Airworthiness Directives; Gulfstream Model GV-SP Series Airplanes, 18253-18254 [E6-5253]
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Federal Register / Vol. 71, No. 69 / Tuesday, April 11, 2006 / Proposed Rules
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The Federal Aviation
Administration (FAA) amends § 39.13
by removing amendment 39–14396 (70
FR 72595, December 6, 2005) and
adding the following new airworthiness
directive (AD):
Boeing: Docket No. FAA–2006–24369;
Directorate Identifier 2006–NM–001–AD.
Comments Due Date
(a) The FAA must receive comments on
this AD action by May 26, 2006.
Affected ADs
(b) This AD supersedes AD 2005–25–03.
Applicability
(c) This AD applies to Boeing Model 737–
600, –700, –700C, and –800 series airplanes,
certificated in any category; as identified in
Boeing Alert Service Bulletin (ASB) 737–
53A1222, Revision 2, dated October 20, 2005.
Unsafe Condition
(d) This AD results from full-scale fuselage
fatigue testing on a splice fitting that failed
prior to the design objective on Boeing Model
737–800 series airplanes, and a report of a
cracked splice fitting on an operational
airplane. We are issuing this AD to prevent
cracking of the existing fitting, which may
result in cracking through the skin and
consequent decompression of the flight
cabin.
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.
hsrobinson on PROD1PC70 with PROPOSALS
Restatement of Certain Requirements of AD
2005–25–03
Replacing the Splice Fittings
(f) Replace the splice fittings with new
splice fittings in accordance with the
Accomplishment Instructions of Boeing ASB
737–53A1222, Revision 2, dated October 20,
2005, at the times specified in paragraph
(f)(1) or (f)(2) of this AD, as applicable. Before
further flight, do any related investigative
actions by accomplishing all the applicable
actions specified in the Accomplishment
Instructions.
(1) For airplanes that have accumulated
fewer than 13,500 total flight cycles as
December 21, 2005 (the effective date of AD
2005–25–03): Replace prior to the
accumulation of 13,500 total flight cycles, or
within 1,000 flight cycles after December 21,
2005, whichever occurs later.
(2) For airplanes that have accumulated
13,500 or more total flight cycles as of
December 21, 2005: Replace at the later of the
times specified in paragraphs (f)(2)(i) and
(f)(2)(ii) of this AD.
VerDate Aug<31>2005
15:25 Apr 10, 2006
Jkt 208001
18253
(i) Prior to the accumulation of 18,000 total
flight cycles, or within 1,000 flight cycles
after December 21, 2005, whichever occurs
first.
(ii) Within 90 days after December 21,
2005.
DEPARTMENT OF TRANSPORTATION
New Requirements of This AD
[Docket No. FAA–2005–23249; Directorate
Identifier 2005–NM–219–AD]
Repetitive Inspections
(g) Within 24,000 flight cycles after
accomplishing the actions specified in
paragraph (f) of this AD, perform an external
detailed inspection of the skin just below
each splice fitting, in accordance with the
Accomplishment Instructions of Boeing ASB
737–53A1222, Revision 2, dated October 20,
2005. Thereafter, repeat the external detailed
inspections at intervals not to exceed 24,000
flight cycles.
Corrective Actions
(h) If any cracking is found during any
inspection required by this AD, prior to
further flight, repair in accordance with a
method approved by the Manager, Seattle
Aircraft Certification Office (ACO), FAA, or
with a method approved in accordance with
the procedures specified in paragraph (j) of
this AD.
Acceptable Method of Compliance
(i) Replacing the splice fitting and any
related investigative actions before December
21, 2005 (the effective date of AD 2005–25–
03), in accordance with Boeing Service
Bulletin 737–53–1222, dated June 6, 2002; or
Boeing ASB 737–53A1222, Revision 1, dated
January 30, 2003, is acceptable for
compliance with the requirements of
paragraph (f) of this AD.
Alternative Methods of Compliance (AMOCs)
(j)(1) The Manager, Seattle 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) 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.
(3) An AMOC that provides an acceptable
level of safety may be used for any repair
required by this AD, if it is approved by an
Authorized Representative for the Boeing
Commercial Airplanes Delegation Option
Authorization Organization who has been
authorized by the Manager, Seattle ACO, to
make those findings. For a repair method to
be approved, the repair must meet the
certification basis of the airplane, and the
approval must specifically refer to this AD.
(4) AMOCs approved previously in
accordance with AD 2005–25–03,
amendment 39–14396, are approved as
AMOCs for the corresponding provisions of
paragraphs (f) and (h) of this AD.
Issued in Renton, Washington, on March
31, 2006.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 06–3442 Filed 4–10–06; 8:45 am]
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Federal Aviation Administration
14 CFR Part 39
RIN 2120–AA64
Airworthiness Directives; Gulfstream
Model GV–SP Series Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Proposed rule; withdrawal.
AGENCY:
SUMMARY: The FAA withdraws a notice
of proposed rulemaking (NPRM) that
proposed a new airworthiness directive
(AD) for certain Gulfstream Model GV–
SP series airplanes. The proposed AD
would have required an inspection to
determine the serial number of the antiskid control unit (ACU) in the right
electronics equipment rack, and
replacement of the ACU with a new or
serviceable ACU if necessary. Since the
proposed AD was issued, we have
received new data that indicate the
identified unsafe condition has been
corrected on all airplanes that would
have been affected by the NPRM, and on
all ACUs in the affected range of serial
numbers. Accordingly, the proposed AD
is withdrawn.
ADDRESSES: 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 U.S. Department of Transportation,
400 Seventh Street, SW., Room PL–401,
Washington, DC. This docket number is
FAA–2005–23249; the directorate
identifier for this docket is 2005–NM–
219–AD.
FOR FURTHER INFORMATION CONTACT:
Darby Mirocha, 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)
703–6095; fax (770) 703–6097.
SUPPLEMENTARY INFORMATION:
Discussion
We proposed to amend part 39 of the
Federal Aviation Regulations (14 CFR
part 39) with a notice of proposed
rulemaking (NPRM) for a new AD for
certain Gulfstream Model GV–SP series
airplanes. That NPRM was published in
E:\FR\FM\11APP1.SGM
11APP1
18254
Federal Register / Vol. 71, No. 69 / Tuesday, April 11, 2006 / Proposed Rules
the Federal Register on December 9,
2005 (70 FR 73173). The NPRM would
have required an inspection to
determine the serial number of the antiskid control unit (ACU) in the right
electronics equipment rack, and
replacement of the ACU with a new or
serviceable ACU if necessary. The
NPRM resulted from a report that an
airplane temporarily lost normal braking
function during landing rollout on a
pre-delivery flight. The proposed
actions were intended to prevent loss of
normal braking function, which could
result in a runway overrun that could
cause injury to flightcrew or passengers
or damage to the airplane.
hsrobinson on PROD1PC70 with PROPOSALS
Actions Since NPRM Was Issued
Since we issued the NPRM,
Gulfstream Aerospace has provided data
that indicate the identified unsafe
condition has been corrected on all
airplanes that would have been affected
by the NPRM, and on all ACUs in the
affected range of serial numbers (S/Ns).
Gulfstream Aerospace therefore requests
that we withdraw the NPRM. We agree
with the commenter.
Request To Incorporate by Reference
(IBR) the Service Information
The Modification and Replacement
Parts Association (MARPA) requests
that we either publish the relevant
service information with the AD, or IBR
it with the NPRM. If we IBR rather than
publish the relevant service
information, then MARPA further
requests that we identify the S/Ns of the
defective ACUs in the AD. As
justification, MARPA states that parts
purveyors and maintenance facilities
cannot identify the defective parts
unless we specify them in the AD
because they do not possess the
proprietary service information
referenced in the NPRM. For the same
reason, MARPA states that those in the
alternative parts industry (operating
under 14 CFR 21.303) also cannot
identify any parts manufacturer
approval (PMA) parts equivalent to the
defective ACUs. MARPA asserts that
there are many ACUs in its PMA
database that also may be affected by
unsafe condition identified in the
NPRM.
MARPA also comments on our
practice of IBR and referencing
propriety service information. MARPA
asserts that if we IBR proprietary service
information with a public document,
such as an AD, then that service
information loses its protected status
and becomes a public document. Also,
MARPA claims that IBR requires we
provide a copy of the relevant service
information to the Director of the
VerDate Aug<31>2005
15:25 Apr 10, 2006
Jkt 208001
Federal Register before the NPRM can
be published. MARPA further states
that: ‘‘Merely referencing a service
document without incorporation thus
becomes an ‘‘end run’’ around the
publication requirement while still
requiring possession of a proprietary
document in order to comply with the
law.’’ MARPA believes our practice of
IBR is flawed legally where it is
impossible to comply with the
requirements of an AD without first
obtaining the necessary propriety
service information.
Although we acknowledge MARPA’s
comments, we do not agree with its
request, since the identified unsafe
condition has been corrected on all
airplanes that would have been affected
by the NPRM and on all ACUs in the
affected range of S/Ns. Those affected
parts are ACUs having part number
1159SCL501–1 and S/Ns 355 through
400 inclusive. The unsafe condition
identified in the NPRM was caused by
the installation of incorrect capacitors in
the affected ACUs only. Since that
NPRM addresses a quality control issue
limited to a range of S/Ns, we find that
the MARPA’s statements regarding PMA
equivalent parts are not relevant to that
particular NPRM.
We have one correction regarding
MARPA’s comments on our practice of
IBR and referencing propriety service
information; we are required to provide
a copy of any relevant service
information to the Director of the
Federal Register for publication of a
final rule, not an NPRM. We are
currently reviewing our practice of
referencing proprietary service
information. Once we have thoroughly
examined all aspects of this issue, and
have made a final determination, we
will consider whether our current
practice needs to be revised.
FAA’s Conclusions
Upon further consideration, we have
determined that the actions that would
have been required by the NPRM have
already been accomplished on all
affected airplanes, and that the
identified unsafe condition has been
corrected on all affected ACUs.
Accordingly, the NPRM is withdrawn.
Withdrawal of the NPRM does not
preclude the FAA from issuing another
related action or commit the FAA to any
course of action in the future.
Regulatory Impact
Since this action only withdraws an
NPRM, it is neither a proposed nor a
final rule and therefore is not covered
under Executive Order 12866, the
Regulatory Flexibility Act, or DOT
PO 00000
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Regulatory Policies and Procedures (44
FR 11034, February 26, 1979).
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Safety.
The Withdrawal
Accordingly, we withdraw the NPRM,
Docket No. FAA–2005–23249,
Directorate Identifier 2005–NM–219–
AD, which was published in the Federal
Register on December 9, 2005 (70 FR
73173).
Issued in Renton, Washington, on March
31, 2006.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E6–5253 Filed 4–10–06; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 71
[Docket No. FAA–2006–23902; Airspace
Docket No. 06–AGL–01]
Proposed Modification of Class E
Airspace; Fremont, MI
Federal Aviation
Administration, (FAA), DOT.
ACTION: Notice of proposed rulemaking.
AGENCY:
SUMMARY: This document proposes to
modify Class E airspace at Fremont, MI.
Standard Instrument Approach
Procedures have been developed for
Fremont Municipal Airport, Fremont,
MI. Controlled airspace extending
upward from 700 feet or more above the
surface of the earth is needed to contain
aircraft executing these approaches.
This action would increase the area of
the existing controlled airspace for
Fremont, MI.
DATES: Comments must be received on
or before June 5, 2006.
ADDRESSES: Send comments on the
proposal to the Docket Management
System, U.S. Department of
Transportation, Room Plaza 401, 400
Seventh Street, SW., Washington, DC
20590–0001. You must identify the
docket Number FAA–2006–23901/
Airspace Docket No. 06–AGL–01, at the
beginning of your comments. You may
also submit comments on the Internet at
https://dms.dot.gov. You may review the
public docket containing the proposal,
any comments received, and any final
disposition in person in the Dockets
Office between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal
holidays. The Docket Office (telephone
E:\FR\FM\11APP1.SGM
11APP1
Agencies
[Federal Register Volume 71, Number 69 (Tuesday, April 11, 2006)]
[Proposed Rules]
[Pages 18253-18254]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E6-5253]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-23249; Directorate Identifier 2005-NM-219-AD]
RIN 2120-AA64
Airworthiness Directives; Gulfstream Model GV-SP Series Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Proposed rule; withdrawal.
-----------------------------------------------------------------------
SUMMARY: The FAA withdraws a notice of proposed rulemaking (NPRM) that
proposed a new airworthiness directive (AD) for certain Gulfstream
Model GV-SP series airplanes. The proposed AD would have required an
inspection to determine the serial number of the anti-skid control unit
(ACU) in the right electronics equipment rack, and replacement of the
ACU with a new or serviceable ACU if necessary. Since the proposed AD
was issued, we have received new data that indicate the identified
unsafe condition has been corrected on all airplanes that would have
been affected by the NPRM, and on all ACUs in the affected range of
serial numbers. Accordingly, the proposed AD is withdrawn.
ADDRESSES: 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 U.S.
Department of Transportation, 400 Seventh Street, SW., Room PL-401,
Washington, DC. This docket number is FAA-2005-23249; the directorate
identifier for this docket is 2005-NM-219-AD.
FOR FURTHER INFORMATION CONTACT: Darby Mirocha, 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) 703-6095; fax (770) 703-
6097.
SUPPLEMENTARY INFORMATION:
Discussion
We proposed to amend part 39 of the Federal Aviation Regulations
(14 CFR part 39) with a notice of proposed rulemaking (NPRM) for a new
AD for certain Gulfstream Model GV-SP series airplanes. That NPRM was
published in
[[Page 18254]]
the Federal Register on December 9, 2005 (70 FR 73173). The NPRM would
have required an inspection to determine the serial number of the anti-
skid control unit (ACU) in the right electronics equipment rack, and
replacement of the ACU with a new or serviceable ACU if necessary. The
NPRM resulted from a report that an airplane temporarily lost normal
braking function during landing rollout on a pre-delivery flight. The
proposed actions were intended to prevent loss of normal braking
function, which could result in a runway overrun that could cause
injury to flightcrew or passengers or damage to the airplane.
Actions Since NPRM Was Issued
Since we issued the NPRM, Gulfstream Aerospace has provided data
that indicate the identified unsafe condition has been corrected on all
airplanes that would have been affected by the NPRM, and on all ACUs in
the affected range of serial numbers (S/Ns). Gulfstream Aerospace
therefore requests that we withdraw the NPRM. We agree with the
commenter.
Request To Incorporate by Reference (IBR) the Service Information
The Modification and Replacement Parts Association (MARPA) requests
that we either publish the relevant service information with the AD, or
IBR it with the NPRM. If we IBR rather than publish the relevant
service information, then MARPA further requests that we identify the
S/Ns of the defective ACUs in the AD. As justification, MARPA states
that parts purveyors and maintenance facilities cannot identify the
defective parts unless we specify them in the AD because they do not
possess the proprietary service information referenced in the NPRM. For
the same reason, MARPA states that those in the alternative parts
industry (operating under 14 CFR 21.303) also cannot identify any parts
manufacturer approval (PMA) parts equivalent to the defective ACUs.
MARPA asserts that there are many ACUs in its PMA database that also
may be affected by unsafe condition identified in the NPRM.
MARPA also comments on our practice of IBR and referencing
propriety service information. MARPA asserts that if we IBR proprietary
service information with a public document, such as an AD, then that
service information loses its protected status and becomes a public
document. Also, MARPA claims that IBR requires we provide a copy of the
relevant service information to the Director of the Federal Register
before the NPRM can be published. MARPA further states that: ``Merely
referencing a service document without incorporation thus becomes an
``end run'' around the publication requirement while still requiring
possession of a proprietary document in order to comply with the law.''
MARPA believes our practice of IBR is flawed legally where it is
impossible to comply with the requirements of an AD without first
obtaining the necessary propriety service information.
Although we acknowledge MARPA's comments, we do not agree with its
request, since the identified unsafe condition has been corrected on
all airplanes that would have been affected by the NPRM and on all ACUs
in the affected range of S/Ns. Those affected parts are ACUs having
part number 1159SCL501-1 and S/Ns 355 through 400 inclusive. The unsafe
condition identified in the NPRM was caused by the installation of
incorrect capacitors in the affected ACUs only. Since that NPRM
addresses a quality control issue limited to a range of S/Ns, we find
that the MARPA's statements regarding PMA equivalent parts are not
relevant to that particular NPRM.
We have one correction regarding MARPA's comments on our practice
of IBR and referencing propriety service information; we are required
to provide a copy of any relevant service information to the Director
of the Federal Register for publication of a final rule, not an NPRM.
We are currently reviewing our practice of referencing proprietary
service information. Once we have thoroughly examined all aspects of
this issue, and have made a final determination, we will consider
whether our current practice needs to be revised.
FAA's Conclusions
Upon further consideration, we have determined that the actions
that would have been required by the NPRM have already been
accomplished on all affected airplanes, and that the identified unsafe
condition has been corrected on all affected ACUs. Accordingly, the
NPRM is withdrawn.
Withdrawal of the NPRM does not preclude the FAA from issuing
another related action or commit the FAA to any course of action in the
future.
Regulatory Impact
Since this action only withdraws an NPRM, it is neither a proposed
nor a final rule and therefore is not covered under Executive Order
12866, the Regulatory Flexibility Act, or DOT Regulatory Policies and
Procedures (44 FR 11034, February 26, 1979).
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Safety.
The Withdrawal
Accordingly, we withdraw the NPRM, Docket No. FAA-2005-23249,
Directorate Identifier 2005-NM-219-AD, which was published in the
Federal Register on December 9, 2005 (70 FR 73173).
Issued in Renton, Washington, on March 31, 2006.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E6-5253 Filed 4-10-06; 8:45 am]
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