Airworthiness Directives; Lockheed Model L-1011 Series Airplanes, 74462-74464 [E6-20953]
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74462
Federal Register / Vol. 71, No. 238 / Tuesday, December 12, 2006 / Rules and Regulations
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2006–25554; Directorate
Identifier 2006–NM–123–AD; Amendment
39–14852; AD 2006–25–11]
RIN 2120–AA64
Airworthiness Directives; Lockheed
Model L–1011 Series Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
SUMMARY: The FAA is adopting a new
airworthiness directive (AD) for certain
Lockheed Model L–1011 series
airplanes. This AD requires a one-time
detailed inspection of the C112 harness
clamp assembly for proper installation,
a one-time detailed inspection of the
C112 and C162 harness assemblies for
damage, and corrective actions if
necessary. This AD results from a report
of electrical arcing of the essential bus
feeder cables behind hinged circuit
breaker panel CB3 P–K. We are issuing
this AD to prevent arcing of essential
bus feeder cables due to improper
installation of the harness C112 clamp
assembly, which could result in loss of
electrical systems and smoke and/or fire
behind the CB3 P–K hinged circuit
breaker panel in the flight compartment.
DATES: This AD becomes effective
January 16, 2007.
The Director of the Federal Register
approved the incorporation by reference
of a certain publications listed in the AD
as of January 16, 2007.
ADDRESSES: You may examine the AD
docket on the Internet at https://
dms.dot.gov or in person at the Docket
Management Facility, U.S. Department
of Transportation, 400 Seventh Street
SW., Nassif Building, Room PL–401,
Washington, DC.
Contact Lockheed Martin Aircraft &
Logistics Center, 120 Orion Street,
Greenville, South Carolina 29605, for
service information identified in this
AD.
jlentini on PROD1PC65 with RULES
FOR FURTHER INFORMATION CONTACT:
Robert Chupka, Aerospace Engineer,
Systems and Equipment Branch, ACE–
119A, FAA, Atlanta Aircraft
Certification Office, One Crown Center,
1895 Phoenix Boulevard, Suite 450,
Atlanta, Georgia 30349; telephone (770)
703–6070; fax (770) 703–6097.
SUPPLEMENTARY INFORMATION:
VerDate Aug<31>2005
17:58 Dec 11, 2006
Jkt 211001
Examining the Docket
You may examine the airworthiness
directive (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 street address stated in the
ADDRESSES section.
Discussion
The FAA issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would
apply to certain Lockheed Model L–
1011 series airplanes. That NPRM was
published in the Federal Register on
August 9, 2006 (71 FR 45447). That
NPRM proposed to require a one-time
detailed inspection of the C112 harness
clamp assembly for proper installation,
a one-time detailed inspection of the
C112 and C162 harness assemblies for
damage, and corrective actions if
necessary.
Comments
We provided the public the
opportunity to participate in the
development of this AD. We have
considered the comments received.
Request to Make Service Documents
Available to the Public by
Incorporation by Reference and
Publication in the Docket Management
System (DMS)
The Modification and Replacement
Parts Association (MARPA) requests
that we incorporate by reference the
essential service documents in the
NPRM. MARPA states that ADs are
typically based upon service
information originating with the type
certificate holder or its suppliers.
MARPA asserts that, if a service
document is used as a mandatory
element of compliance, it should not
only be referred to, but also
incorporated into the AD. MARPA adds
that manufacturer’s service documents
are privately authored instruments,
generally having copyright protection
against duplication and distribution.
When a service document is
incorporated by reference into a public
document, such as an AD, pursuant to
5 U.S.C. 552(a) and 1 CFR part 51, it
loses its private, protected status and
becomes a public document. MARPA
notes that the NPRM is one of these
public documents, but does not
incorporate by reference that service
document. Therefore, the NPRM, as
proposed, attempts to require
compliance with a public law by
PO 00000
Frm 00008
Fmt 4700
Sfmt 4700
reference to a private writing. MARPA
believes that public laws, by definition,
should be public and that they cannot
rely on private writings.
We do not agree that documents
should be incorporated by reference
during the NPRM phase of rulemaking.
The Office of the Federal Register (OFR)
requires that documents that are
necessary to accomplish the
requirements of the AD be incorporated
by reference during the final rule phase
of rulemaking. This final rule
incorporates by reference the document
necessary for the accomplishment of the
requirements mandated by this AD.
Further, we point out that while
documents that are incorporated by
reference do become public information,
they do not lose their copyright
protection. For that reason, we advise
the public to contact the manufacturer
to obtain copies of the referenced
service information.
MARPA also requests that essential
service documents be published in
DMS. MARPA states that service
documents incorporated by reference
should be made available to the public
by publication in either the Federal
Register or DMS. MARPA also states
that the purpose of the incorporation by
reference method is brevity, to keep
from expanding the Federal Register
needlessly by publishing documents
already in the hands of the affected
individuals. MARPA adds that,
traditionally, ‘‘affected individuals’’
means aircraft owners and operators,
who are generally provided service
information by the manufacturer.
MARPA further adds that a new class of
affected individuals has emerged, since
the majority of aircraft maintenance is
now performed by specialty shops
instead of aircraft owners and operators.
This new class includes maintenance
and repair organizations, component
servicing and repair shops, parts
purveyors and distributors, and/or
organizations repairing or servicing
alternatively certified parts under
section 21.303 (‘‘Parts Manufacturer
Approval’’) of the Federal Aviation
Regulations (14 CFR 21.303). MARPA
states that the concept of brevity is now
nearly archaic as documents exist more
frequently in electronic format than on
paper.
In regard to MARPA’s request that
service documents be made available to
the public by publication in the Federal
Register, we agree that incorporation by
reference was authorized to reduce the
volume of material published in the
Federal Register and the Code of
Federal Regulations. However, as
specified in the Federal Register
Document Drafting Handbook, the
E:\FR\FM\12DER1.SGM
12DER1
Federal Register / Vol. 71, No. 238 / Tuesday, December 12, 2006 / Rules and Regulations
Director of the OFR decides when an
agency may incorporate material by
reference. As the commenter is aware,
the OFR files documents for public
inspection on the workday before the
date of publication of the rule at its
office in Washington, DC. As stated in
the Federal Register Document Drafting
Handbook, when documents are filed
for public inspection, anyone may
inspect or copy file documents during
the OFR’s hours of business. Further
questions regarding publication of
documents in the Federal Register or
incorporation by reference should be
directed to the OFR.
In regards to MARPA’s request to post
service bulletins on the Department of
Transportation’s DMS, we are currently
in the process of reviewing issues
surrounding the posting of service
bulletins on the DMS as part of an AD
docket. 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. No change
to the final rule is necessary in response
to this comment.
74463
Conclusion
We have carefully reviewed the
available data, including the comment
received, and determined that air safety
and the public interest require adopting
the AD as proposed.
Costs of Compliance
There are about 126 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
Action
Work hours
Average labor
rate per hour
Parts
Cost per
airplane
Number of
U.S.-registered
airplanes
Fleet cost
Inspection of clamp assembly .................
2
$80
$0
$160
53
$8,480
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.
on a substantial number of small entities
under the criteria of the Regulatory
Flexibility Act.
We prepared a regulatory evaluation
of the estimated costs to comply with
this AD and placed it in the AD docket.
See the ADDRESSES section for a location
to examine the regulatory evaluation.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
Adoption of the Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
I
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.
jlentini on PROD1PC65 with RULES
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,
VerDate Aug<31>2005
17:58 Dec 11, 2006
Jkt 211001
§ 39.13
[Amended]
2. The Federal Aviation
Administration (FAA) amends § 39.13
by adding the following new
airworthiness directive (AD):
I
2006–25–11 Lockheed: Amendment 39–
14852. Docket No. FAA–2006–25554;
Directorate Identifier 2006–NM–123–AD.
Effective Date
(a) This AD becomes effective January 16,
2007.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Lockheed Model L–
1011–385–1, L–1011–385–1–14, L–1011–
PO 00000
Frm 00009
Fmt 4700
Sfmt 4700
385–1–15, and L–1011–385–3 series
airplanes, certificated in any category; having
serial numbers 93A through 193Y inclusive
and 293A through 293F inclusive: –1002
through –1250 inclusive.
Unsafe Condition
(d) This AD results from a report of
electrical arcing of the essential bus feeder
cables behind hinged circuit breaker panel
CB3 P–K. We are issuing this AD to prevent
arcing of essential bus feeder cables due to
improper installation of the harness C112
clamp assembly, which could result in loss
of electrical systems and smoke and/or fire
behind the CB3 P–K hinged circuit breaker
panel in the flight compartment.
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.
Detailed Inspection of the C112 Harness
Clamp Assembly
(f) Within 90 days after the effective date
of this AD: Do the actions in paragraphs (f)(1)
and (f)(2) of this AD by accomplishing all the
actions specified in the Accomplishment
Instructions of Lockheed L–1011 Service
Bulletin 093–24–142, dated November 16,
2005. Do all applicable corrective actions
before further flight.
(1) Perform a one-time detailed inspection
of the C112 harness clamp assembly to find
incorrectly installed harness clamps, and do
all applicable corrective actions.
(2) Perform a one-time detailed inspection
of the C112 and C162 harness assemblies to
find evidence of chafing, arcing, or
deterioration, and do all applicable corrective
actions.
Note 1: For the purposes of this AD, a
detailed inspection is: ‘‘An intensive
examination of a specific item, installation,
or assembly to detect damage, failure, or
irregularity. Available lighting is normally
supplemented with a direct source of good
lighting at an intensity deemed appropriate.
E:\FR\FM\12DER1.SGM
12DER1
74464
Federal Register / Vol. 71, No. 238 / Tuesday, December 12, 2006 / Rules and Regulations
Inspection aids such as mirror, magnifying
lenses, etc., may be necessary. Surface
cleaning and elaborate procedures may be
required.’’
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
Alternative Methods of Compliance
(AMOCs)
(g)(1) The Manager, Atlanta Aircraft
Certification Office, 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.
Material Incorporated by Reference
(h) You must use Lockheed L–1011 Service
Bulletin 093–24–142, dated November 16,
2005, to perform the actions that are required
by this AD, unless the AD specifies
otherwise. The Director of the Federal
Register approved the incorporation by
reference of this document in accordance
with 5 U.S.C. 552(a) and 1 CFR part 51.
Contact Lockheed Martin Aircraft & Logistics
Center, 120 Orion Street, Greenville, South
Carolina 29605, for a copy of this service
information. You may review copies at the
Docket Management Facility, U.S.
Department of Transportation, 400 Seventh
Street SW., Room PL–401, Nassif Building,
Washington, DC; on the Internet at https://
dms.dot.gov; or at the National Archives and
Records Administration (NARA). For
information on the availability of this
material at the NARA, call (202) 741–6030,
or go to https://www.archives.gov/
federal_register/code_of_federal_regulations/
ibr_locations.html.
Issued in Renton, Washington, on
December 1, 2006.
Kevin M. Mullin,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. E6–20953 Filed 12–11–06; 8:45 am]
BILLING CODE 4910–13–P
[Docket No. FAA–2006–25920; Directorate
Identifier 2006–NM–137–AD; Amendment
39–14851; AD 2006–25–10]
FOR FURTHER INFORMATION CONTACT:
Todd Thompson, Aerospace Engineer,
International Branch, ANM–116,
Transport Airplane Directorate, FAA,
1601 Lind Avenue, SW., Renton,
Washington 98057–3356; telephone
(425) 227–1175; fax (425) 227–1149.
SUPPLEMENTARY INFORMATION:
RIN 2120–AA64
Examining the Docket
Airworthiness Directives; BAE
Systems (Operations) Limited Model
BAe 146 and Avro 146–RJ Airplanes
You may examine the airworthiness
directive (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 street address stated in the
ADDRESSES section.
Federal Aviation
Administration, DOT.
ACTION: Final rule.
AGENCY:
SUMMARY: The FAA is adopting a new
airworthiness directive (AD) for all BAE
Systems (Operations) Limited Model
BAe 146 and Model Avro 146–RJ
airplanes. This AD requires calculating
the current life of each lift spoiler jack,
and eventually replacing each lift
spoiler jack. This AD results from a
review of all system components as part
of the life-extension program for the
affected airplanes that indicated the
fatigue life limit of certain lift spoiler
jacks cannot be extended from the
current life limit. We are issuing this AD
to prevent failure of the lift spoiler jack,
and consequent increased drag and
uncommanded roll inputs, which could
reduce the flightcrew’s ability to control
the airplane.
DATES: This AD becomes effective
January 16, 2007.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in the AD
as of January 16, 2007.
ADDRESSES: You may examine the AD
docket on the Internet at https://
dms.dot.gov or in person at the Docket
Management Facility, U.S. Department
of Transportation, 400 Seventh Street,
SW., Nassif Building, Room PL–401,
Washington, DC.
Contact British Aerospace Regional
Aircraft American Support, 13850
Mclearen Road, Herndon, Virginia
20171, for service information identified
in this AD.
Discussion
The FAA issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would
apply to all BAE Systems (Operations)
Limited Model BAe 146 and Model
Avro 146–RJ airplanes. That NPRM was
published in the Federal Register on
September 28, 2006 (71 FR 56903). That
NPRM proposed to require calculating
the current life of each lift spoiler jack,
and eventually replacing each lift
spoiler jack.
Comments
We provided the public the
opportunity to participate in the
development of this AD. We received no
comments on the NPRM or on the
determination of the cost to the public.
Conclusion
We have carefully reviewed the
available data and determined that air
safety and the public interest require
adopting the AD as proposed.
Costs of Compliance
The following table provides the
estimated costs for U.S. operators to
comply with this AD.
ESTIMATED COSTS
Action
jlentini on PROD1PC65 with RULES
Determine the life of each lift spoiler jack ..
Replace each lift spoiler jack (6 per airplane).
VerDate Aug<31>2005
17:58 Dec 11, 2006
Average labor
rate per hour
Work hours
Jkt 211001
1
6
PO 00000
Frm 00010
$80
80
Fmt 4700
Parts
None ...........
$102,000 .....
Sfmt 4700
Cost per
airplane
$80
102,480
E:\FR\FM\12DER1.SGM
12DER1
Number of
U.S.-registered
airplanes
53
53
Fleet cost
$4,240
5,431,440
Agencies
[Federal Register Volume 71, Number 238 (Tuesday, December 12, 2006)]
[Rules and Regulations]
[Pages 74462-74464]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E6-20953]
[[Page 74462]]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2006-25554; Directorate Identifier 2006-NM-123-AD;
Amendment 39-14852; AD 2006-25-11]
RIN 2120-AA64
Airworthiness Directives; Lockheed Model L-1011 Series Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Lockheed Model L-1011 series airplanes. This AD requires a one-
time detailed inspection of the C112 harness clamp assembly for proper
installation, a one-time detailed inspection of the C112 and C162
harness assemblies for damage, and corrective actions if necessary.
This AD results from a report of electrical arcing of the essential bus
feeder cables behind hinged circuit breaker panel CB3 P-K. We are
issuing this AD to prevent arcing of essential bus feeder cables due to
improper installation of the harness C112 clamp assembly, which could
result in loss of electrical systems and smoke and/or fire behind the
CB3 P-K hinged circuit breaker panel in the flight compartment.
DATES: This AD becomes effective January 16, 2007.
The Director of the Federal Register approved the incorporation by
reference of a certain publications listed in the AD as of January 16,
2007.
ADDRESSES: You may examine the AD docket on the Internet at https://
dms.dot.gov or in person at the Docket Management Facility, U.S.
Department of Transportation, 400 Seventh Street SW., Nassif Building,
Room PL-401, Washington, DC.
Contact Lockheed Martin Aircraft & Logistics Center, 120 Orion
Street, Greenville, South Carolina 29605, for service information
identified in this AD.
FOR FURTHER INFORMATION CONTACT: Robert Chupka, Aerospace Engineer,
Systems and Equipment Branch, ACE-119A, FAA, Atlanta Aircraft
Certification Office, One Crown Center, 1895 Phoenix Boulevard, Suite
450, Atlanta, Georgia 30349; telephone (770) 703-6070; fax (770) 703-
6097.
SUPPLEMENTARY INFORMATION:
Examining the Docket
You may examine the airworthiness directive (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 street address stated in the ADDRESSES section.
Discussion
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to include an AD that would apply to certain Lockheed Model
L-1011 series airplanes. That NPRM was published in the Federal
Register on August 9, 2006 (71 FR 45447). That NPRM proposed to require
a one-time detailed inspection of the C112 harness clamp assembly for
proper installation, a one-time detailed inspection of the C112 and
C162 harness assemblies for damage, and corrective actions if
necessary.
Comments
We provided the public the opportunity to participate in the
development of this AD. We have considered the comments received.
Request to Make Service Documents Available to the Public by
Incorporation by Reference and Publication in the Docket Management
System (DMS)
The Modification and Replacement Parts Association (MARPA) requests
that we incorporate by reference the essential service documents in the
NPRM. MARPA states that ADs are typically based upon service
information originating with the type certificate holder or its
suppliers. MARPA asserts that, if a service document is used as a
mandatory element of compliance, it should not only be referred to, but
also incorporated into the AD. MARPA adds that manufacturer's service
documents are privately authored instruments, generally having
copyright protection against duplication and distribution. When a
service document is incorporated by reference into a public document,
such as an AD, pursuant to 5 U.S.C. 552(a) and 1 CFR part 51, it loses
its private, protected status and becomes a public document. MARPA
notes that the NPRM is one of these public documents, but does not
incorporate by reference that service document. Therefore, the NPRM, as
proposed, attempts to require compliance with a public law by reference
to a private writing. MARPA believes that public laws, by definition,
should be public and that they cannot rely on private writings.
We do not agree that documents should be incorporated by reference
during the NPRM phase of rulemaking. The Office of the Federal Register
(OFR) requires that documents that are necessary to accomplish the
requirements of the AD be incorporated by reference during the final
rule phase of rulemaking. This final rule incorporates by reference the
document necessary for the accomplishment of the requirements mandated
by this AD. Further, we point out that while documents that are
incorporated by reference do become public information, they do not
lose their copyright protection. For that reason, we advise the public
to contact the manufacturer to obtain copies of the referenced service
information.
MARPA also requests that essential service documents be published
in DMS. MARPA states that service documents incorporated by reference
should be made available to the public by publication in either the
Federal Register or DMS. MARPA also states that the purpose of the
incorporation by reference method is brevity, to keep from expanding
the Federal Register needlessly by publishing documents already in the
hands of the affected individuals. MARPA adds that, traditionally,
``affected individuals'' means aircraft owners and operators, who are
generally provided service information by the manufacturer. MARPA
further adds that a new class of affected individuals has emerged,
since the majority of aircraft maintenance is now performed by
specialty shops instead of aircraft owners and operators. This new
class includes maintenance and repair organizations, component
servicing and repair shops, parts purveyors and distributors, and/or
organizations repairing or servicing alternatively certified parts
under section 21.303 (``Parts Manufacturer Approval'') of the Federal
Aviation Regulations (14 CFR 21.303). MARPA states that the concept of
brevity is now nearly archaic as documents exist more frequently in
electronic format than on paper.
In regard to MARPA's request that service documents be made
available to the public by publication in the Federal Register, we
agree that incorporation by reference was authorized to reduce the
volume of material published in the Federal Register and the Code of
Federal Regulations. However, as specified in the Federal Register
Document Drafting Handbook, the
[[Page 74463]]
Director of the OFR decides when an agency may incorporate material by
reference. As the commenter is aware, the OFR files documents for
public inspection on the workday before the date of publication of the
rule at its office in Washington, DC. As stated in the Federal Register
Document Drafting Handbook, when documents are filed for public
inspection, anyone may inspect or copy file documents during the OFR's
hours of business. Further questions regarding publication of documents
in the Federal Register or incorporation by reference should be
directed to the OFR.
In regards to MARPA's request to post service bulletins on the
Department of Transportation's DMS, we are currently in the process of
reviewing issues surrounding the posting of service bulletins on the
DMS as part of an AD docket. 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. No change to
the final rule is necessary in response to this comment.
Conclusion
We have carefully reviewed the available data, including the
comment received, and determined that air safety and the public
interest require adopting the AD as proposed.
Costs of Compliance
There are about 126 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
--------------------------------------------------------------------------------------------------------------------------------------------------------
Number of U.S.-
Action Work hours Average labor Parts Cost per registered Fleet cost
rate per hour airplane airplanes
--------------------------------------------------------------------------------------------------------------------------------------------------------
Inspection of clamp assembly...................... 2 $80 $0 $160 53 $8,480
--------------------------------------------------------------------------------------------------------------------------------------------------------
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.
Sec. 39.13 [Amended]
0
2. The Federal Aviation Administration (FAA) amends Sec. 39.13 by
adding the following new airworthiness directive (AD):
2006-25-11 Lockheed: Amendment 39-14852. Docket No. FAA-2006-25554;
Directorate Identifier 2006-NM-123-AD.
Effective Date
(a) This AD becomes effective January 16, 2007.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Lockheed Model L-1011-385-1, L-1011-385-
1-14, L-1011-385-1-15, and L-1011-385-3 series airplanes,
certificated in any category; having serial numbers 93A through 193Y
inclusive and 293A through 293F inclusive: -1002 through -1250
inclusive.
Unsafe Condition
(d) This AD results from a report of electrical arcing of the
essential bus feeder cables behind hinged circuit breaker panel CB3
P-K. We are issuing this AD to prevent arcing of essential bus
feeder cables due to improper installation of the harness C112 clamp
assembly, which could result in loss of electrical systems and smoke
and/or fire behind the CB3 P-K hinged circuit breaker panel in the
flight compartment.
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.
Detailed Inspection of the C112 Harness Clamp Assembly
(f) Within 90 days after the effective date of this AD: Do the
actions in paragraphs (f)(1) and (f)(2) of this AD by accomplishing
all the actions specified in the Accomplishment Instructions of
Lockheed L-1011 Service Bulletin 093-24-142, dated November 16,
2005. Do all applicable corrective actions before further flight.
(1) Perform a one-time detailed inspection of the C112 harness
clamp assembly to find incorrectly installed harness clamps, and do
all applicable corrective actions.
(2) Perform a one-time detailed inspection of the C112 and C162
harness assemblies to find evidence of chafing, arcing, or
deterioration, and do all applicable corrective actions.
Note 1: For the purposes of this AD, a detailed inspection is:
``An intensive examination of a specific item, installation, or
assembly to detect damage, failure, or irregularity. Available
lighting is normally supplemented with a direct source of good
lighting at an intensity deemed appropriate.
[[Page 74464]]
Inspection aids such as mirror, magnifying lenses, etc., may be
necessary. Surface cleaning and elaborate procedures may be
required.''
Alternative Methods of Compliance (AMOCs)
(g)(1) The Manager, Atlanta Aircraft Certification Office, 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 Sec.
39.19 on any airplane to which the AMOC applies, notify the
appropriate principal inspector in the FAA Flight Standards
Certificate Holding District Office.
Material Incorporated by Reference
(h) You must use Lockheed L-1011 Service Bulletin 093-24-142,
dated November 16, 2005, to perform the actions that are required by
this AD, unless the AD specifies otherwise. The Director of the
Federal Register approved the incorporation by reference of this
document in accordance with 5 U.S.C. 552(a) and 1 CFR part 51.
Contact Lockheed Martin Aircraft & Logistics Center, 120 Orion
Street, Greenville, South Carolina 29605, for a copy of this service
information. You may review copies at the Docket Management
Facility, U.S. Department of Transportation, 400 Seventh Street SW.,
Room PL-401, Nassif Building, Washington, DC; on the Internet at
https://dms.dot.gov; or at the National Archives and Records
Administration (NARA). For information on the availability of this
material at the NARA, call (202) 741-6030, or go to https://
www.archives.gov/federal_register/code_of_federal_regulations/
ibr_locations.html.
Issued in Renton, Washington, on December 1, 2006.
Kevin M. Mullin,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E6-20953 Filed 12-11-06; 8:45 am]
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