Airworthiness Directives; Gulfstream Aerospace LP Model Galaxy and Gulfstream 200 Airplanes, 47720-47722 [05-16002]
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47720
Federal Register / Vol. 70, No. 156 / Monday, August 15, 2005 / Rules and Regulations
Issued in Kansas City, Missouri, on August
8, 2005.
Kim Smith,
Acting Manager, Small Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 05–16000 Filed 8–12–05; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2005–22073; Directorate
Identifier 2005–NM–140–AD; Amendment
39–14219; AD 2005–16–13]
RIN 2120–AA64
Airworthiness Directives; Gulfstream
Aerospace LP Model Galaxy and
Gulfstream 200 Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; request for
comments.
AGENCY:
SUMMARY: The FAA is adopting a new
airworthiness directive (AD) for certain
Gulfstream Aerospace LP Model Galaxy
and Gulfstream 200 airplanes. This AD
requires a one-time general visual
inspection for any damaged wiring,
splice, connector, and pins for the fuel
standby feed pumps and replacement of
any damaged wiring, splice, connector,
or pin. This AD also requires
replacement of the power and ground
wires for the fuel standby feed pumps.
This AD results from reports of evidence
of overheating found on the feeder wires
of the left and right fuel standby feed
pumps. We are issuing this AD to detect
and correct damaged wiring for the fuel
standby feed pumps, which could result
in an ignition source in an area where
fuel vapor may be present, and a
consequent fire or explosion.
DATES: Effective Date: August 30, 2005.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in the AD
as of August 30, 2005.
We must receive comments on this
AD by October 14, 2005.
ADDRESSES: Use one of the following
addresses to submit comments on this
AD.
• DOT Docket Web site: Go to
https://dms.dot.gov and follow the
instructions for sending your comments
electronically.
• Government-wide rulemaking Web
site: Go to https://www.regulations.gov
and follow the instructions for sending
your comments electronically.
VerDate jul<14>2003
13:13 Aug 12, 2005
Jkt 205001
• 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 Gulfstream Aerospace
Corporation, P.O. Box 2206, Mail
Station D–25, Savannah, Georgia 31402–
2206, for service information identified
in this AD.
FOR FURTHER INFORMATION CONTACT: Dan
Rodina, Aerospace Engineer,
International Branch, ANM–116, FAA,
Transport Airplane Directorate, 1601
Lind Avenue, SW., Renton, Washington
98055–4056; telephone (425) 227–2125;
fax (425) 227–1149.
SUPPLEMENTARY INFORMATION:
Discussion
The Civil Aviation Administration of
Israel (CAAI), which is the
airworthiness authority for Israel,
notified us that an unsafe condition may
exist on certain Gulfstream Aerospace
LP Model Galaxy and Gulfstream 200
airplanes. The CAAI advises that, while
troubleshooting a fuel quantity
indication condition on a Model
Gulfstream 200 airplane, technicians
found evidence of overheating on the
feeder wires splice of the left fuel
standby feed pump 3Q1. Subsequent
investigation revealed a similar
condition in the wiring of the left and
right fuel standby feed pumps of four
other Model Gulfstream 200 airplanes.
This condition, if not corrected, could
result in an ignition source in an area
where fuel vapor may be present, and a
consequent fire or explosion.
The subject fuel standby feed pump
wiring on Model Galaxy airplanes is
identical to that on the affected Model
Gulfstream 200 airplanes. Therefore,
both of these models may be subject to
the same unsafe condition.
Relevant Service Information
Gulfstream Aerospace LP has issued
Alert Service Bulletin 200–28A–261,
dated June 7, 2005. The alert service
bulletin describes procedures for
performing a visual inspection of the
wiring, splice, connector, and pins for
the left (3Q1) and right (4Q1) fuel
standby feed pumps for damage, and for
replacing any damaged wiring, splice,
connector, or pin with a new wire,
splice, connector, or pin, as applicable.
Damage includes evidence of
overheating and worn or chafed
insulation. The alert service bulletin
PO 00000
Frm 00010
Fmt 4700
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also describes procedures for replacing
the power and ground wires for the fuel
standby feed pumps with 12-AmericanWire-Gauge (AWG) wires.
Accomplishing the actions specified in
the service information is intended to
adequately address the unsafe
condition.
The CAAI mandated the alert service
bulletin and issued Israeli airworthiness
directive 28–05–06–08, dated July 3,
2005, to ensure the continued
airworthiness of these airplanes in
Israel.
FAA’s Determination and Requirements
of This AD
These airplane models are
manufactured in Israel 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. Pursuant to this bilateral
airworthiness agreement, the CAAI has
kept the FAA informed of the situation
described above. We have examined the
CAAI’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
detect and correct any damaged wiring,
splice, connector, or pin for the fuel
standby feed pumps, which could result
in an ignition source in an area where
fuel vapor may be present, and a
consequent fire or explosion. This AD
requires accomplishing the actions
specified in the service information
described previously, except as
discussed under ‘‘Differences Between
the AD and Alert Service Bulletin’’.
Clarification of Inspection in the Israeli
Airworthiness Directive
The Israeli airworthiness directive
states only to ‘‘inspect’’ the wiring; it
does not define what type of inspection
should be done. We have determined
that the inspection in the Israeli
airworthiness directive should be
described as a ‘‘general visual
inspection.’’ Note 1 has been included
in this AD to define this type of
inspection.
Differences Between the AD and Alert
Service Bulletin
The Accomplishment Instructions of
Gulfstream Alert Service Bulletin 200–
28A–261, dated June 7, 2005, instruct
operators to inspect the wiring for worn
or chafed insulation; however, it gives
no repair instructions if any worn or
chafed insulation is found. This AD
requires operators to replace any wiring
E:\FR\FM\15AUR1.SGM
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Federal Register / Vol. 70, No. 156 / Monday, August 15, 2005 / Rules and Regulations
found with worn or chafed insulation
with new wiring. This difference has
been coordinated with the CAAI.
The Accomplishment Instructions of
Gulfstream Alert Service Bulletin 200–
28A–261, dated June 7, 2005, instruct
operators to complete and return a
Service Reply Card to Gulfstream
Aerospace LP. This AD does not include
that requirement.
FAA’s Determination of the Effective
Date
An unsafe condition exists that
requires the immediate adoption of this
AD; therefore, providing notice and
opportunity for public comment before
the AD is issued is impracticable, and
good cause exists to make this AD
effective in less than 30 days.
Comments Invited
This AD is a final rule that involves
requirements that affect flight safety and
was not preceded by notice and an
opportunity for public comment;
however, we invite you to submit any
relevant written data, views, or
arguments regarding this AD. Send your
comments to the address listed under
the ADDRESSES section. Include ‘‘Docket
No. FAA–2005–22073; Directorate
Identifier 2005–NM–140–AD’’ at the
beginning of your comments. We
specifically invite comments on the
overall regulatory, economic,
environmental, and energy aspects of
the AD that might suggest a need to
modify it.
We will post all comments we
receive, without change, to https://
dms.dot.gov, including any personal
information you provide. We will also
post a report summarizing each
substantive verbal contact with FAA
personnel concerning this AD. Using the
search function of that Web site, anyone
can find and read the comments in any
of our dockets, including the name of
the individual who sent the comment
(or signed the comment on behalf of an
association, business, labor union, etc.).
You may review the DOT’s complete
Privacy Act Statement in the Federal
Register published on April 11, 2000
(65 FR 19477–78), or you may visit
https://dms.dot.gov.
Examining the Docket
You may examine the AD docket on
the Internet at https://dms.dot.gov, or in
person at the Docket Management
Facility office between 9 a.m. and 5
p.m., Monday through Friday, except
Federal holidays. The Docket
Management Facility office (telephone
(800) 647–5227) is located on the plaza
level of the Nassif Building at the DOT
street address stated in the ADDRESSES
VerDate jul<14>2003
13:13 Aug 12, 2005
Jkt 205001
section. Comments will be available in
the AD docket shortly after the Docket
Management System receives them.
Authority for This Rulemaking
Title 49 of the United States Code
specifies the FAA’s authority to issue
rules on aviation safety. Subtitle I,
Section 106, describes the authority of
the FAA Administrator. Subtitle VII,
Aviation Programs, describes in more
detail the scope of the Agency’s
authority.
We are issuing this rulemaking under
the authority described in Subtitle VII,
Part A, Subpart III, Section 44701,
‘‘General requirements.’’ Under that
section, Congress charges the FAA with
promoting safe flight of civil aircraft in
air commerce by prescribing regulations
for practices, methods, and procedures
the Administrator finds necessary for
safety in air commerce. This regulation
is within the scope of that authority
because it addresses an unsafe condition
that is likely to exist or develop on
products identified in this rulemaking
action.
Regulatory Findings
We have determined that this AD will
not have federalism implications under
Executive Order 13132. This AD will
not have a substantial direct effect on
the States, on the relationship between
the National Government and the States,
or on the distribution of power and
responsibilities among the various
levels of government.
For the reasons discussed above, I
certify that the regulation:
1. Is not a ‘‘significant regulatory
action’’ under Executive Order 12866;
2. Is not a ‘‘significant rule’’ under the
DOT Regulatory Policies and Procedures
(44 FR 11034, February 26, 1979); and
3. Will not have a significant
economic impact, positive or negative,
on a substantial number of small entities
under the criteria of the Regulatory
Flexibility Act.
We prepared a regulatory evaluation
of the estimated costs to comply with
this AD and placed it in the AD docket.
See the ADDRESSES section for a location
to examine the regulatory evaluation.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
Adoption of the Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
I
PO 00000
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Fmt 4700
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47721
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
I
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The Federal Aviation
Administration (FAA) amends § 39.13 by
adding the following new airworthiness
directive (AD):
I
2005–16–13 Gulfstream Aerospace LP
(Formerly Israel Aircraft Industries,
Ltd.): Amendment 39–14219; Docket No.
FAA–2005–22073; Directorate Identifier
2005–NM–140–AD.
Effective Date
(a) This AD becomes effective August 30,
2005.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Gulfstream Model
Galaxy and Gulfstream 200 airplanes, having
serial numbers 004 through 113 inclusive,
certificated in any category.
Unsafe Condition
(d) This AD results from reports of
evidence of overheating found on the feeder
wires of the left and right fuel standby feed
pumps. We are issuing this AD to detect and
correct any damaged wiring, splice,
connector, or pin for the fuel standby feed
pumps, which could result in an ignition
source in an area where fuel vapor may be
present, and a consequent fire or explosion.
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.
Service Bulletin Reference
(f) The term ‘‘alert service bulletin,’’ as
used in this AD, means the Accomplishment
Instructions of Gulfstream Alert Service
Bulletin 200–28A–261, dated June 7, 2005.
Although the alert service bulletin referenced
in this AD specifies to submit information to
the manufacturer, this AD does not include
that requirement.
Inspection of the Wiring for the Fuel
Standby Feed Pumps
(g) Within 25 flight hours after the effective
date of this AD: Perform a general visual
inspection to detect damage of the wiring,
splice, connector, or pins of the left and right
fuel standby feed pumps, in accordance with
the alert service bulletin.
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
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15AUR1
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Federal Register / Vol. 70, No. 156 / Monday, August 15, 2005 / Rules and Regulations
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.’’
(1) If no damage is found: No further work
is required by this paragraph.
(2) If any damage is found: Before further
flight, replace the damaged wiring (including
wiring with worn or chafed insulation),
splice, connector, or pin with a new wiring,
splice, connector or pin, as applicable, in
accordance with the alert service bulletin.
Power and Ground Wire Replacement
(h) Within 25 flight hours after the effective
date of this AD: Replace the power and
ground wires of the left and right fuel
standby feed pumps with new, 12-AmericanWire-Gauge (AWG) wires, in accordance with
the alert service bulletin.
Alternative Methods of Compliance
(AMOCs)
Issued in Renton, Washington, on August
4, 2005.
Kevin M. Mullin,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. 05–16002 Filed 8–12–05; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2005–22074; Directorate
Identifier 2005–NM–152–AD; Amendment
39–14220; AD 2005–16–14]
RIN 2120–AA64
Airworthiness Directives; Gulfstream
Model G–IV, GIV–X, GV, and GV–SP
Series Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; request for
comments.
AGENCY:
(i) The Manager, International Branch,
ANM–116, Transport Airplane Directorate,
FAA, has the authority to approve AMOCs
for this AD, if requested in accordance with
the procedures found in 14 CFR 39.19.
Related Information
(j) Israeli airworthiness directive 28–05–
06–08, dated July 3, 2005, also addresses the
subject of this AD.
Material Incorporated by Reference
(k) You must use Gulfstream Alert Service
Bulletin 200–28A–261, dated June 7, 2005, 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 Gulfstream Aerospace
Corporation, P.O. Box 2206, Mail Station D–
25, Savannah, Georgia 31402–2206, for a
copy of this service information. You may
review copies at the Docket Management
Facility, U.S. Department of Transportation,
400 Seventh Street SW., Room PL–401,
Nassif Building, Washington, DC; on the
Internet at https://dms.dot.gov; or at the
National Archives and Records
Administration (NARA).
For information on the availability of this
material at the NARA, call (202) 741–6030,
or go to https://www.archives.gov/
federal_register/ code_of_federal_
regulations/ ibr_locations.html.
SUMMARY: The FAA is adopting a new
airworthiness directive (AD) for all
Gulfstream Model G–IV and GV series
airplanes, and certain GIV–X and GV–
SP series airplanes. This AD requires a
one-time inspection to determine if a
certain floor heater pad system is
installed, and deactivation of the subject
floor heater pad system if it is installed.
This AD results from an incident of
short-circuiting of the floor heater pads,
in which no circuit breakers tripped in
response to the short-circuiting. We are
issuing this AD to prevent shortcircuiting of the floor heater pad system,
which could result in a fire in the
airplane cabin.
DATES: Effective Date: August 30, 2005.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in the AD
as of August 30, 2005.
We must receive comments on this
AD by October 14, 2005.
ADDRESSES: Use one of the following
addresses to submit comments on this
AD.
• DOT Docket Web site: Go to
https://dms.dot.gov and follow the
instructions for sending your comments
electronically.
• Government-wide rulemaking Web
site: Go to https://www.regulations.gov
and follow the instructions for sending
your comments electronically.
• Mail: Docket Management Facility;
U.S. Department of Transportation, 400
Seventh Street SW., Nassif Building,
Room PL–401, Washington, DC 20590.
• Fax: (202) 493–2251.
• Hand Delivery: Room PL–401 on
the plaza level of the Nassif Building,
400 Seventh Street SW., Washington,
DC, between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
Contact Gulfstream Aerospace
Corporation, Technical Publications
Dept., P.O. Box 2206, Savannah, Georgia
31402–2206, for service information
identified in this AD.
FOR FURTHER INFORMATION CONTACT:
Robert Chupka, Aerospace Engineer,
Systems and Equipment Branch, ACE–
119A, FAA, Atlanta Aircraft
Certification Office, One Crown Center,
1895 Phoenix Boulevard, suite 450,
Atlanta, Georgia 30349; telephone (770)
703–6070; fax (770) 703–6097.
SUPPLEMENTARY INFORMATION:
Discussion
We have received a report of an
incident in which an Adel Wiggins floor
heater pad system short-circuited on a
Gulfstream GV–SP series airplane. The
short-circuit was discovered after an
odor of burning was detected emanating
from the floor of the cabin. The shortcircuit resulted in localized damage to
the floorboard and carpet. No circuit
breakers tripped as a result of the shortcircuiting. This condition, if not
corrected, could result in a fire in the
airplane cabin.
The subject Adel Wiggins floor heater
pad system may also be installed on all
Gulfstream Model G–IV and G–V series
airplanes and certain Gulfstream Model
GIV–X series airplanes. Therefore, those
models may be subject to the unsafe
condition revealed on certain Model
GV–SP series airplanes.
Relevant Service Information
We have reviewed the service
information specified in the table below.
RELEVANT GULFSTREAM SERVICE INFORMATION
For Gulfstream model—
Document title
G–IV ...........................................................................................
GV ..............................................................................................
G–IV (G300) ..............................................................................
GIV–X (G350) ............................................................................
G–IV (G400) ..............................................................................
GIV–X (G450) ............................................................................
GV–SP (G500) ...........................................................................
VerDate jul<14>2003
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Jkt 205001
PO 00000
Frm 00012
Gulfstream
Gulfstream
Gulfstream
Gulfstream
Gulfstream
Gulfstream
Gulfstream
Fmt 4700
Date
G–IV Alert Customer Bulletin 33 ...........................
GV Alert Customer Bulletin 22 ..............................
G300 Alert Customer Bulletin 33 ..........................
G350 Alert Customer Bulletin 2 ............................
G400 Alert Customer Bulletin 33 ..........................
G450 Alert Customer Bulletin 2 ............................
G500 Alert Customer Bulletin 3 ............................
Sfmt 4700
E:\FR\FM\15AUR1.SGM
15AUR1
June
June
June
June
June
June
June
13,
13,
13,
13,
13,
13,
13,
2005.
2005.
2005.
2005.
2005.
2005.
2005.
]]>Agencies
[Federal Register Volume 70, Number 156 (Monday, August 15, 2005)]
[Rules and Regulations]
[Pages 47720-47722]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-16002]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-22073; Directorate Identifier 2005-NM-140-AD;
Amendment 39-14219; AD 2005-16-13]
RIN 2120-AA64
Airworthiness Directives; Gulfstream Aerospace LP Model Galaxy
and Gulfstream 200 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 Gulfstream Aerospace LP Model Galaxy and Gulfstream 200
airplanes. This AD requires a one-time general visual inspection for
any damaged wiring, splice, connector, and pins for the fuel standby
feed pumps and replacement of any damaged wiring, splice, connector, or
pin. This AD also requires replacement of the power and ground wires
for the fuel standby feed pumps. This AD results from reports of
evidence of overheating found on the feeder wires of the left and right
fuel standby feed pumps. We are issuing this AD to detect and correct
damaged wiring for the fuel standby feed pumps, which could result in
an ignition source in an area where fuel vapor may be present, and a
consequent fire or explosion.
DATES: Effective Date: August 30, 2005.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in the AD as of August 30,
2005.
We must receive comments on this AD by October 14, 2005.
ADDRESSES: Use one of the following addresses to submit comments on
this AD.
DOT Docket Web site: Go to https://dms.dot.gov and follow
the instructions for sending your comments electronically.
Government-wide rulemaking Web site: Go to https://
www.regulations.gov and follow the instructions for sending your
comments electronically.
Mail: Docket Management Facility; U.S. Department of
Transportation, 400 Seventh Street SW., Nassif Building, Room PL-401,
Washington, DC 20590.
Fax: (202) 493-2251.
Hand Delivery: Room PL-401 on the plaza level of the
Nassif Building, 400 Seventh Street SW., Washington, DC, between 9 a.m.
and 5 p.m., Monday through Friday, except Federal holidays.
Contact Gulfstream Aerospace Corporation, P.O. Box 2206, Mail
Station D-25, Savannah, Georgia 31402-2206, for service information
identified in this AD.
FOR FURTHER INFORMATION CONTACT: Dan Rodina, Aerospace Engineer,
International Branch, ANM-116, FAA, Transport Airplane Directorate,
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425)
227-2125; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION:
Discussion
The Civil Aviation Administration of Israel (CAAI), which is the
airworthiness authority for Israel, notified us that an unsafe
condition may exist on certain Gulfstream Aerospace LP Model Galaxy and
Gulfstream 200 airplanes. The CAAI advises that, while troubleshooting
a fuel quantity indication condition on a Model Gulfstream 200
airplane, technicians found evidence of overheating on the feeder wires
splice of the left fuel standby feed pump 3Q1. Subsequent investigation
revealed a similar condition in the wiring of the left and right fuel
standby feed pumps of four other Model Gulfstream 200 airplanes. This
condition, if not corrected, could result in an ignition source in an
area where fuel vapor may be present, and a consequent fire or
explosion.
The subject fuel standby feed pump wiring on Model Galaxy airplanes
is identical to that on the affected Model Gulfstream 200 airplanes.
Therefore, both of these models may be subject to the same unsafe
condition.
Relevant Service Information
Gulfstream Aerospace LP has issued Alert Service Bulletin 200-28A-
261, dated June 7, 2005. The alert service bulletin describes
procedures for performing a visual inspection of the wiring, splice,
connector, and pins for the left (3Q1) and right (4Q1) fuel standby
feed pumps for damage, and for replacing any damaged wiring, splice,
connector, or pin with a new wire, splice, connector, or pin, as
applicable. Damage includes evidence of overheating and worn or chafed
insulation. The alert service bulletin also describes procedures for
replacing the power and ground wires for the fuel standby feed pumps
with 12-American-Wire-Gauge (AWG) wires. Accomplishing the actions
specified in the service information is intended to adequately address
the unsafe condition.
The CAAI mandated the alert service bulletin and issued Israeli
airworthiness directive 28-05-06-08, dated July 3, 2005, to ensure the
continued airworthiness of these airplanes in Israel.
FAA's Determination and Requirements of This AD
These airplane models are manufactured in Israel 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. Pursuant to this
bilateral airworthiness agreement, the CAAI has kept the FAA informed
of the situation described above. We have examined the CAAI'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 detect and correct any damaged
wiring, splice, connector, or pin for the fuel standby feed pumps,
which could result in an ignition source in an area where fuel vapor
may be present, and a consequent fire or explosion. This AD requires
accomplishing the actions specified in the service information
described previously, except as discussed under ``Differences Between
the AD and Alert Service Bulletin''.
Clarification of Inspection in the Israeli Airworthiness Directive
The Israeli airworthiness directive states only to ``inspect'' the
wiring; it does not define what type of inspection should be done. We
have determined that the inspection in the Israeli airworthiness
directive should be described as a ``general visual inspection.'' Note
1 has been included in this AD to define this type of inspection.
Differences Between the AD and Alert Service Bulletin
The Accomplishment Instructions of Gulfstream Alert Service
Bulletin 200-28A-261, dated June 7, 2005, instruct operators to inspect
the wiring for worn or chafed insulation; however, it gives no repair
instructions if any worn or chafed insulation is found. This AD
requires operators to replace any wiring
[[Page 47721]]
found with worn or chafed insulation with new wiring. This difference
has been coordinated with the CAAI.
The Accomplishment Instructions of Gulfstream Alert Service
Bulletin 200-28A-261, dated June 7, 2005, instruct operators to
complete and return a Service Reply Card to Gulfstream Aerospace LP.
This AD does not include that requirement.
FAA's Determination of the Effective Date
An unsafe condition exists that requires the immediate adoption of
this AD; therefore, providing notice and opportunity for public comment
before the AD is issued is impracticable, and good cause exists to make
this AD effective in less than 30 days.
Comments Invited
This AD is a final rule that involves requirements that affect
flight safety and was not preceded by notice and an opportunity for
public comment; however, we invite you to submit any relevant written
data, views, or arguments regarding this AD. Send your comments to the
address listed under the ADDRESSES section. Include ``Docket No. FAA-
2005-22073; Directorate Identifier 2005-NM-140-AD'' at the beginning of
your comments. We specifically invite comments on the overall
regulatory, economic, environmental, and energy aspects of the AD that
might suggest a need to modify it.
We will post all comments we receive, without change, to https://
dms.dot.gov, including any personal information you provide. We will
also post a report summarizing each substantive verbal contact with FAA
personnel concerning this AD. Using the search function of that Web
site, anyone can find and read the comments in any of our dockets,
including the name of the individual who sent the comment (or signed
the comment on behalf of an association, business, labor union, etc.).
You may review the DOT's complete Privacy Act Statement in the Federal
Register published on April 11, 2000 (65 FR 19477-78), or you may visit
https://dms.dot.gov.
Examining the Docket
You may examine the AD docket on the Internet at https://
dms.dot.gov, or in person at the Docket Management Facility office
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The Docket Management Facility office (telephone (800) 647-
5227) is located on the plaza level of the Nassif Building at the DOT
street address stated in the ADDRESSES section. Comments will be
available in the AD docket shortly after the Docket Management System
receives them.
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, Section 106, describes the
authority of the FAA Administrator. Subtitle VII, Aviation Programs,
describes in more detail the scope of the Agency's authority.
We are issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701, ``General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.
Regulatory Findings
We have determined that this AD will not have federalism
implications under Executive Order 13132. This AD will not have a
substantial direct effect on the States, on the relationship between
the National Government and the States, or on the distribution of power
and responsibilities among the various levels of government.
For the reasons discussed above, I certify that the regulation:
1. Is not a ``significant regulatory action'' under Executive Order
12866;
2. Is not a ``significant rule'' under the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979); and
3. Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
We prepared a regulatory evaluation of the estimated costs to
comply with this AD and placed it in the AD docket. See the ADDRESSES
section for a location to examine the regulatory evaluation.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
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):
2005-16-13 Gulfstream Aerospace LP (Formerly Israel Aircraft
Industries, Ltd.): Amendment 39-14219; Docket No. FAA-2005-22073;
Directorate Identifier 2005-NM-140-AD.
Effective Date
(a) This AD becomes effective August 30, 2005.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Gulfstream Model Galaxy and Gulfstream
200 airplanes, having serial numbers 004 through 113 inclusive,
certificated in any category.
Unsafe Condition
(d) This AD results from reports of evidence of overheating
found on the feeder wires of the left and right fuel standby feed
pumps. We are issuing this AD to detect and correct any damaged
wiring, splice, connector, or pin for the fuel standby feed pumps,
which could result in an ignition source in an area where fuel vapor
may be present, and a consequent fire or explosion.
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.
Service Bulletin Reference
(f) The term ``alert service bulletin,'' as used in this AD,
means the Accomplishment Instructions of Gulfstream Alert Service
Bulletin 200-28A-261, dated June 7, 2005. Although the alert service
bulletin referenced in this AD specifies to submit information to
the manufacturer, this AD does not include that requirement.
Inspection of the Wiring for the Fuel Standby Feed Pumps
(g) Within 25 flight hours after the effective date of this AD:
Perform a general visual inspection to detect damage of the wiring,
splice, connector, or pins of the left and right fuel standby feed
pumps, in accordance with the alert service bulletin.
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
[[Page 47722]]
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.''
(1) If no damage is found: No further work is required by this
paragraph.
(2) If any damage is found: Before further flight, replace the
damaged wiring (including wiring with worn or chafed insulation),
splice, connector, or pin with a new wiring, splice, connector or
pin, as applicable, in accordance with the alert service bulletin.
Power and Ground Wire Replacement
(h) Within 25 flight hours after the effective date of this AD:
Replace the power and ground wires of the left and right fuel
standby feed pumps with new, 12-American-Wire-Gauge (AWG) wires, in
accordance with the alert service bulletin.
Alternative Methods of Compliance (AMOCs)
(i) The Manager, International Branch, ANM-116, Transport
Airplane Directorate, FAA, has the authority to approve AMOCs for
this AD, if requested in accordance with the procedures found in 14
CFR 39.19.
Related Information
(j) Israeli airworthiness directive 28-05-06-08, dated July 3,
2005, also addresses the subject of this AD.
Material Incorporated by Reference
(k) You must use Gulfstream Alert Service Bulletin 200-28A-261,
dated June 7, 2005, 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
Gulfstream Aerospace Corporation, P.O. Box 2206, Mail Station D-25,
Savannah, Georgia 31402-2206, for a copy of this service
information. You may review copies at the Docket Management
Facility, U.S. Department of Transportation, 400 Seventh Street SW.,
Room PL-401, Nassif Building, Washington, DC; on the Internet at
https://dms.dot.gov; or at the National Archives and Records
Administration (NARA).
For information on the availability of this material at the
NARA, call (202) 741-6030, or go to https://www.archives.gov/
federal_register/code_of_federal_regulations/ibr_
locations.html.
Issued in Renton, Washington, on August 4, 2005.
Kevin M. Mullin,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 05-16002 Filed 8-12-05; 8:45 am]
BILLING CODE 4910-13-P
