Airworthiness Directives; Gulfstream Aerospace LP Model Gulfstream 200 Airplanes, 15816-15818 [E7-5898]
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<![CDATA[
15816
Federal Register / Vol. 72, No. 63 / Tuesday, April 3, 2007 / Rules and Regulations
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 March
22, 2007.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E7–5885 Filed 4–2–07; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2007–27737; Directorate
Identifier 2007–NM–029–AD; Amendment
39–15008; AD 2007–07–11]
RIN 2120–AA64
Airworthiness Directives; Gulfstream
Aerospace LP Model Gulfstream 200
Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; request for
comments.
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:
rwilkins on PROD1PC63 with RULES
Due to quality escape during serial
production, the jumpers at the Right Fuel
Standby Pump Connector 4Q1 were
manufactured from 14 AWG electrical wiring
instead of 12 AWG wires as required per
approved drawing. The possible overheating
of the 14 AWG jumpers routed in vicinity of
the fuel tank may present the unsafe flight
condition.
This AD requires actions that are
intended to address the unsafe
condition described in the MCAI.
DATES: This AD becomes effective April
18, 2007.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication, listed in the AD
as of April 18, 2007.
We must receive comments on this
AD by May 3, 2007.
ADDRESSES: You may send comments by
any of the following methods:
• DOT Docket Web Site: Go to
https://dms.dot.gov and follow the
instructions for sending your comments
electronically.
VerDate Aug<31>2005
16:32 Apr 02, 2007
Jkt 211001
• Fax: (202) 493–2251.
• Mail: Docket Management Facility,
U.S. Department of Transportation, 400
Seventh Street, SW., Nassif Building,
Room PL–401, Washington, DC 20590–
0001.
• 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.
• Federal eRulemaking Portal: https://
www.regulations.gov. Follow the
instructions for submitting comments.
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 this
AD, the regulatory evaluation, any
comments received, and other
information. The street address for the
Docket Office (telephone (800) 647–
5227) is in the ADDRESSES section.
Comments will be available in the AD
docket shortly after receipt.
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:
Streamlined Issuance of AD
The FAA is implementing a new
process for streamlining the issuance of
ADs related to MCAI. This streamlined
process will allow us to adopt MCAI
safety requirements in a more efficient
manner and will reduce safety risks to
the public. This process continues to
follow all FAA AD issuance processes to
meet legal, economic, Administrative
Procedure Act, and Federal Register
requirements. We also continue to meet
our technical decision-making
responsibilities to identify and correct
unsafe conditions on U.S.-certificated
products.
This AD references the MCAI and
related service information that we
considered in forming the engineering
basis to correct the unsafe condition.
The AD contains text copied from the
MCAI and for this reason might not
follow our plain language principles.
Discussion
The Civil Aviation Authority of Israel
(CAAI), which is the aviation authority
for Israel, has issued Israeli
Airworthiness Directive 28–07–02–03,
dated February 11, 2007 (referred to
after this as ‘‘the MCAI’’), to correct an
PO 00000
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Fmt 4700
Sfmt 4700
unsafe condition for the specified
products. The MCAI states:
Due to quality escape during serial
production, the jumpers at the Right Fuel
Standby Pump Connector 4Q1 were
manufactured from 14 AWG electrical wiring
instead of 12 AWG wires as required per
approved drawing. The possible overheating
of the 14 AWG jumpers routed in vicinity of
the fuel tank may present the unsafe flight
condition.
The corrective actions include
replacing the wiring, inspecting for
other components damaged by
overheating, and replacing damaged
components if necessary. You may
obtain further information by examining
the MCAI in the AD docket.
Relevant Service Information
Gulfstream has issued Alert Service
Bulletin 200–28A–315, dated February
5, 2007. The actions described in this
service information are intended to
correct the unsafe condition identified
in the MCAI.
FAA’s Determination and Requirements
of This AD
This product has been approved by
the aviation authority of another
country, and is approved for operation
in the United States. Pursuant to our
bilateral agreement with the State of
Design Authority, we have been notified
of the unsafe condition described in the
MCAI and service information
referenced above. We are issuing this
AD because we evaluated all pertinent
information and determined the unsafe
condition exists and is likely to exist or
develop on other products of the same
type design.
Differences Between the 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.
FAA’s Determination of the Effective
Date
An unsafe condition exists that
requires the immediate adoption of this
AD. The FAA has found that the risk to
the flying public justifies waiving notice
E:\FR\FM\03APR1.SGM
03APR1
Federal Register / Vol. 72, No. 63 / Tuesday, April 3, 2007 / Rules and Regulations
and comment prior to adoption of this
rule because, due to a quality escape
during serial production, the jumpers at
the right fuel standby pump connector
4Q1 were manufactured from 14 AWG
electrical wiring instead of 12 AWG
wires as required per approved drawing.
The overheating of the 14 AWG jumpers
routed in vicinity of the fuel tank may
cause the unsafe flight condition.
Therefore, we determined that notice
and opportunity for public comment
before issuing this AD are impracticable
and that good cause exists for making
this amendment effective in fewer than
30 days.
Comments Invited
This AD is a final rule that involves
requirements affecting flight safety, and
we did not precede it by notice and
opportunity for public comment. We
invite you to send any written relevant
data, views, or arguments about this AD.
Send your comments to an address
listed under the ADDRESSES section.
Include ‘‘Docket No. FAA–2007–27737;
Directorate Identifier 2007–NM–029–
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://
dms.dot.gov, including any personal
information you provide. We will also
post a report summarizing each
substantive verbal contact we receive
about this AD.
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.
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.
rwilkins on PROD1PC63 with RULES
Authority for This Rulemaking
§ 39.13
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.
I
VerDate Aug<31>2005
16:32 Apr 02, 2007
Jkt 211001
[Amended]
2007–07–11 Gulfstream Aerospace LP
(Formerly Israel Aircraft Industries,
Ltd.): Amendment 39–15008. Docket No.
FAA–2007–27737; Directorate Identifier
2007–NM–029–AD.
Effective Date
(a) This airworthiness directive (AD)
becomes effective April 18, 2007.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Gulfstream Model
Gulfstream 200 airplanes, certificated in any
category, serial numbers 121 through 154.
Subject
(d) Fuel.
Reason
(e) The mandatory continued airworthiness
information (MCAI) states:
Frm 00013
Fmt 4700
Due to quality escape during serial
production, the jumpers at the Right Fuel
Standby Pump Connector 4Q1 were
manufactured from 14 AWG electrical wiring
instead of 12 AWG wires as required per
approved drawing. The possible overheating
of the 14 AWG jumpers routed in vicinity of
the fuel tank may present the unsafe flight
condition.
The corrective actions include replacing
the wiring, inspecting for other components
damaged by overheating, and replacing
damaged components if necessary.
Actions and Compliance
(f) Within 25 flight hours or 30 days,
whichever occurs first, after the effective date
of this AD, unless already done, do the
following actions.
(1) Replace the wiring according to the
Gulfstream Alert Service Bulletin 200–28A–
315, dated February 5, 2007.
(2) Do a general visual inspection for other
components damaged by overheating.
Replace all damaged components, before
further flight, using a method approved by
either the Manager, International Branch,
ANM–116, Transport Airplane Directorate,
FAA; or the Civil Aviation Authority of Israel
(CAAI) (or its delegated agent). One approved
method is the Gulfstream G200 Maintenance
Manual.
Note 1: For the purposes of this AD, a
general visual inspection is: ‘‘A visual
examination of an interior or exterior area,
installation, or assembly to detect obvious
damage, failure, or irregularity. This level of
inspection is made from within touching
distance unless otherwise specified. A mirror
may be necessary to ensure visual access to
all surfaces in the inspection area. This level
of inspection is made under normally
available lighting conditions such as
daylight, hangar lighting, flashlight, or
droplight and may require removal or
opening of access panels or doors. Stands,
ladders, or platforms may be required to gain
proximity to the area being checked.’’
FAA AD Differences
2. The FAA amends § 39.13 by adding
the following new AD:
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15817
Sfmt 4700
Note 2: This AD differs from the MCAI
and/or service information as follows:
(1) The MCAI specifies to ‘‘inspect and
replace the wiring’’ and ‘‘replace other
components damaged by overheating.’’
However, this AD requires replacing the
wiring, inspecting for other components
damaged by overheating, and replacing
damaged components as applicable. We have
defined the inspection as a ‘‘general visual
inspection.’’
(2) The MCAI does not specify service
information for replacing components other
than wiring. We require that the
replacements be done in accordance with a
method approved by the FAA or CAAI.
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, 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,
E:\FR\FM\03APR1.SGM
03APR1
15818
Federal Register / Vol. 72, No. 63 / Tuesday, April 3, 2007 / Rules and Regulations
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. Before using
any AMOC approved in accordance with
§ 39.19 on any airplane to which the AMOC
applies, notify the appropriate principal
inspector in the FAA Flight Standards
Certificate Holding District Office.
(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 28–07–02–03, dated February 11,
2007, and Gulfstream Alert Service Bulletin
200–28A–315, dated February 5, 2007, for
related information.
Material Incorporated by Reference
(i) You must use Gulfstream Alert Service
Bulletin 200–28A–315, dated February 5,
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.
(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 March
23, 2007.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E7–5898 Filed 4–2–07; 8:45 am]
rwilkins on PROD1PC63 with RULES
BILLING CODE 4910–13–P
VerDate Aug<31>2005
16:32 Apr 02, 2007
Jkt 211001
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2007–27735; Directorate
Identifier 2007–NM–027–AD; Amendment
39–15009; AD 2007–07–12]
RIN 2120–AA64
Airworthiness Directives; Honeywell
Flight Management Systems (FMSs)
Served by Honeywell NZ–2000
Navigation Computers Approved
Under Technical Standard Order (TSO)
TSO–C115a, and IC–800 Integrated
Avionics Computers Approved Under
TSOs C9c, C52a, and C115a; as
Installed on Various Transport
Category Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; request for
comments.
AGENCY:
The FAA is adopting a new
airworthiness directive (AD) for all
Honeywell FMSs served by Honeywell
NZ–2000 navigation computers and IC–
800 integrated avionics computers. This
AD requires identifying affected
computers by part number and software
modification level and revising the
Limitations section of applicable
airplane flight manuals to provide
procedures for retaining optimum
position determination and intended
navigation. This AD results from reports
of in-flight unannunciated shifts of
computed position in airplanes with the
subject flight management system (FMS)
computers. We are issuing this AD to
prevent a shift in the FMS computed
position, which could result in
uncommanded deviations from the
intended flight path of the airplane and,
if those deviations are undetected by the
flight crew, compromised terrain/traffic
avoidance.
DATES: This AD becomes effective April
18, 2007.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in the AD
as of April 18, 2007.
We must receive comments on this
AD by June 4, 2007.
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
SUMMARY:
PO 00000
Frm 00014
Fmt 4700
Sfmt 4700
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 Honeywell, P.O. Box 21111,
Phoenix, AZ 85036–1111, for service
information identified in this AD.
FOR FURTHER INFORMATION CONTACT: Joe
Brownlee, Flight Test Pilot, Flight Test
Branch, ANM–160L, FAA, Los Angeles
Aircraft Certification Office, 3960
Paramount Boulevard, Lakewood,
California 90712–4137; telephone (562)
627–5365; fax (562) 627–5210.
SUPPLEMENTARY INFORMATION:
Discussion
We have received reports of in-flight
unannunciated shifts of computed
position in airplanes with Honeywell
NZ–2000 navigation and IC–800
integrated avionics computers serving
Honeywell Flight Management Systems
(FMSs). The computed position shift,
attributed to a software design error
induced during a previous software
modification, occurs when the number
of inertial reference units (IRUs)
supplying data to the FMS degrades
from 3 to 2 or from 2 to 1, or increases
from 2 to 3 or from 1 to 2. If the FMS
system is coupled to an autopilot or
flight director system, this shift in the
FMS computed position could result in
uncommanded deviations from the
intended flight path of the airplane and,
if those deviations are undetected by the
flight crew, compromised terrain/traffic
avoidance.
Relevant Service Information
We have reviewed Honeywell
Technical Newsletter A23–6111–008,
Revision 001, dated February 22, 2007.
This technical newsletter describes
procedures for determining affected
FMS computers receiving position
information from multiple IRUs by
identifying the part number and
software modification level of the NZ–
2000 navigation and IC–800 integrated
avionics computers serving these Flight
Management Systems. For airplanes
with affected part numbers and software
modification levels, the newsletter also
describes revising the Limitations
section of the applicable airplane flight
manuals (AFMs) to provide procedures
for deselecting all but one IRS to each
FMS on every power-up cycle. The
E:\FR\FM\03APR1.SGM
03APR1
]]>Agencies
[Federal Register Volume 72, Number 63 (Tuesday, April 3, 2007)]
[Rules and Regulations]
[Pages 15816-15818]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E7-5898]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2007-27737; Directorate Identifier 2007-NM-029-AD;
Amendment 39-15008; AD 2007-07-11]
RIN 2120-AA64
Airworthiness Directives; Gulfstream Aerospace LP Model
Gulfstream 200 Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; request for comments.
-----------------------------------------------------------------------
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:
Due to quality escape during serial production, the jumpers at
the Right Fuel Standby Pump Connector 4Q1 were manufactured from 14
AWG electrical wiring instead of 12 AWG wires as required per
approved drawing. The possible overheating of the 14 AWG jumpers
routed in vicinity of the fuel tank may present the unsafe flight
condition.
This AD requires actions that are intended to address the unsafe
condition described in the MCAI.
DATES: This AD becomes effective April 18, 2007.
The Director of the Federal Register approved the incorporation by
reference of a certain publication, listed in the AD as of April 18,
2007.
We must receive comments on this AD by May 3, 2007.
ADDRESSES: You may send comments by any of the following methods:
DOT Docket Web Site: Go to https://dms.dot.gov and follow
the instructions for sending your comments electronically.
Fax: (202) 493-2251.
Mail: Docket Management Facility, U.S. Department of
Transportation, 400 Seventh Street, SW., Nassif Building, Room PL-401,
Washington, DC 20590-0001.
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.
Federal eRulemaking Portal: https://www.regulations.gov.
Follow the instructions for submitting comments.
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 this AD, the regulatory evaluation, any comments
received, and other information. The street address for the Docket
Office (telephone (800) 647-5227) is in the ADDRESSES section. Comments
will be available in the AD docket shortly after receipt.
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:
Streamlined Issuance of AD
The FAA is implementing a new process for streamlining the issuance
of ADs related to MCAI. This streamlined process will allow us to adopt
MCAI safety requirements in a more efficient manner and will reduce
safety risks to the public. This process continues to follow all FAA AD
issuance processes to meet legal, economic, Administrative Procedure
Act, and Federal Register requirements. We also continue to meet our
technical decision-making responsibilities to identify and correct
unsafe conditions on U.S.-certificated products.
This AD references the MCAI and related service information that we
considered in forming the engineering basis to correct the unsafe
condition. The AD contains text copied from the MCAI and for this
reason might not follow our plain language principles.
Discussion
The Civil Aviation Authority of Israel (CAAI), which is the
aviation authority for Israel, has issued Israeli Airworthiness
Directive 28-07-02-03, dated February 11, 2007 (referred to after this
as ``the MCAI''), to correct an unsafe condition for the specified
products. The MCAI states:
Due to quality escape during serial production, the jumpers at
the Right Fuel Standby Pump Connector 4Q1 were manufactured from 14
AWG electrical wiring instead of 12 AWG wires as required per
approved drawing. The possible overheating of the 14 AWG jumpers
routed in vicinity of the fuel tank may present the unsafe flight
condition.
The corrective actions include replacing the wiring, inspecting for
other components damaged by overheating, and replacing damaged
components if necessary. You may obtain further information by
examining the MCAI in the AD docket.
Relevant Service Information
Gulfstream has issued Alert Service Bulletin 200-28A-315, dated
February 5, 2007. The actions described in this service information are
intended to correct the unsafe condition identified in the MCAI.
FAA's Determination and Requirements of This AD
This product has been approved by the aviation authority of another
country, and is approved for operation in the United States. Pursuant
to our bilateral agreement with the State of Design Authority, we have
been notified of the unsafe condition described in the MCAI and service
information referenced above. We are issuing this AD because we
evaluated all pertinent information and determined the unsafe condition
exists and is likely to exist or develop on other products of the same
type design.
Differences Between the 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.
FAA's Determination of the Effective Date
An unsafe condition exists that requires the immediate adoption of
this AD. The FAA has found that the risk to the flying public justifies
waiving notice
[[Page 15817]]
and comment prior to adoption of this rule because, due to a quality
escape during serial production, the jumpers at the right fuel standby
pump connector 4Q1 were manufactured from 14 AWG electrical wiring
instead of 12 AWG wires as required per approved drawing. The
overheating of the 14 AWG jumpers routed in vicinity of the fuel tank
may cause the unsafe flight condition. Therefore, we determined that
notice and opportunity for public comment before issuing this AD are
impracticable and that good cause exists for making this amendment
effective in fewer than 30 days.
Comments Invited
This AD is a final rule that involves requirements affecting flight
safety, and we did not precede it by notice and opportunity for public
comment. We invite you to send any written relevant data, views, or
arguments about this AD. Send your comments to an address listed under
the ADDRESSES section. Include ``Docket No. FAA-2007-27737; Directorate
Identifier 2007-NM-029-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://
dms.dot.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 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.
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:
2007-07-11 Gulfstream Aerospace LP (Formerly Israel Aircraft
Industries, Ltd.): Amendment 39-15008. Docket No. FAA-2007-27737;
Directorate Identifier 2007-NM-029-AD.
Effective Date
(a) This airworthiness directive (AD) becomes effective April
18, 2007.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Gulfstream Model Gulfstream 200
airplanes, certificated in any category, serial numbers 121 through
154.
Subject
(d) Fuel.
Reason
(e) The mandatory continued airworthiness information (MCAI)
states:
Due to quality escape during serial production, the jumpers at
the Right Fuel Standby Pump Connector 4Q1 were manufactured from 14
AWG electrical wiring instead of 12 AWG wires as required per
approved drawing. The possible overheating of the 14 AWG jumpers
routed in vicinity of the fuel tank may present the unsafe flight
condition.
The corrective actions include replacing the wiring, inspecting
for other components damaged by overheating, and replacing damaged
components if necessary.
Actions and Compliance
(f) Within 25 flight hours or 30 days, whichever occurs first,
after the effective date of this AD, unless already done, do the
following actions.
(1) Replace the wiring according to the Gulfstream Alert Service
Bulletin 200-28A-315, dated February 5, 2007.
(2) Do a general visual inspection for other components damaged
by overheating. Replace all damaged components, before further
flight, using a method approved by either the Manager, International
Branch, ANM-116, Transport Airplane Directorate, FAA; or the Civil
Aviation Authority of Israel (CAAI) (or its delegated agent). One
approved method is the Gulfstream G200 Maintenance Manual.
Note 1: For the purposes of this AD, a general visual inspection
is: ``A visual examination of an interior or exterior area,
installation, or assembly to detect obvious damage, failure, or
irregularity. This level of inspection is made from within touching
distance unless otherwise specified. A mirror may be necessary to
ensure visual access to all surfaces in the inspection area. This
level of inspection is made under normally available lighting
conditions such as daylight, hangar lighting, flashlight, or
droplight and may require removal or opening of access panels or
doors. Stands, ladders, or platforms may be required to gain
proximity to the area being checked.''
FAA AD Differences
Note 2: This AD differs from the MCAI and/or service information
as follows:
(1) The MCAI specifies to ``inspect and replace the wiring'' and
``replace other components damaged by overheating.'' However, this
AD requires replacing the wiring, inspecting for other components
damaged by overheating, and replacing damaged components as
applicable. We have defined the inspection as a ``general visual
inspection.''
(2) The MCAI does not specify service information for replacing
components other than wiring. We require that the replacements be
done in accordance with a method approved by the FAA or CAAI.
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, 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,
[[Page 15818]]
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. Before
using any AMOC approved in accordance with Sec. 39.19 on any
airplane to which the AMOC applies, notify the appropriate principal
inspector in the FAA Flight Standards Certificate Holding District
Office.
(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 28-07-02-03,
dated February 11, 2007, and Gulfstream Alert Service Bulletin 200-
28A-315, dated February 5, 2007, for related information.
Material Incorporated by Reference
(i) You must use Gulfstream Alert Service Bulletin 200-28A-315,
dated February 5, 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.
(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 March 23, 2007.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E7-5898 Filed 4-2-07; 8:45 am]
BILLING CODE 4910-13-P
