Corrective actions are considered
FAA-approved if they are approved by the State of Design Authority
(or their delegated agent). You are required to assure the product
is airworthy before it is returned to service.
(3) Reporting Requirements: For any reporting requirement in
this AD, under the provisions of the Paperwork Reduction Act, the
Office of Management and Budget (OMB) has approved the information
collection requirements and has assigned OMB Control Number 2120-
0056.
Related Information
(h) Refer to MCAI Israeli Airworthiness Directive 21-07-01-01,
dated February 20, 2007; and Gulfstream Service Bulletin 200-21-308,
dated February 23, 2007; and Honeywell Service Bulletin 103842-21-
4126, dated December 5, 2006; for related information.
Material Incorporated by Reference
(i) You must use Gulfstream Service Bulletin 200-21-308, dated
February 23, 2007, to do the actions required by this AD, unless the
AD specifies otherwise.
(1) The Director of the Federal Register approved the
incorporation by reference of this service information under 5
U.S.C. 552(a) and 1 CFR part 51.
(2) For service information identified in this AD, contact
Gulfstream Aerospace Corporation, P.O. Box 2206, Mail Station D-25,
Savannah, Georgia 31402-2206.
[[Page 49172]]
(3) 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 August 14, 2007.
Stephen P. Boyd,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E7-16655 Filed 8-27-07; 8:45 am]
BILLING CODE 4910-13-P
