Airworthiness Directives; McDonnell Douglas Corporation Model DC-8-31, DC-8-32, DC-8-33, DC-8-41, DC-8-42, and DC-8-43 Airplanes; Model DC-8-50 Series Airplanes; Model DC-8F-54 and DC-8F-55 Airplanes; Model DC-8-60 Series Airplanes; Model DC-8-60F Series Airplanes; Model DC-8-70 Series Airplanes; and Model DC-8-70F Series Airplanes, 61989-61993 [2010-25021]
Download as PDF
<![CDATA[
Federal Register / Vol. 75, No. 194 / Thursday, October 7, 2010 / Rules and Regulations
61989
TABLE 1—PREVIOUS SERVICE INFORMATION
Bombardier Service Bulletin—
Revision—
Dated—
8–32–166 .............................................................................................................................................
8–32–166 .............................................................................................................................................
84–32–57 .............................................................................................................................................
Original ....................
A ..............................
Original ....................
April 14, 2008.
January 29, 2009.
April 30, 2008.
FAA AD Differences
Note 1: This AD differs from the MCAI
and/or service information as follows: No
differences.
Other FAA AD Provisions
(i) The following provisions also apply to
this AD:
(1) Alternative Methods of Compliance
(AMOCs): The Manager, New York Aircraft
Certification Office, ANE–170, 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:
Program Manager, Continuing Operational
Safety, FAA, New York ACO, 1600 Stewart
Avenue, Suite 410, Westbury, New York,
11590; telephone 516–228–7300; fax 516–
794–5531. Before using any approved AMOC
on any airplane to which the AMOC applies,
notify your principal maintenance inspector
(PMI) or principal avionics inspector (PAI),
as appropriate, or lacking a principal
inspector, your local Flight Standards District
Office. The AMOC approval letter must
specifically reference this AD.
(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
(44 U.S.C. 3501 et seq.), the Office of
Management and Budget (OMB) has
approved the information collection
requirements and has assigned OMB Control
Number 2120–0056.
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Related Information
(j) Refer to MCAI Canadian Airworthiness
Directive CF–2009–46, dated December 14,
2009; Bombardier Service Bulletin 8–32–166,
Revision B, dated March 2, 2010; and
Bombardier Service Bulletin 84–32–57,
Revision A, dated June 15, 2009; for related
information.
Material Incorporated by Reference
(k) You must use Bombardier Service
Bulletin 84–32–57, Revision A, dated June
15, 2009; or Bombardier Service Bulletin 8–
32–166, Revision B, dated March 2, 2010; as
applicable; 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
ˆ
this AD, contact Bombardier, Inc., 400 Cote-
VerDate Mar<15>2010
17:58 Oct 06, 2010
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´
Vertu Road West, Dorval, Quebec H4S 1Y9,
Canada; telephone 514–855–5000; fax 514–
855–7401; e-mail
thd.qseries@aero.bombardier.com; Internet
https://www.bombardier.com.
(3) You may review copies of the service
information at the FAA, Transport Airplane
Directorate, 1601 Lind Avenue SW., Renton,
Washington. For information on the
availability of this material at the FAA, call
425–227–1221.
(4) You may also review copies of the
service information that is incorporated by
reference 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
September 23, 2010.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 2010–25016 Filed 10–6–10; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2010–0639; Directorate
Identifier 2009–NM–232–AD; Amendment
39–16463; AD 2010–21–03]
RIN 2120–AA64
Airworthiness Directives; McDonnell
Douglas Corporation Model DC–8–31,
DC–8–32, DC–8–33, DC–8–41, DC–8–
42, and DC–8–43 Airplanes; Model DC–
8–50 Series Airplanes; Model DC–8F–
54 and DC–8F–55 Airplanes; Model
DC–8–60 Series Airplanes; Model DC–
8–60F Series Airplanes; Model DC–8–
70 Series Airplanes; and Model DC–8–
70F Series Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
The FAA is superseding an
existing airworthiness directive (AD)
that applies to all of the McDonnell
Douglas Corporation airplanes
identified above. The existing AD
currently requires revising the
SUMMARY:
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maintenance program to incorporate
new airworthiness limitations for fuel
tank systems to satisfy Special Federal
Aviation Regulation No. 88
requirements. This new AD adds
requirements to revise the maintenance
program to incorporate specific Critical
Design Configuration Control
Limitations (CDCCL) information and
install fuel tank float switch in-line
fuses. This new AD also adds two
Airworthiness Limitations inspections
(ALIs). This AD results from a design
review of the fuel tank systems. We are
issuing this AD to prevent the potential
for ignition sources inside fuel tanks
caused by latent failures, alterations,
repairs, or maintenance actions, which,
in combination with flammable fuel
vapors, could result in a fuel tank
explosion and consequent loss of the
airplane.
This AD becomes effective
November 12, 2010.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in the AD
as of November 12, 2010.
On May 27, 2008 (73 FR 21523, April
22, 2008), the Director of the Federal
Register approved the incorporation by
reference of a certain other publication
listed in the AD.
ADDRESSES: For service information
identified in this AD, contact Boeing
Commercial Airplanes, Attention: Data
& Services Management, 3855
Lakewood Boulevard, MC D800–0019,
Long Beach, California 90846–0001;
telephone 206–544–5000, extension 2;
fax 206–766–5683; e-mail
dse.boecom@boeing.com; Internet
https://www.myboeingfleet.com.
DATES:
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,
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Federal Register / Vol. 75, No. 194 / Thursday, October 7, 2010 / Rules and Regulations
maintenance program. That NPRM also
proposed to add requirements to revise
the maintenance program to incorporate
specific Critical Design Configuration
Control Limitations (CDCCL)
information and install fuel tank float
switch in-line fuses. That NPRM also
proposed to add two Airworthiness
Limitations inspections (ALIs).
1200 New Jersey Avenue, SE.,
Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT:
Samuel Lee, Aerospace Engineer,
Propulsion Branch, ANM–140L, FAA,
Los Angeles Aircraft Certification
Office, 3960 Paramount Boulevard,
Lakewood, California 90712–4137;
telephone (562) 627–5262; fax (562)
627–5210.
SUPPLEMENTARY INFORMATION:
Discussion
The FAA issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that
supersedes AD 2008–09–04,
Amendment 39–15484 (73 FR 21523,
April 22, 2008). The existing AD applies
to all Model DC–8–31, DC–8–32, DC–8–
33, DC–8–41, DC–8–42, and DC–8–43
airplanes; Model DC–8–50 series
airplanes; Model DC–8F–54 and DC–
8F–55 airplanes; Model DC–8–60 series
airplanes; Model DC–8–60F series
airplanes; Model DC–8–70 series
airplanes; and Model DC–8–70F series
airplanes. That NPRM was published in
the Federal Register on June 25, 2010
(75 FR 36298). That NPRM proposed to
continue to require revising the
Relevant Service Information
We reviewed Boeing DC–8 Special
Compliance Item Report, MDC–
02K9030, Revision D, dated June 9,
2010. This service information does not
add any additional work. We have
revised paragraphs (j), (m), and (n) of
this AD to refer to this report.
Comments
We provided the public the
opportunity to participate in the
development of this AD. No comments
have been received on the NPRM or on
the determination of the cost to the
public.
Change to Paragraph Reference
We revised paragraph (l) of this AD to
correct a typographical error that
appeared in the NPRM. In paragraph (l)
of the NPRM, we inadvertently referred
to ‘‘paragraph (k)’’ instead of ‘‘paragraph
(j)’’ of the AD. Paragraph (l) of this final
rule correctly references paragraph (j) of
this AD.
Explanation of Additional Change to
NPRM
We also clarified the airplanes
affected by paragraph (k) of this AD by
referring to the airplanes identified in
Boeing Service Bulletin DC8–28–090,
dated October 9, 2009. Airplanes not
listed in the effectivity of Boeing Service
Bulletin DC8–28–090, dated October 9,
2009, are not required to do the
installation required by paragraph (k) of
this AD.
Conclusion
We have carefully reviewed the
available data and determined that air
safety and the public interest require
adopting the AD with the changes
mentioned previously.
Costs of Compliance
There are about 125 airplanes of the
affected design in the worldwide fleet.
The following table provides the
estimated costs for U.S. operators to
comply with this AD.
ESTIMATED COSTS
Average
labor rate
per hour
Revising the Maintenance Program (required by AD 2008–09–04).
Revising the Airworthiness Limitation
Section (new action).
Installing fuses (new action) .................
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Work hours
1 ............................
$85
$0
$85 ........................
125
$10,625.
1 ............................
85
0
$85 ........................
125
$10,625.
Up to 35 hours .....
85
0
Up to $2,975 .........
125
Up to $371,875.
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.
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Parts
Cost per airplane
Number of
U.S.-registered
airplanes
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 this AD:
(1) Is not a ‘‘significant regulatory
action’’ under Executive Order 12866;
(2) Is not a ‘‘significant rule’’ under
DOT Regulatory Policies and Procedures
(44 FR 11034, February 26, 1979); and
(3) Will not have a significant
economic impact, positive or negative,
on a substantial number of small entities
under the criteria of the Regulatory
Flexibility Act.
We prepared a regulatory evaluation
of the estimated costs to comply with
PO 00000
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Fmt 4700
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Fleet cost
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:
■
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.
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Federal Register / Vol. 75, No. 194 / Thursday, October 7, 2010 / Rules and Regulations
§ 39.13
[Amended]
2. The Federal Aviation
Administration (FAA) amends § 39.13
by removing Amendment 39–15484 (73
FR 21523, April 22, 2008) and by adding
the following new airworthiness
directive (AD):
■
2010–21–03 McDonnell Douglas
Corporation: Amendment 39–16463.
Docket No. FAA–2010–0639; Directorate
Identifier 2009–NM–232–AD.
Effective Date
(a) This AD becomes effective November
12, 2010.
Affected ADs
(b) This AD supersedes AD 2008–09–04,
Amendment 39–15484.
Applicability
(c) This AD applies to all McDonnell
Douglas Model DC–8–31, DC–8–32, DC–8–
33, DC–8–41, DC–8–42, and DC–8–43
airplanes; Model DC–8–51, DC–8–52, DC–8–
53, and DC–8–55 airplanes; Model DC–8F–54
and DC–8F–55 airplanes; Model DC–8–61,
DC–8–62, and DC–8–63 airplanes; Model
DC–8–61F, DC–8–62F, and DC–8–63F
airplanes; Model DC–8–71, DC–8–72, and
DC–8–73 airplanes; and Model DC–8–71F,
DC–8–72F, and DC–8–73F airplanes;
certificated in any category.
Note 1: This AD requires revisions to
certain operator maintenance documents to
include new inspections. Compliance with
these inspections is required by 14 CFR
91.403(c). For airplanes that have been
previously modified, altered, or repaired in
the areas addressed by these inspections, the
operator may not be able to accomplish the
inspections described in the revisions. In this
situation, to comply with 14 CFR 91.403(c),
the operator must request approval for an
alternative method of compliance (AMOC) in
accordance with paragraph (o) of this AD.
The request should include a description of
changes to the required inspections that will
ensure the continued operational safety of
the airplane.
Subject
(d) Air Transport Association (ATA) of
America Code 28: Fuel.
srobinson on DSKHWCL6B1PROD with RULES
Unsafe Condition
(e) This AD results from a design review
of the fuel tank systems. The Federal
Aviation Administration is issuing this AD to
prevent the potential for ignition sources
inside fuel tanks caused by latent failures,
alterations, repairs, or maintenance actions,
which, in combination with flammable fuel
vapors, could result in a fuel tank explosion
and consequent loss of the airplane.
Compliance
(f) You are responsible for having the
actions required by this AD performed within
the compliance times specified, unless the
actions have already been done.
Restatement of Requirements of AD 2008–
09–04, With Revised Compliance Method
Revise the Maintenance Program
(g) Before December 16, 2008, revise the
maintenance program to incorporate the
information specified in Appendixes B, C,
and D of the Boeing DC–8 Special
Compliance Item Report, MDC–02K9030,
Revision A, dated August 8, 2006.
No Reporting Requirement
(h) Although the Boeing DC–8 Special
Compliance Item Report, MDC–02K9030,
Revision A, dated August 8, 2006, specifies
to submit certain information to the
manufacturer, this AD does not require that
action.
No Alternative Inspections, Inspection
Intervals, or Critical Design Configuration
Control Limitations (CDCCLs)
(i) Except as provided by paragraph (m) of
this AD, after accomplishing the applicable
actions specified in paragraph (g) of this AD,
no alternative inspections, inspection
intervals, or CDCCLs may be used unless the
inspections, intervals, or CDCCLs are
approved as an AMOC in accordance with
the procedures specified in paragraph (o) of
this AD.
New Requirements of This AD
Revise the Maintenance Program
(j) Within 30 days after the effective date
of this AD, revise the maintenance program
to incorporate the information required by
paragraphs (j)(1), (j)(2), and (j)(3) of this AD.
(1) CDCCL 20–10, ‘‘DC–8 Float Switch
Circuit’’ in Appendix B of Boeing DC–8
Special Compliance Item Report, MDC–
02K9030, Revision C, dated January 5, 2010;
or Revision D, dated June 9, 2010.
(2) ALI 30–1 ‘‘DC–8 Pneumatic System
Decay Check’’ in Appendix C of Boeing DC–
8 Special Compliance Item Report, MDC–
02K9030, Revision C, dated January 5, 2010;
or Revision D, dated June 9, 2010.
(3) ALI 28–1, ‘‘DC–8 Alternate and Center
Auxiliary Tank Fuel Pump Control Systems
Check,’’ in Appendix C of Boeing DC–8
Special Compliance Item Report, MDC–
02K9030, Revision C, dated January 5, 2010;
or Revision D, dated June 9, 2010.
Install the In-Line Fuses
(k) For airplanes identified in Boeing
Service Bulletin DC8–28–090, dated October
9, 2009: Within 60 months after the effective
date of this AD, install the fuel tank float
switch in-line fuses in the leading edges of
the front spars of the left and right wings, in
accordance with the Accomplishment
Instructions of Boeing Service Bulletin DC8–
28–090, dated October 9, 2009.
No Alternative Inspections, Inspection
Intervals, or Critical Design Configuration
Control Limitations (CDCCLs)
(l) After accomplishing the actions
specified in paragraph (j) of this AD, no
alternative inspections, inspection intervals,
or CDCCLs may be used unless the
inspections, intervals, or CDCCLs are
approved as an AMOC in accordance with
the procedures specified in paragraph (o) of
this AD.
(m) Revising the maintenance program to
incorporate the information specified in
Appendixes B, C, and D of the Boeing DC–
8 Special Compliance Item Report, MDC–
02K9030, Revision B, dated July 23, 2009;
Revision C, dated January 5, 2010; or
Revision D, dated June 9, 2010; is acceptable
for compliance with the actions specified in
paragraph (g) of this AD.
No Reporting Requirement
(n) Although the Boeing DC–8 Special
Compliance Item Report, MDC–02K9030,
Revision B, dated July 23, 2009; Revision C,
dated January 5, 2010; and Revision D, dated
June 9, 2010; specify to submit certain
information to the manufacturer, this AD
does not require that action.
Alternative Methods of Compliance
(AMOCs)
(o)(1) The Manager, Los Angeles Aircraft
Certification Office (ACO), 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:
Samuel Lee, Aerospace Engineer, Propulsion
Branch, ANM–140L, FAA, Los Angeles
Aircraft Certification Office (ACO), 3960
Paramount Boulevard, Lakewood, California
90712–4137; telephone (562) 627–5262; fax
(562) 627–5210.
(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 principal maintenance inspector
(PMI) or principal avionics inspector (PAI),
as appropriate, or lacking a principal
inspector, your local Flight Standards District
Office. The AMOC approval letter must
specifically reference this AD.
Material Incorporated by Reference
(p) You must use the applicable service
information contained in Table 1 of this AD
to do the actions required by this AD, unless
the AD specifies otherwise.
TABLE 1—ALL MATERIAL INCORPORATED BY REFERENCE
Document
Boeing
Boeing
Boeing
Boeing
DC–8
DC–8
DC–8
DC–8
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Special
Special
Special
Special
Compliance
Compliance
Compliance
Compliance
17:58 Oct 06, 2010
Item
Item
Item
Item
Report,
Report,
Report,
Report,
Jkt 223001
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MDC–02K9030
MDC–02K9030
MDC–02K9030
MDC–02K9030
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...................................................
...................................................
...................................................
...................................................
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A
B
C
D
................................
................................
................................
................................
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07OCR1
Date
August 8, 2006.
July 23, 2009.
January 5, 2010.
June 9, 2010.
61992
Federal Register / Vol. 75, No. 194 / Thursday, October 7, 2010 / Rules and Regulations
TABLE 1—ALL MATERIAL INCORPORATED BY REFERENCE—Continued
Document
Revision
Boeing Service Bulletin DC8–28–090 .............................................................................................
Original ......................
Boeing DC–8 Special Compliance Item
Report, MDC–02K9030, Revision B, dated
Date
October 9, 2009.
July 23, 2009, contains the following effective
pages:
LIST OF EFFECTIVE PAGES
Page title/description
Page number(s)
Revision number
Report Title Page ..................................
Index of Page Changes .........................
Table of Contents ..................................
Discussion .............................................
Appendix A ............................................
Appendix B ............................................
None shown .........................................
ii, iii .......................................................
iv, v .......................................................
1 ...........................................................
A1–A4 ...................................................
B1, B3, B4, B6–B12 .............................
B2, B5, B13–B24 .................................
C1–C5 ..................................................
C6–C10 ................................................
D1 .........................................................
B ...........................................................
B ...........................................................
B ...........................................................
New ......................................................
New ......................................................
New ......................................................
B ...........................................................
New ......................................................
B ...........................................................
New ......................................................
Appendix C ............................................
Appendix D ............................................
Boeing DC–8 Special Compliance Item
Report, MDC–02K9030, Revision C, dated
Date shown on
Page(s)
July 23, 2009.
None shown.*
None shown.*
None shown.*
None shown.*
None shown.*
None shown.*
None shown.*
None shown.*
None shown.*
January 5, 2010, contains the following
effective pages:
LIST OF EFFECTIVE PAGES
Page title/description
Page number(s)
Revision number
Report Title Page ..................................
Index of Page Changes .........................
Table of Contents ..................................
Discussion .............................................
Appendix A ............................................
None shown .........................................
ii, iii .......................................................
iv, v .......................................................
1 ...........................................................
A1–A3 ...................................................
A4–A25 .................................................
B1, B3, B4, B6–B12 .............................
B2, B5, B13–B24 .................................
C1–C5 ..................................................
C6–C10 ................................................
C11–C14 ..............................................
D1 .........................................................
C ...........................................................
C ...........................................................
C ...........................................................
C ...........................................................
New ......................................................
C ...........................................................
New ......................................................
B ...........................................................
New ......................................................
B ...........................................................
C ...........................................................
New ......................................................
Appendix B ............................................
Appendix C ............................................
Appendix D ............................................
Boeing DC–8 Special Compliance Item
Report, MDC–02K9030, Revision D, dated
Date shown on
page(s)
January 5, 2010.
None shown.*
None shown.*
None shown.*
None shown.*
None shown.*
None shown.*
None shown.*
None shown.*
None shown.*
None shown.*
None shown.*
June 9, 2010, contains the following effective
pages:
LIST OF EFFECTIVE PAGES
Page title/description
Page number(s)
Revision number
Report Title Page ..................................
Attachment A .........................................
Index of Page Changes .........................
None shown .........................................
None shown .........................................
ii ............................................................
iii ...........................................................
iv, v .......................................................
1 ...........................................................
A1–A3 ...................................................
A4–A25 .................................................
B1, B3, B6, B7, B9, B12 ......................
B2, B13–B24 ........................................
B4, B5, B8, B10, B11 ...........................
C1–C5 ..................................................
C6–C10 ................................................
C11–C14 ..............................................
D1 .........................................................
D ...........................................................
None shown .........................................
B ...........................................................
C ...........................................................
C ...........................................................
C ...........................................................
New ......................................................
C ...........................................................
New ......................................................
B ...........................................................
D ...........................................................
New ......................................................
B ...........................................................
C ...........................................................
New ......................................................
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Table of Contents ..................................
Discussion .............................................
Appendix A ............................................
Appendix B ............................................
Appendix C ............................................
Appendix D ............................................
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Date shown on
page(s)
June 9, 2010.
June 22, 2010.
None shown.*
None shown.*
None shown.*
None shown.*
None shown.*
None shown.*
None shown.*
None shown.*
None shown.*
None shown.*
None shown.*
None shown.*
None shown.*
61993
Federal Register / Vol. 75, No. 194 / Thursday, October 7, 2010 / Rules and Regulations
(* The revision date of these documents is
shown only on the title page of these
documents.)
(1) The Director of the Federal Register
approved the incorporation by reference of
the service information contained in Table 2
of this AD under 5 U.S.C. 552(a) and 1 CFR
part 51.
TABLE 2—NEW MATERIAL INCORPORATED BY REFERENCE
Document
Boeing
Boeing
Boeing
Boeing
DC–8 Special Compliance Item Report, MDC–02K9030 ...................................................
DC–8 Special Compliance Item Report, MDC–02K9030 ...................................................
DC–8 Special Compliance Item Report, MDC–02K9030 ...................................................
Service Bulletin DC8–28–090 .............................................................................................
(2) The Director of the Federal Register
previously approved the incorporation by
reference of Boeing DC–8 Special
Compliance Item Report, MDC–02K9030,
Revision A, dated August 8, 2006, on May 27,
2008 (73 FR 21523, April 22, 2008).
(3) For service information identified in
this AD, contact Boeing Commercial
Airplanes, Attention: Data & Services
Management, 3855 Lakewood Boulevard, MC
D800–0019, Long Beach, California 90846–
0001; telephone 206–544–5000, extension 2;
fax 206–766–5683; e-mail
dse.boecom@boeing.com; Internet https://
www.myboeingfleet.com.
(4) You may review copies of the service
information at the FAA, Transport Airplane
Directorate, 1601 Lind Avenue, SW., Renton,
Washington. For information on the
availability of this material at the FAA, call
425–227–1221.
(5) You may also review copies of the
service information that is incorporated by
reference 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
September 23, 2010.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 2010–25021 Filed 10–6–10; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 71
[Docket No. FAA–2010–0808; Airspace
Docket No. 10–AWP–14]
RIN 2120–AA66
Amendment of Class E Airspace;
Kwajalein Island, Marshall Islands, RMI
srobinson on DSKHWCL6B1PROD with RULES
Revision
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule, technical
amendment.
AGENCY:
This action removes the
reference to the Kwajalein Tactacial Air
SUMMARY:
VerDate Mar<15>2010
17:58 Oct 06, 2010
Jkt 223001
Navigation (TACAN) System from the
legal description of the Class E airspace
areas for Kwajalein Island, Bucholz
AAF, Marshall Islands, RMI. The U.S.
Army notified the FAA that the
Kwajalein TACAN was
decommissioned. This action corrects
the legal descriptions for the Class E
airspace areas in the vicinity of the
Marshall Islands.
DATES: Effective date 0901 UTC, January
13, 2011. The Director of the Federal
Register approves this incorporation by
reference action under 1 CFR part 51,
subject to the annual revision of FAA
Order 7400.9 and publication of
conforming amendments.
FOR FURTHER INFORMATION CONTACT: Ken
McElroy, Airspace and Rules Group,
Office of System Operations Airspace
and AIM, Federal Aviation
Administration, 800 Independence
Avenue, SW., Washington, DC 20591;
telephone: (202) 267–8783.
SUPPLEMENTARY INFORMATION:
The Rule
This action amends Title 14 Code of
Federal Regulations (14 CFR) part 71 by
removing the reference to the Kwajalein
TACAN, as it has been
decommissioned, from the legal
description of Class E airspace
designated as an extension to a Class D
surface area, and Class E airspace areas
extending upward from 700 feet or more
above the surface of the earth at
Kwajalein Island, Bucholz AAF,
Marshall Islands, RMI. Therefore, notice
and public procedures under 5 U.S.C.
553(b) are unnecessary.
Class E airspace designations are
published in paragraphs 6004 and 6005
of FAA Order 7400.9U signed August
18, 2010, and effective September 15,
2010, which is incorporated by
reference in 14 CFR 71.1. The Class E
airspace designations listed in this
document will be published
subsequently in the Order.
The FAA has determined that this
regulation only involves an established
body of technical regulations for which
frequent and routine amendments are
necessary to keep them operationally
PO 00000
Frm 00019
Fmt 4700
Sfmt 4700
B ................................
C ................................
D ................................
Original ......................
Date
July 23, 2009.
January 5, 2010.
June 9, 2010.
October 9, 2009.
current. Therefore, this regulation: (1) Is
not a ‘‘significant regulatory action’’
under Executive Order 12866; (2) is not
a ‘‘significant rule’’ under Department of
Transportation (DOT) Regulatory
Policies and Procedures (44 FR 11034;
February 26, 1979); and (3) does not
warrant preparation of a regulatory
evaluation as the anticipated impact is
so minimal. Since this is a routine
matter that will only affect air traffic
procedures and air navigation, it is
certified that this rule, when
promulgated, will not have a significant
economic impact on a substantial
number of small entities under the
criteria of the Regulatory Flexibility Act.
The FAA’s authority to issue rules
regarding aviation safety is found in
Title 49 of the United States Code.
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.
This rulemaking is promulgated
under the authority described in subtitle
VII, part A, subpart I, section 40103.
Under that section, the FAA is charged
with prescribing regulations to assign
the use of the airspace necessary to
ensure the safety of aircraft and the
efficient use of airspace. This regulation
is within the scope of that authority as
it amends Class E airspace at Kwajalein
Island, Marshall Island, RMI.
Environmental Review
The FAA has determined that this
action qualifies for categorical exclusion
under the National Environmental
Policy Act in accordance with 311a.,
FAA Order 1050.1E, ‘‘Environmental
Impacts: Policies and Procedures.’’ This
airspace action is not expected to cause
any potentially significant
environmental impacts, and no
extraordinary circumstances exist that
warrant preparation of an
environmental assessment.
List of Subjects in 14 CFR Part 71
Airspace, Incorporation by reference,
Navigation (air).
E:\FR\FM\07OCR1.SGM
07OCR1
]]>Agencies
[Federal Register Volume 75, Number 194 (Thursday, October 7, 2010)]
[Rules and Regulations]
[Pages 61989-61993]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2010-25021]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2010-0639; Directorate Identifier 2009-NM-232-AD;
Amendment 39-16463; AD 2010-21-03]
RIN 2120-AA64
Airworthiness Directives; McDonnell Douglas Corporation Model DC-
8-31, DC-8-32, DC-8-33, DC-8-41, DC-8-42, and DC-8-43 Airplanes; Model
DC-8-50 Series Airplanes; Model DC-8F-54 and DC-8F-55 Airplanes; Model
DC-8-60 Series Airplanes; Model DC-8-60F Series Airplanes; Model DC-8-
70 Series Airplanes; and Model DC-8-70F Series Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is superseding an existing airworthiness directive
(AD) that applies to all of the McDonnell Douglas Corporation airplanes
identified above. The existing AD currently requires revising the
maintenance program to incorporate new airworthiness limitations for
fuel tank systems to satisfy Special Federal Aviation Regulation No. 88
requirements. This new AD adds requirements to revise the maintenance
program to incorporate specific Critical Design Configuration Control
Limitations (CDCCL) information and install fuel tank float switch in-
line fuses. This new AD also adds two Airworthiness Limitations
inspections (ALIs). This AD results from a design review of the fuel
tank systems. We are issuing this AD to prevent the potential for
ignition sources inside fuel tanks caused by latent failures,
alterations, repairs, or maintenance actions, which, in combination
with flammable fuel vapors, could result in a fuel tank explosion and
consequent loss of the airplane.
DATES: This AD becomes effective November 12, 2010.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in the AD as of November 12,
2010.
On May 27, 2008 (73 FR 21523, April 22, 2008), the Director of the
Federal Register approved the incorporation by reference of a certain
other publication listed in the AD.
ADDRESSES: For service information identified in this AD, contact
Boeing Commercial Airplanes, Attention: Data & Services Management,
3855 Lakewood Boulevard, MC D800-0019, Long Beach, California 90846-
0001; telephone 206-544-5000, extension 2; fax 206-766-5683; e-mail
dse.boecom@boeing.com; Internet https://www.myboeingfleet.com.
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,
[[Page 61990]]
1200 New Jersey Avenue, SE., Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT: Samuel Lee, Aerospace Engineer,
Propulsion Branch, ANM-140L, FAA, Los Angeles Aircraft Certification
Office, 3960 Paramount Boulevard, Lakewood, California 90712-4137;
telephone (562) 627-5262; fax (562) 627-5210.
SUPPLEMENTARY INFORMATION:
Discussion
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to include an AD that supersedes AD 2008-09-04, Amendment
39-15484 (73 FR 21523, April 22, 2008). The existing AD applies to all
Model DC-8-31, DC-8-32, DC-8-33, DC-8-41, DC-8-42, and DC-8-43
airplanes; Model DC-8-50 series airplanes; Model DC-8F-54 and DC-8F-55
airplanes; Model DC-8-60 series airplanes; Model DC-8-60F series
airplanes; Model DC-8-70 series airplanes; and Model DC-8-70F series
airplanes. That NPRM was published in the Federal Register on June 25,
2010 (75 FR 36298). That NPRM proposed to continue to require revising
the maintenance program. That NPRM also proposed to add requirements to
revise the maintenance program to incorporate specific Critical Design
Configuration Control Limitations (CDCCL) information and install fuel
tank float switch in-line fuses. That NPRM also proposed to add two
Airworthiness Limitations inspections (ALIs).
Relevant Service Information
We reviewed Boeing DC-8 Special Compliance Item Report, MDC-
02K9030, Revision D, dated June 9, 2010. This service information does
not add any additional work. We have revised paragraphs (j), (m), and
(n) of this AD to refer to this report.
Comments
We provided the public the opportunity to participate in the
development of this AD. No comments have been received on the NPRM or
on the determination of the cost to the public.
Change to Paragraph Reference
We revised paragraph (l) of this AD to correct a typographical
error that appeared in the NPRM. In paragraph (l) of the NPRM, we
inadvertently referred to ``paragraph (k)'' instead of ``paragraph
(j)'' of the AD. Paragraph (l) of this final rule correctly references
paragraph (j) of this AD.
Explanation of Additional Change to NPRM
We also clarified the airplanes affected by paragraph (k) of this
AD by referring to the airplanes identified in Boeing Service Bulletin
DC8-28-090, dated October 9, 2009. Airplanes not listed in the
effectivity of Boeing Service Bulletin DC8-28-090, dated October 9,
2009, are not required to do the installation required by paragraph (k)
of this AD.
Conclusion
We have carefully reviewed the available data and determined that
air safety and the public interest require adopting the AD with the
changes mentioned previously.
Costs of Compliance
There are about 125 airplanes of the affected design in the
worldwide fleet. The following table provides the estimated costs for
U.S. operators to comply with this AD.
Estimated Costs
--------------------------------------------------------------------------------------------------------------------------------------------------------
Average Number of U.S.-
Action Work hours labor rate Parts Cost per airplane registered Fleet cost
per hour airplanes
--------------------------------------------------------------------------------------------------------------------------------------------------------
Revising the Maintenance Program 1..................... $85 $0 $85................... 125 $10,625.
(required by AD 2008-09-04).
Revising the Airworthiness 1..................... 85 0 $85................... 125 $10,625.
Limitation Section (new action).
Installing fuses (new action)....... Up to 35 hours........ 85 0 Up to $2,975.......... 125 Up to $371,875.
--------------------------------------------------------------------------------------------------------------------------------------------------------
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 this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866;
(2) Is not a ``significant rule'' under DOT Regulatory Policies and
Procedures (44 FR 11034, February 26, 1979); and
(3) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
We prepared a regulatory evaluation of the estimated costs to
comply with this AD and placed it in the AD docket. 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.
[[Page 61991]]
Sec. 39.13 [Amended]
0
2. The Federal Aviation Administration (FAA) amends Sec. 39.13 by
removing Amendment 39-15484 (73 FR 21523, April 22, 2008) and by adding
the following new airworthiness directive (AD):
2010-21-03 McDonnell Douglas Corporation: Amendment 39-16463. Docket
No. FAA-2010-0639; Directorate Identifier 2009-NM-232-AD.
Effective Date
(a) This AD becomes effective November 12, 2010.
Affected ADs
(b) This AD supersedes AD 2008-09-04, Amendment 39-15484.
Applicability
(c) This AD applies to all McDonnell Douglas Model DC-8-31, DC-
8-32, DC-8-33, DC-8-41, DC-8-42, and DC-8-43 airplanes; Model DC-8-
51, DC-8-52, DC-8-53, and DC-8-55 airplanes; Model DC-8F-54 and DC-
8F-55 airplanes; Model DC-8-61, DC-8-62, and DC-8-63 airplanes;
Model DC-8-61F, DC-8-62F, and DC-8-63F airplanes; Model DC-8-71, DC-
8-72, and DC-8-73 airplanes; and Model DC-8-71F, DC-8-72F, and DC-8-
73F airplanes; certificated in any category.
Note 1: This AD requires revisions to certain operator
maintenance documents to include new inspections. Compliance with
these inspections is required by 14 CFR 91.403(c). For airplanes
that have been previously modified, altered, or repaired in the
areas addressed by these inspections, the operator may not be able
to accomplish the inspections described in the revisions. In this
situation, to comply with 14 CFR 91.403(c), the operator must
request approval for an alternative method of compliance (AMOC) in
accordance with paragraph (o) of this AD. The request should include
a description of changes to the required inspections that will
ensure the continued operational safety of the airplane.
Subject
(d) Air Transport Association (ATA) of America Code 28: Fuel.
Unsafe Condition
(e) This AD results from a design review of the fuel tank
systems. The Federal Aviation Administration is issuing this AD to
prevent the potential for ignition sources inside fuel tanks caused
by latent failures, alterations, repairs, or maintenance actions,
which, in combination with flammable fuel vapors, could result in a
fuel tank explosion and consequent loss of the airplane.
Compliance
(f) You are responsible for having the actions required by this
AD performed within the compliance times specified, unless the
actions have already been done.
Restatement of Requirements of AD 2008-09-04, With Revised Compliance
Method
Revise the Maintenance Program
(g) Before December 16, 2008, revise the maintenance program to
incorporate the information specified in Appendixes B, C, and D of
the Boeing DC-8 Special Compliance Item Report, MDC-02K9030,
Revision A, dated August 8, 2006.
No Reporting Requirement
(h) Although the Boeing DC-8 Special Compliance Item Report,
MDC-02K9030, Revision A, dated August 8, 2006, specifies to submit
certain information to the manufacturer, this AD does not require
that action.
No Alternative Inspections, Inspection Intervals, or Critical Design
Configuration Control Limitations (CDCCLs)
(i) Except as provided by paragraph (m) of this AD, after
accomplishing the applicable actions specified in paragraph (g) of
this AD, no alternative inspections, inspection intervals, or CDCCLs
may be used unless the inspections, intervals, or CDCCLs are
approved as an AMOC in accordance with the procedures specified in
paragraph (o) of this AD.
New Requirements of This AD
Revise the Maintenance Program
(j) Within 30 days after the effective date of this AD, revise
the maintenance program to incorporate the information required by
paragraphs (j)(1), (j)(2), and (j)(3) of this AD.
(1) CDCCL 20-10, ``DC-8 Float Switch Circuit'' in Appendix B of
Boeing DC-8 Special Compliance Item Report, MDC-02K9030, Revision C,
dated January 5, 2010; or Revision D, dated June 9, 2010.
(2) ALI 30-1 ``DC-8 Pneumatic System Decay Check'' in Appendix C
of Boeing DC-8 Special Compliance Item Report, MDC-02K9030, Revision
C, dated January 5, 2010; or Revision D, dated June 9, 2010.
(3) ALI 28-1, ``DC-8 Alternate and Center Auxiliary Tank Fuel
Pump Control Systems Check,'' in Appendix C of Boeing DC-8 Special
Compliance Item Report, MDC-02K9030, Revision C, dated January 5,
2010; or Revision D, dated June 9, 2010.
Install the In-Line Fuses
(k) For airplanes identified in Boeing Service Bulletin DC8-28-
090, dated October 9, 2009: Within 60 months after the effective
date of this AD, install the fuel tank float switch in-line fuses in
the leading edges of the front spars of the left and right wings, in
accordance with the Accomplishment Instructions of Boeing Service
Bulletin DC8-28-090, dated October 9, 2009.
No Alternative Inspections, Inspection Intervals, or Critical Design
Configuration Control Limitations (CDCCLs)
(l) After accomplishing the actions specified in paragraph (j)
of this AD, no alternative inspections, inspection intervals, or
CDCCLs may be used unless the inspections, intervals, or CDCCLs are
approved as an AMOC in accordance with the procedures specified in
paragraph (o) of this AD.
(m) Revising the maintenance program to incorporate the
information specified in Appendixes B, C, and D of the Boeing DC-8
Special Compliance Item Report, MDC-02K9030, Revision B, dated July
23, 2009; Revision C, dated January 5, 2010; or Revision D, dated
June 9, 2010; is acceptable for compliance with the actions
specified in paragraph (g) of this AD.
No Reporting Requirement
(n) Although the Boeing DC-8 Special Compliance Item Report,
MDC-02K9030, Revision B, dated July 23, 2009; Revision C, dated
January 5, 2010; and Revision D, dated June 9, 2010; specify to
submit certain information to the manufacturer, this AD does not
require that action.
Alternative Methods of Compliance (AMOCs)
(o)(1) The Manager, Los Angeles Aircraft Certification Office
(ACO), 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: Samuel Lee, Aerospace Engineer, Propulsion
Branch, ANM-140L, FAA, Los Angeles Aircraft Certification Office
(ACO), 3960 Paramount Boulevard, Lakewood, California 90712-4137;
telephone (562) 627-5262; fax (562) 627-5210.
(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 principal maintenance inspector (PMI) or
principal avionics inspector (PAI), as appropriate, or lacking a
principal inspector, your local Flight Standards District Office.
The AMOC approval letter must specifically reference this AD.
Material Incorporated by Reference
(p) You must use the applicable service information contained in
Table 1 of this AD to do the actions required by this AD, unless the
AD specifies otherwise.
Table 1--All Material Incorporated by Reference
----------------------------------------------------------------------------------------------------------------
Document Revision Date
----------------------------------------------------------------------------------------------------------------
Boeing DC-8 Special Compliance Item A.................................. August 8, 2006.
Report, MDC-02K9030.
Boeing DC-8 Special Compliance Item B.................................. July 23, 2009.
Report, MDC-02K9030.
Boeing DC-8 Special Compliance Item C.................................. January 5, 2010.
Report, MDC-02K9030.
Boeing DC-8 Special Compliance Item D.................................. June 9, 2010.
Report, MDC-02K9030.
[[Page 61992]]
Boeing Service Bulletin DC8-28-090.... Original........................... October 9, 2009.
----------------------------------------------------------------------------------------------------------------
Boeing DC-8 Special Compliance Item Report, MDC-02K9030,
Revision B, dated July 23, 2009, contains the following effective
pages:
List of Effective Pages
----------------------------------------------------------------------------------------------------------------
Page title/description Page number(s) Revision number Date shown on Page(s)
----------------------------------------------------------------------------------------------------------------
Report Title Page................. None shown........... B.................... July 23, 2009.
Index of Page Changes............. ii, iii.............. B.................... None shown.*
Table of Contents................. iv, v................ B.................... None shown.*
Discussion........................ 1.................... New.................. None shown.*
Appendix A........................ A1-A4................ New.................. None shown.*
Appendix B........................ B1, B3, B4, B6-B12... New.................. None shown.*
B2, B5, B13-B24...... B.................... None shown.*
Appendix C........................ C1-C5................ New.................. None shown.*
C6-C10............... B.................... None shown.*
Appendix D........................ D1................... New.................. None shown.*
----------------------------------------------------------------------------------------------------------------
Boeing DC-8 Special Compliance Item Report, MDC-02K9030,
Revision C, dated January 5, 2010, contains the following effective
pages:
List of Effective Pages
----------------------------------------------------------------------------------------------------------------
Page title/description Page number(s) Revision number Date shown on page(s)
----------------------------------------------------------------------------------------------------------------
Report Title Page................. None shown........... C.................... January 5, 2010.
Index of Page Changes............. ii, iii.............. C.................... None shown.*
Table of Contents................. iv, v................ C.................... None shown.*
Discussion........................ 1.................... C.................... None shown.*
Appendix A........................ A1-A3................ New.................. None shown.*
A4-A25............... C.................... None shown.*
Appendix B........................ B1, B3, B4, B6-B12... New.................. None shown.*
B2, B5, B13-B24...... B.................... None shown.*
Appendix C........................ C1-C5................ New.................. None shown.*
C6-C10............... B.................... None shown.*
C11-C14.............. C.................... None shown.*
Appendix D........................ D1................... New.................. None shown.*
----------------------------------------------------------------------------------------------------------------
Boeing DC-8 Special Compliance Item Report, MDC-02K9030,
Revision D, dated June 9, 2010, contains the following effective
pages:
List of Effective Pages
----------------------------------------------------------------------------------------------------------------
Page title/description Page number(s) Revision number Date shown on page(s)
----------------------------------------------------------------------------------------------------------------
Report Title Page................. None shown........... D.................... June 9, 2010.
Attachment A...................... None shown........... None shown........... June 22, 2010.
Index of Page Changes............. ii................... B.................... None shown.*
iii.................. C.................... None shown.*
Table of Contents................. iv, v................ C.................... None shown.*
Discussion........................ 1.................... C.................... None shown.*
Appendix A........................ A1-A3................ New.................. None shown.*
A4-A25............... C.................... None shown.*
Appendix B........................ B1, B3, B6, B7, B9, New.................. None shown.*
B12.
B2, B13-B24.......... B.................... None shown.*
B4, B5, B8, B10, B11. D.................... None shown.*
Appendix C........................ C1-C5................ New.................. None shown.*
C6-C10............... B.................... None shown.*
C11-C14.............. C.................... None shown.*
Appendix D........................ D1................... New.................. None shown.*
----------------------------------------------------------------------------------------------------------------
[[Page 61993]]
(* The revision date of these documents is shown only on the
title page of these documents.)
(1) The Director of the Federal Register approved the
incorporation by reference of the service information contained in
Table 2 of this AD under 5 U.S.C. 552(a) and 1 CFR part 51.
Table 2--New Material Incorporated By Reference
----------------------------------------------------------------------------------------------------------------
Document Revision Date
----------------------------------------------------------------------------------------------------------------
Boeing DC-8 Special Compliance Item B.................................. July 23, 2009.
Report, MDC-02K9030.
Boeing DC-8 Special Compliance Item C.................................. January 5, 2010.
Report, MDC-02K9030.
Boeing DC-8 Special Compliance Item D.................................. June 9, 2010.
Report, MDC-02K9030.
Boeing Service Bulletin DC8-28-090.... Original........................... October 9, 2009.
----------------------------------------------------------------------------------------------------------------
(2) The Director of the Federal Register previously approved the
incorporation by reference of Boeing DC-8 Special Compliance Item
Report, MDC-02K9030, Revision A, dated August 8, 2006, on May 27,
2008 (73 FR 21523, April 22, 2008).
(3) For service information identified in this AD, contact
Boeing Commercial Airplanes, Attention: Data & Services Management,
3855 Lakewood Boulevard, MC D800-0019, Long Beach, California 90846-
0001; telephone 206-544-5000, extension 2; fax 206-766-5683; e-mail
dse.boecom@boeing.com; Internet https://www.myboeingfleet.com.
(4) You may review copies of the service information at the FAA,
Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton,
Washington. For information on the availability of this material at
the FAA, call 425-227-1221.
(5) You may also review copies of the service information that
is incorporated by reference 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 September 23, 2010.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2010-25021 Filed 10-6-10; 8:45 am]
BILLING CODE 4910-13-P
