Airworthiness Directives; McDonnell Douglas Model DC-8-61, DC-8-61F, DC-8-63, DC-8-63F, DC-8-71F, and DC-8-73F Airplanes, 47043-47044 [E8-17743]
Download as PDF
Federal Register / Vol. 73, No. 157 / Wednesday, August 13, 2008 / Rules and Regulations
Diamond Aircraft Industries GmbH Work
Instruction WI–MSB–42–043, dated February
4, 2008; and Diamond Aircraft Industries
GmbH Drawing Number D60–2717–00–00,
dated January 24, 2008, for related
information.
Material Incorporated by Reference
(i) You must use Diamond Aircraft
Industries GmbH Mandatory Service Bulletin
No. MSB–42–043/1, dated April 3, 2008;
Diamond Aircraft Industries GmbH Work
Instruction WI–MSB–42–043, dated February
4, 2008; and Diamond Aircraft Industries
GmbH Drawing Number D60–2717–00–00,
dated January 24, 2008, 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 Diamond Aircraft Industries
GmbH, N.A. Otto-Stra+e 5, A–2700 Wiener
Neustadt; telephone: +43 2622 26700; fax:
+43 2622 26780; e-mail: office@diamondair.at.
(3) You may review copies at the FAA,
Central Region, Office of the Regional
Counsel, 901 Locust, Room 506, Kansas City,
Missouri 64106; 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 Kansas City, Missouri, on August
1, 2008.
James E. Jackson,
Acting Manager, Small Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E8–18205 Filed 8–12–08; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2008–0497; Directorate
Identifier 2007–NM–096–AD; Amendment
39–15629; AD 2008–16–11]
RIN 2120–AA64
Airworthiness Directives; McDonnell
Douglas Model DC–8–61, DC–8–61F,
DC–8–63, DC–8–63F, DC–8–71F, and
DC–8–73F Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
We are adopting a new
airworthiness directive (AD) for certain
McDonnell Douglas Model DC–8–61,
DC–8–61F, DC–8–63, DC–8–63F, DC–8–
71F, and DC–8–73F airplanes. For
certain airplanes, this AD requires nondestructive testing (NDT) to detect
hsrobinson on PROD1PC76 with RULES
SUMMARY:
VerDate Aug<31>2005
15:55 Aug 12, 2008
Jkt 214001
cracks of the door jamb corners of the
forward and aft service doors, and doing
applicable related investigative and
corrective actions. For certain other
airplanes, this AD requires inspecting
and repairing if necessary or replacing
previously repaired door jamb corners
with an applicable repair. This AD
results from reports of numerous cases
of cracks in the skin at the door jamb
corners of the forward and aft service
doors. We are issuing this AD to detect
and correct fatigue cracking of door
jamb corners of the forward and aft
service doors, which could adversely
affect the structural integrity of the
airplane.
DATES: This AD is effective September
17, 2008.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of September 17, 2008.
ADDRESSES: For service information
identified in this AD, contact Boeing
Commercial Airplanes, Long Beach
Division, 3855 Lakewood Boulevard,
Long Beach, California 90846, Attention:
Data and Service Management, Dept.
C1–L5A (D800–0024)
Examining the AD Docket
You may examine the AD docket on
the Internet at https://
www.regulations.gov; or in person at the
Docket Management Facility between 9
a.m. and 5 p.m., Monday through
Friday, except Federal holidays. The AD
docket contains this AD, the regulatory
evaluation, any comments received, and
other information. The address for the
Docket Office (telephone 800–647–5527)
is the Document Management Facility,
U.S. Department of Transportation,
Docket Operations, M–30, West
Building Ground Floor, Room W12–140,
1200 New Jersey Avenue, SE.,
Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT: Jon
Mowery, Aerospace Engineer, Airframe
Branch, ANM–120L, FAA, Los Angeles
Aircraft Certification Office, 3960
Paramount Boulevard, Lakewood,
California 90712–4137; telephone (562)
627–5322; fax (562) 627–5210.
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 to include an airworthiness
directive (AD) that would apply to
certain McDonnell Douglas Model DC–
8–61, DC–8–61F, DC–8–63, DC–8–63F,
DC–8–71F, and DC–8–73F airplanes.
That NPRM was published in the
Federal Register on May 6, 2008 (73 FR
24887). For certain airplanes, that
PO 00000
Frm 00017
Fmt 4700
Sfmt 4700
47043
NPRM proposed to require nondestructive testing (NDT) to detect
cracks of the door jamb corners of the
forward and aft service doors, and doing
applicable related investigative and
corrective actions. For certain other
airplanes, that NPRM proposed to
require inspecting and repairing if
necessary or replacing previously
repaired door jamb corners with an
applicable repair.
Comments
We gave the public the opportunity to
participate in developing this AD. We
received no comments on the NPRM or
on the determination of the cost to the
public.
Conclusion
We reviewed the relevant data and
determined that air safety and the
public interest require adopting the AD
as proposed.
Costs of Compliance
There are about 299 airplanes of the
affected design in the worldwide fleet.
This AD affects about 55 airplanes of
U.S. registry. The testing takes about 1
work hour per airplane, at an average
labor rate of $80 per work hour. Based
on these figures, the estimated cost of
the AD for U.S. operators is $4,400, or
$80 per airplane, per testing cycle.
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
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
E:\FR\FM\13AUR1.SGM
13AUR1
47044
Federal Register / Vol. 73, No. 157 / Wednesday, August 13, 2008 / Rules and Regulations
responsibilities among the various
levels of government.
For the reasons discussed above, I
certify that this AD:
(1) Is not a ‘‘significant regulatory
action’’ under Executive Order 12866,
(2) Is not a ‘‘significant rule’’ under
DOT Regulatory Policies and Procedures
(44 FR 11034, February 26, 1979), and
(3) Will not have a significant
economic impact, positive or negative,
on a substantial number of small entities
under the criteria of the Regulatory
Flexibility Act.
You can find our regulatory
evaluation and the estimated costs of
compliance 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.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new AD:
I
2008–16–11 McDonnell Douglas:
Amendment 39–15629. Docket No.
FAA–2008–0497; Directorate Identifier
2007–NM–096–AD.
Effective Date
(a) This airworthiness directive (AD) is
effective September 17, 2008.
Affected ADs
(b) As specified in paragraph (g) of this AD,
this AD affects certain requirements of AD
93–01–15, amendment 39–8469.
hsrobinson on PROD1PC76 with RULES
Applicability
(c) This AD applies to McDonnell Douglas
Model DC–8–61, DC–8–61F, DC–8–63, DC–
8–63F, DC–8–71F, and DC–8–73F airplanes,
certificated in any category; as identified in
Boeing Alert Service Bulletin DC8–53A082,
dated February 6, 2007.
Unsafe Condition
(d) This AD results from reports of
numerous cases of cracks in the skin at the
door jamb corners of forward and aft service
doors. We are issuing this AD to detect and
correct fatigue cracking of door jamb corners
of the forward and aft service doors, which
could adversely affect the structural integrity
of the airplane.
VerDate Aug<31>2005
15:55 Aug 12, 2008
Jkt 214001
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.
Testing, Inspecting, Repairing, and Related
Investigative and Corrective Actions
(f) At the applicable compliance time and
repeat intervals listed in Tables 1 through 5
inclusive of paragraph 1.E., ‘‘Compliance,’’ of
Boeing Alert Service Bulletin DC8–53A082,
dated February 6, 2007; except where ‘‘the
service bulletin’’ specifies a compliance time
after the date on the service bulletin, this AD
requires compliance within the specified
compliance time after the effective date of
this AD: Do the actions specified in
paragraph (f)(1), (f)(2), or (f)(3) of this AD, as
applicable.
(1) For airplanes identified as Group 1,
Configurations 1 and 2, in the service
bulletin: Do the testing and related
investigative and corrective actions by
accomplishing all the applicable actions
specified in the Accomplishment
Instructions of the service bulletin.
(2) For airplanes identified as Group 1,
Configuration 3, in the service bulletin:
Inspect and repair discrepancies in
accordance with a method approved by the
Manager, Los Angeles Aircraft Certification
Office (ACO), FAA.
(3) For airplanes identified as Group 1,
Configuration 4, in the service bulletin: Do
the actions specified in paragraph (f)(3)(i) or
(f)(3)(ii) of this AD.
(i) Repair door jamb corners of the service
door using a method approved in accordance
with the procedures specified in paragraph
(h) of this AD.
(ii) Replace the previously repaired door
jamb corners with an applicable repair in
accordance with the Accomplishment
Instructions of the service bulletin.
Compliance With Certain Requirements of
AD 93–01–15
(g) Accomplishment of the applicable
actions required by paragraph (f) of this AD
constitutes compliance with certain
requirements of AD 93–01–15, as it pertains
to the affected areas of principal structural
elements 53.08.039 and 53.08.040 of
McDonnell Douglas Report No. L26–011,
‘‘DC–8 Supplemental Inspection Document
(SID),’’ dated December 1985.
Alternative Methods of Compliance
(AMOCs)
(h)(1) The Manager, Los Angeles ACO, has
the authority to approve AMOCs for this AD,
if requested in accordance with the
procedures found in 14 CFR 39.19.
(2) To request a different method of
compliance or a different compliance time
for this AD, follow the procedures in 14 CFR
39.19. Before using any approved AMOC on
any airplane to which the AMOC applies,
notify your appropriate principal inspector
(PI) in the FAA Flight Standards District
Office (FSDO), or lacking a PI, your local
FSDO.
(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
PO 00000
Frm 00018
Fmt 4700
Sfmt 4700
Authorized Representative for the Boeing
Commercial Airplanes Delegation Option
Authorization Organization who has been
authorized by the Manager, Los Angeles
ACO, to make those findings. For a repair
method to be approved, the repair must meet
the certification basis of the airplane and 14
CFR 25.571, Amendment 45, and the
approval must specifically refer to this AD.
Material Incorporated by Reference
(i) You must use Boeing Alert Service
Bulletin DC8–53A082, dated February 6,
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 Boeing Commercial
Airplanes, Long Beach Division, 3855
Lakewood Boulevard, Long Beach, California
90846, Attention: Data and Service
Management, Dept. C1–L5A (D800–0024).
(3) You may review copies of the service
information incorporated by reference 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/
code_of_federal_regulations/
ibr_locations.html.
Issued in Renton, Washington, on July 23,
2008.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E8–17743 Filed 8–12–08; 8:45 am]
BILLING CODE 4910–13–P
RAILROAD RETIREMENT BOARD
20 CFR Part 295
RIN 3220–AB61
Payments Pursuant to Court Decree or
Court-Approved Property Settlement
Railroad Retirement Board.
Final rule.
AGENCY:
ACTION:
SUMMARY: The Railroad Retirement
Board (Board) amends its regulations
concerning partition of annuities
pursuant to a court decree or courtapproved property settlement in order
to incorporate provisions of the Pension
Protection Act of 2006, to make
corrections in the existing regulation,
and to update the regulation to reflect
changes in titles within the agency.
DATES: This rule will be effective August
13, 2008.
ADDRESSES: Beatrice Ezerski, Secretary
to the Board, Railroad Retirement Board,
844 N. Rush Street, Chicago, Illinois
60611–2092.
E:\FR\FM\13AUR1.SGM
13AUR1
Agencies
[Federal Register Volume 73, Number 157 (Wednesday, August 13, 2008)]
[Rules and Regulations]
[Pages 47043-47044]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E8-17743]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2008-0497; Directorate Identifier 2007-NM-096-AD;
Amendment 39-15629; AD 2008-16-11]
RIN 2120-AA64
Airworthiness Directives; McDonnell Douglas Model DC-8-61, DC-8-
61F, DC-8-63, DC-8-63F, DC-8-71F, and DC-8-73F Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for certain
McDonnell Douglas Model DC-8-61, DC-8-61F, DC-8-63, DC-8-63F, DC-8-71F,
and DC-8-73F airplanes. For certain airplanes, this AD requires non-
destructive testing (NDT) to detect cracks of the door jamb corners of
the forward and aft service doors, and doing applicable related
investigative and corrective actions. For certain other airplanes, this
AD requires inspecting and repairing if necessary or replacing
previously repaired door jamb corners with an applicable repair. This
AD results from reports of numerous cases of cracks in the skin at the
door jamb corners of the forward and aft service doors. We are issuing
this AD to detect and correct fatigue cracking of door jamb corners of
the forward and aft service doors, which could adversely affect the
structural integrity of the airplane.
DATES: This AD is effective September 17, 2008.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of September
17, 2008.
ADDRESSES: For service information identified in this AD, contact
Boeing Commercial Airplanes, Long Beach Division, 3855 Lakewood
Boulevard, Long Beach, California 90846, Attention: Data and Service
Management, Dept. C1-L5A (D800-0024)
Examining the AD Docket
You may examine the AD docket on the Internet at https://
www.regulations.gov; or in person at the Docket Management Facility
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The AD docket contains this AD, the regulatory evaluation,
any comments received, and other information. The address for the
Docket Office (telephone 800-647-5527) is the Document Management
Facility, U.S. Department of Transportation, Docket Operations, M-30,
West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue, SE.,
Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT: Jon Mowery, Aerospace Engineer,
Airframe Branch, ANM-120L, FAA, Los Angeles Aircraft Certification
Office, 3960 Paramount Boulevard, Lakewood, California 90712-4137;
telephone (562) 627-5322; fax (562) 627-5210.
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to include an airworthiness directive (AD) that would apply to
certain McDonnell Douglas Model DC-8-61, DC-8-61F, DC-8-63, DC-8-63F,
DC-8-71F, and DC-8-73F airplanes. That NPRM was published in the
Federal Register on May 6, 2008 (73 FR 24887). For certain airplanes,
that NPRM proposed to require non-destructive testing (NDT) to detect
cracks of the door jamb corners of the forward and aft service doors,
and doing applicable related investigative and corrective actions. For
certain other airplanes, that NPRM proposed to require inspecting and
repairing if necessary or replacing previously repaired door jamb
corners with an applicable repair.
Comments
We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM or on the determination of
the cost to the public.
Conclusion
We reviewed the relevant data and determined that air safety and
the public interest require adopting the AD as proposed.
Costs of Compliance
There are about 299 airplanes of the affected design in the
worldwide fleet. This AD affects about 55 airplanes of U.S. registry.
The testing takes about 1 work hour per airplane, at an average labor
rate of $80 per work hour. Based on these figures, the estimated cost
of the AD for U.S. operators is $4,400, or $80 per airplane, per
testing cycle.
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
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
[[Page 47044]]
responsibilities among the various levels of government.
For the reasons discussed above, I certify that this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Is not a ``significant rule'' under DOT Regulatory Policies and
Procedures (44 FR 11034, February 26, 1979), and
(3) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
You can find our regulatory evaluation and the estimated costs of
compliance 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:
2008-16-11 McDonnell Douglas: Amendment 39-15629. Docket No. FAA-
2008-0497; Directorate Identifier 2007-NM-096-AD.
Effective Date
(a) This airworthiness directive (AD) is effective September 17,
2008.
Affected ADs
(b) As specified in paragraph (g) of this AD, this AD affects
certain requirements of AD 93-01-15, amendment 39-8469.
Applicability
(c) This AD applies to McDonnell Douglas Model DC-8-61, DC-8-
61F, DC-8-63, DC-8-63F, DC-8-71F, and DC-8-73F airplanes,
certificated in any category; as identified in Boeing Alert Service
Bulletin DC8-53A082, dated February 6, 2007.
Unsafe Condition
(d) This AD results from reports of numerous cases of cracks in
the skin at the door jamb corners of forward and aft service doors.
We are issuing this AD to detect and correct fatigue cracking of
door jamb corners of the forward and aft service doors, which could
adversely affect the structural integrity of the airplane.
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.
Testing, Inspecting, Repairing, and Related Investigative and
Corrective Actions
(f) At the applicable compliance time and repeat intervals
listed in Tables 1 through 5 inclusive of paragraph 1.E.,
``Compliance,'' of Boeing Alert Service Bulletin DC8-53A082, dated
February 6, 2007; except where ``the service bulletin'' specifies a
compliance time after the date on the service bulletin, this AD
requires compliance within the specified compliance time after the
effective date of this AD: Do the actions specified in paragraph
(f)(1), (f)(2), or (f)(3) of this AD, as applicable.
(1) For airplanes identified as Group 1, Configurations 1 and 2,
in the service bulletin: Do the testing and related investigative
and corrective actions by accomplishing all the applicable actions
specified in the Accomplishment Instructions of the service
bulletin.
(2) For airplanes identified as Group 1, Configuration 3, in the
service bulletin: Inspect and repair discrepancies in accordance
with a method approved by the Manager, Los Angeles Aircraft
Certification Office (ACO), FAA.
(3) For airplanes identified as Group 1, Configuration 4, in the
service bulletin: Do the actions specified in paragraph (f)(3)(i) or
(f)(3)(ii) of this AD.
(i) Repair door jamb corners of the service door using a method
approved in accordance with the procedures specified in paragraph
(h) of this AD.
(ii) Replace the previously repaired door jamb corners with an
applicable repair in accordance with the Accomplishment Instructions
of the service bulletin.
Compliance With Certain Requirements of AD 93-01-15
(g) Accomplishment of the applicable actions required by
paragraph (f) of this AD constitutes compliance with certain
requirements of AD 93-01-15, as it pertains to the affected areas of
principal structural elements 53.08.039 and 53.08.040 of McDonnell
Douglas Report No. L26-011, ``DC-8 Supplemental Inspection Document
(SID),'' dated December 1985.
Alternative Methods of Compliance (AMOCs)
(h)(1) The Manager, Los Angeles ACO, has the authority to
approve AMOCs for this AD, if requested in accordance with the
procedures found in 14 CFR 39.19.
(2) To request a different method of compliance or a different
compliance time for this AD, follow the procedures in 14 CFR 39.19.
Before using any approved AMOC on any airplane to which the AMOC
applies, notify your appropriate principal inspector (PI) in the FAA
Flight Standards District Office (FSDO), or lacking a PI, your local
FSDO.
(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, Los Angeles ACO, to make those findings. For a
repair method to be approved, the repair must meet the certification
basis of the airplane and 14 CFR 25.571, Amendment 45, and the
approval must specifically refer to this AD.
Material Incorporated by Reference
(i) You must use Boeing Alert Service Bulletin DC8-53A082, dated
February 6, 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
Boeing Commercial Airplanes, Long Beach Division, 3855 Lakewood
Boulevard, Long Beach, California 90846, Attention: Data and Service
Management, Dept. C1-L5A (D800-0024).
(3) You may review copies of the service information
incorporated by reference 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/code_of_federal_
regulations/ibr_locations.html.
Issued in Renton, Washington, on July 23, 2008.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E8-17743 Filed 8-12-08; 8:45 am]
BILLING CODE 4910-13-P