Airworthiness Directives; Cessna Aircraft Company, Models 208 and 208B Airplanes, 14191-14193 [E8-5269]
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Federal Register / Vol. 73, No. 52 / Monday, March 17, 2008 / Proposed Rules
Reason
(e) The mandatory continuing
airworthiness information (MCAI) states:
Bombardier Aerospace has completed a
system safety review of the CL–600–2C10/
CL–600–2D24 aircraft fuel system against
new fuel tank safety standards, introduced in
Chapter 525 of the Airworthiness Manual
through Notice of Proposed Amendment
(NPA) 2002–043. The identified noncompliances were assessed using Transport
Canada Policy Letter No. 525–001 to
determine if mandatory corrective action is
required.
The assessment and lightning tests showed
that certain fuel tube self-bonded couplings
do not provide sufficient lightning current
capability. The assessment also showed that
single failure of the integral bonding wire of
the self-bonded couplings could affect
electrical bonding between the tubes.
Insufficient electrical bonding between fuel
tubes or insufficient current capability of fuel
tube couplings, if not corrected, could result
in arcing and potential ignition source[s]
inside the fuel tank during lightning strikes
and consequent fuel tank explosion. To
correct the unsafe condition, this directive
mandates the replacement of certain fuel tube
couplings with redesigned couplings.
Actions and Compliance
(f) Within 4,500 flight hours after the
effective date of this AD, unless already
done, do the following actions.
(1) For airplanes on which Bombardier
Service Bulletin 670BA–28–014, dated
January 4, 2005, has not been incorporated as
of the effective date of this AD: Replace fuel
tube couplings inside the wing and center
fuel tanks with redesigned couplings, in
accordance with Part A of the
Accomplishment Instructions of Bombardier
Service Bulletin 670BA–28–014, Revision A,
dated May 7, 2007.
(2) For airplanes on which Bombardier
Service Bulletin 670BA–28–014, dated
January 4, 2005, has been incorporated as of
the effective date of this AD: Do a visual
inspection of the aft scavenge ejector fuel
couplings inside the left- and right-hand
wing fuel tanks to determine if redesigned
couplings are installed, and replace with
redesigned couplings as applicable, in
accordance with Part B of the
Accomplishment Instructions of Bombardier
Service Bulletin 670BA–28–014, Revision A,
dated May 7, 2007.
FAA AD Differences
pwalker on PROD1PC71 with PROPOSALS
Note: This AD differs from the MCAI and/
or service information as follows: No
differences.
Other FAA AD Provisions
(g) The following provisions also apply to
this AD:
(1) Alternative Methods of Compliance
(AMOCs): The Manager, New York 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: James
Delisio, Aerospace Engineer, Airframe and
Propulsion Branch, ANE–171, FAA, New
York ACO, 1600 Stewart Avenue, Suite 410,
VerDate Aug<31>2005
16:11 Mar 14, 2008
Jkt 214001
Westbury, New York 11590; telephone (516)
228–7321; fax (516) 794–5531. Before using
any approved AMOC on any airplane to
which the AMOC applies, notify your
appropriate principal inspector (PI) in the
FAA Flight Standards District Office (FSDO),
or lacking a PI, your local FSDO.
(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,
the Office of Management and Budget (OMB)
has approved the information collection
requirements and has assigned OMB Control
Number 2120–0056.
Related Information
(h) Refer to MCAI Transport Canada Civil
Aviation Canadian Airworthiness Directive
CF–2008–02, dated January 3, 2008, and
Bombardier Service Bulletin 670BA–28–014,
Revision A, dated May 7, 2007, for related
information.
Issued in Renton, Washington, on March 9,
2008.
Stephen P. Boyd,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E8–5335 Filed 3–14–08; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2008–0331; Directorate
Identifier 2008–CE–009–AD]
RIN 2120–AA64
Airworthiness Directives; Cessna
Aircraft Company, Models 208 and
208B Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
We propose to adopt a new
airworthiness directive (AD) for certain
Cessna Aircraft Company (Cessna)
Models 208 and 208B airplanes. This
proposed AD would require inspection
of the left and right wing wire bundle(s)
and repair or replacement of damaged
wire. This proposed AD would also
require inspecting the wire bundles for
correct attachment to the anchor points
and correcting any deficient
attachments. This proposed AD results
SUMMARY:
PO 00000
Frm 00003
Fmt 4702
Sfmt 4702
14191
from chafed wiring found on wire
bundles in the left and right wings
containing the auto-control wing de-ice
system, fuel quantity indication, and
low fuel annunciation on the Cessna
208B airplanes. Improper installation of
wire bundle supporting hardware can
cause chafed wiring in the affected
bundles. We are proposing this AD to
detect and correct damaged wiring of
the auto-control wing de-ice system,
fuel quantity indication, and low fuel
annunciation systems. This condition
could result in incorrect fuel quantity
indications, loss of low fuel quantity
annunciations, or loss of the autocontrol
wing de-ice system.
DATES: We must receive comments on
this proposed AD by May 16, 2008.
ADDRESSES: Use one of the following
addresses to comment on this proposed
AD:
• Federal eRulemaking Portal: Go to
https://www.regulations.gov. Follow the
instructions for submitting comments.
• Fax: (202) 493–2251.
• Mail: U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue, SE.,
Washington, DC 20590.
• Hand Delivery: U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue, SE.,
Washington, DC 20590, between 9 a.m.
and 5 p.m., Monday through Friday,
except Federal holidays.
For service information identified in
this proposed AD, contact Cessna
Aircraft Company, One Cessna
Boulevard, P.O. Box 7706, Wichita, KS
67277–7704; telephone: (316) 517–5800;
fax: (316) 942–9006.
FOR FURTHER INFORMATION CONTACT:
Daniel Hilton, Aerospace Engineer,
FAA, Wichita Aircraft Certification
Office, 1801 Airport Road, Room 100,
Wichita, Kansas 67209; telephone: 316–
946–4173; e-mail address:
daniel.hilton@faa.gov.
SUPPLEMENTARY INFORMATION:
Comments Invited
We invite you to send any written
relevant data, views, or arguments
regarding this proposed AD. Send your
comments to an address listed under the
ADDRESSES section. Include the docket
number, ‘‘FAA–2008–0331; Directorate
Identifier 2008–CE–009–AD’’ at the
beginning of your comments. We
specifically invite comments on the
overall regulatory, economic,
environmental, and energy aspects of
the proposed AD. We will consider all
comments received by the closing date
E:\FR\FM\17MRP1.SGM
17MRP1
14192
Federal Register / Vol. 73, No. 52 / Monday, March 17, 2008 / Proposed Rules
and may amend the proposed AD in
light of those comments.
We will post all comments we
receive, without change, to https://
www.regulations.gov, including any
personal information you provide. We
will also post a report summarizing each
substantive verbal contact we receive
concerning this proposed AD.
Discussion
We have reports of chafed wiring
found on wire bundles in the left and
right wings containing the auto-control
wing de-ice system, fuel quantity
indication, and low fuel annunciation
on several Cessna Model 208B
airplanes. Improper installation of wire
bundle supporting hardware can cause
chafed wiring in the affected bundles.
We are proposing this AD to detect and
correct damaged wiring of the autocontrol wing de-ice system, fuel
quantity indication, and low fuel
annunciation systems. This condition, if
not corrected, could result in incorrect
fuel quantity indications, loss of low
fuel quantity annunciations, or loss of
the auto-control wing de-ice system.
Relevant Service Information
We have reviewed Cessna Aircraft
Company Service Bulletin CAB08–02,
dated February 4, 2008.
The service information describes
procedures for:
• Inspecting the left and right wing
electrical wire bundles;
• Repairing and properly attaching
damaged wires; and
• Properly securing loosely attached
wires.
FAA’s Determination and Requirements
of the Proposed AD
We are proposing this AD because we
evaluated all information and
determined the unsafe condition
described previously is likely to exist or
develop on other products of the same
type design. This proposed AD would
require the inspection of the wire
harness and repair or replacement of
damaged wire.
Costs of Compliance
We estimate that this proposed AD
would affect 512 airplanes in the U.S.
registry.
We estimate the following costs to do
the proposed inspection:
Labor cost
Parts cost
Total cost per
airplane
Total cost on
U.S. operators
1 work-hour × $80 per hour = $80 ...............................
Not Applicable ..............................................................
$80
$40,960
We estimate the following costs to do
any necessary repairs or replacements
that would be required based on the
results of the proposed inspection. We
have no way of determining the number
of airplanes that may need this repair/
replacement:
Labor cost
Parts cost
Total cost per
airplane
1 work-hour × $80 per hour = $80 ..........................................................................................................................
$10
$90
Warranty credit will be given to the
extent specified in Cessna Aircraft
Company Service Bulletin CAB08–02,
dated February 4, 2008.
Regulatory Findings
pwalker on PROD1PC71 with PROPOSALS
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.
VerDate Aug<31>2005
16:11 Mar 14, 2008
Jkt 214001
We have determined that this
proposed AD would not have federalism
implications under Executive Order
13132. This proposed AD would not
have a substantial direct effect on the
States, on the relationship between the
national Government and the States, or
on the distribution of power and
responsibilities among the various
levels of government.
For the reasons discussed above, I
certify that the proposed regulation:
1. Is not a ‘‘significant regulatory
action’’ under Executive Order 12866;
2. Is not a ‘‘significant rule’’ under the
DOT Regulatory Policies and Procedures
(44 FR 11034, February 26, 1979); and
3. Will not have a significant
economic impact, positive or negative,
on a substantial number of small entities
under the criteria of the Regulatory
Flexibility Act.
We prepared a regulatory evaluation
of the estimated costs to comply with
this proposed AD and placed it in the
AD docket.
regulatory evaluation, any comments
received, and other information 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 Docket Office (telephone
(800) 647–5527) is located at the street
address stated in the ADDRESSES section.
Comments will be available in the AD
docket shortly after receipt.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Safety.
The Proposed Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA proposes to amend 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.
Examining the AD Docket
§ 39.13
You may examine the AD docket that
contains the proposed AD, the
2. The FAA amends § 39.13 by adding
the following new AD:
PO 00000
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E:\FR\FM\17MRP1.SGM
[Amended]
17MRP1
Federal Register / Vol. 73, No. 52 / Monday, March 17, 2008 / Proposed Rules
Cessna Aircraft Company: Docket No. FAA–
2008–0331; Directorate Identifier 2008–
CE–009–AD.
Comments Due Date
(a) We must receive comments on this
airworthiness directive (AD) action by May
16, 2008.
Affected ADs
(b) None.
Applicability
(c) This AD applies to the following
airplane models and serial numbers that are
certificated in any category:
Models
Serial Nos.
208 ......
208B ....
20800001 through 20800415.
208B0001 through 208B1299.
Unsafe Condition
(d) This AD results from reports of chafed
wiring found on wire bundles in the left and
right wings containing the auto-control wing
14193
de-ice system, fuel quantity indication, and
low fuel annunciation on several Cessna
Model 208B airplanes. We are proposing this
AD to detect and correct damaged wiring of
the auto-control wing de-ice system, fuel
quantity indication, and low fuel
annunciation systems. This condition, if not
corrected, could result in incorrect fuel
quantity indications, loss of low fuel quantity
annunciations, or loss of the auto-control
wing de-ice system.
Compliance
(e) To address this problem, you must do
the following, unless already done:
Actions
Compliance
Procedures
(1) Inspect the left and right wing electrical wire
bundles at the anchor attach points for loose
and damaged wiring.
Within the next 200 hours time-in-service after
the effective date of this AD, or within 12
months after the effective date of this AD,
whichever comes first.
Before further flight after the inspection required by paragraph (e)(1) of this AD.
Follow Cessna Aircraft Company Service Bulletin CAB08–02, dated February 4, 2008.
Before further flight after the inspection required by paragraph (e)(1) of this AD.
Follow Cessna Aircraft Company Service Bulletin CAB08–02, dated February 4, 2008.
(2) If, as a result of the inspection required by
paragraph (e)(1) of this AD, damaged wires
are found, repair or replace damaged wires
and properly attach wire bundle.
(3) If, as a result of the inspection required by
paragraph (e)(1) of this AD, loosely attached
wires were found, secure any wires that are
loosely attached and properly attach wire
bundle supporting hardware.
Alternative Methods of Compliance
(AMOCs)
DEPARTMENT OF HOMELAND
SECURITY
(f) The Manager, Wichita Aircraft
Certification Office, 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: Daniel Hilton,
Aerospace Engineer, FAA, Wichita ACO,
1801 Airport Road, Room 100, Wichita,
Kansas 67209; telephone: 316–946–4173; email address: daniel.hilton@faa.gov. Before
using any approved AMOC on any airplane
to which the AMOC applies, notify your
appropriate principal inspector (PI) in the
FAA Flight Standards District Office (FSDO),
or lacking a PI, your local FSDO.
Related Information
pwalker on PROD1PC71 with PROPOSALS
(g) To get copies of the service information
referenced in this AD, contact Cessna Aircraft
Company, One Cessna Boulevard, P.O. Box
7706, Wichita, KS 67277–7704; telephone:
(316) 517–5800; fax: (316) 942–9006. To view
the AD docket, go to U.S. Department of
Transportation, Docket Operations, M–30,
West Building Ground Floor, Room W12–
140, 1200 New Jersey Avenue, SE.,
Washington, DC 20590, or on the Internet at
https://www.regulations.gov.
Issued in Kansas City, Missouri, on March
11, 2008.
David R. Showers,
Acting Manager, Small Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E8–5269 Filed 3–14–08; 8:45 am]
BILLING CODE 4910–13–P
VerDate Aug<31>2005
16:11 Mar 14, 2008
Jkt 214001
Coast Guard
33 CFR Part 181
[Docket No. USCG–2007–29236]
Hull Identification Numbers for
Recreational Vessels
Coast Guard, DHS.
Request for public comments.
AGENCY:
ACTION:
SUMMARY: The Coast Guard announces it
is again requesting comments on the
costs and benefits of expanding the
existing 12-character Hull Identification
Number (HIN) in order to provide
additional information identifying
vessels. The Coast Guard requests
public comments on this issue and on
the specific questions in this Notice.
DATES: Comments and related material
must reach the Docket Management
Facility on or before June 16, 2008.
ADDRESSES: You may submit comments
identified by Coast Guard docket
number USCG–2007–29236 to the
Docket Management Facility at the U.S.
Department of Transportation. To avoid
duplication, please use only one of the
following methods:
(1) Online: https://
www.regulations.gov.
(2) Mail: Docket Management Facility
(M–30), U.S. Department of
Transportation, West Building Ground
PO 00000
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Fmt 4702
Sfmt 4702
Follow Cessna Aircraft Company Service Bulletin CAB08–02, dated February 4, 2008.
Floor, Room W12–140, 1200 New Jersey
Avenue, SE., Washington, DC 20590–
0001.
(3) Hand delivery: Room W12–140 on
the Ground Floor of the West Building,
1200 New Jersey Avenue, SE.,
Washington, DC 20590, between 9 a.m.
and 5 p.m., Monday through Friday,
except Federal holidays. The telephone
number is 202–366–9329.
(4) Fax: 202–493–2251.
FOR FURTHER INFORMATION CONTACT: If
you have questions on this notice, call
Philip Cappel, Office of Boating Safety,
Recreational Boating Product Assurance
Division, Coast Guard, telephone 202–
372–1076. If you have questions on
viewing or submitting material to the
docket, call Renee V. Wright, Program
Manager, Docket Operations, telephone
202–366–9826.
SUPPLEMENTARY INFORMATION:
Public Participation and Request for
Comments
We encourage you to submit
comments and related material on this
notice. All comments received will be
posted, without change, to https://
www.regulations.gov and will include
any personal information you have
provided. We have an agreement with
the Department of Transportation (DOT)
to use the Docket Management Facility.
Please see DOT’s ‘‘Privacy Act’’
paragraph below.
Submitting comments: If you submit a
comment, please include the docket
E:\FR\FM\17MRP1.SGM
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]]>Agencies
[Federal Register Volume 73, Number 52 (Monday, March 17, 2008)]
[Proposed Rules]
[Pages 14191-14193]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E8-5269]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2008-0331; Directorate Identifier 2008-CE-009-AD]
RIN 2120-AA64
Airworthiness Directives; Cessna Aircraft Company, Models 208 and
208B Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Notice of proposed rulemaking (NPRM).
-----------------------------------------------------------------------
SUMMARY: We propose to adopt a new airworthiness directive (AD) for
certain Cessna Aircraft Company (Cessna) Models 208 and 208B airplanes.
This proposed AD would require inspection of the left and right wing
wire bundle(s) and repair or replacement of damaged wire. This proposed
AD would also require inspecting the wire bundles for correct
attachment to the anchor points and correcting any deficient
attachments. This proposed AD results from chafed wiring found on wire
bundles in the left and right wings containing the auto-control wing
de-ice system, fuel quantity indication, and low fuel annunciation on
the Cessna 208B airplanes. Improper installation of wire bundle
supporting hardware can cause chafed wiring in the affected bundles. We
are proposing this AD to detect and correct damaged wiring of the auto-
control wing de-ice system, fuel quantity indication, and low fuel
annunciation systems. This condition could result in incorrect fuel
quantity indications, loss of low fuel quantity annunciations, or loss
of the autocontrol wing de-ice system.
DATES: We must receive comments on this proposed AD by May 16, 2008.
ADDRESSES: Use one of the following addresses to comment on this
proposed AD:
Federal eRulemaking Portal: Go to https://
www.regulations.gov. Follow the instructions for submitting comments.
Fax: (202) 493-2251.
Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue, SE., Washington, DC 20590.
Hand Delivery: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue, SE., Washington, DC 20590, between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays.
For service information identified in this proposed AD, contact
Cessna Aircraft Company, One Cessna Boulevard, P.O. Box 7706, Wichita,
KS 67277-7704; telephone: (316) 517-5800; fax: (316) 942-9006.
FOR FURTHER INFORMATION CONTACT: Daniel Hilton, Aerospace Engineer,
FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Room
100, Wichita, Kansas 67209; telephone: 316-946-4173; e-mail address:
daniel.hilton@faa.gov.
SUPPLEMENTARY INFORMATION:
Comments Invited
We invite you to send any written relevant data, views, or
arguments regarding this proposed AD. Send your comments to an address
listed under the ADDRESSES section. Include the docket number, ``FAA-
2008-0331; Directorate Identifier 2008-CE-009-AD'' at the beginning of
your comments. We specifically invite comments on the overall
regulatory, economic, environmental, and energy aspects of the proposed
AD. We will consider all comments received by the closing date
[[Page 14192]]
and may amend the proposed AD in light of those comments.
We will post all comments we receive, without change, to https://
www.regulations.gov, including any personal information you provide. We
will also post a report summarizing each substantive verbal contact we
receive concerning this proposed AD.
Discussion
We have reports of chafed wiring found on wire bundles in the left
and right wings containing the auto-control wing de-ice system, fuel
quantity indication, and low fuel annunciation on several Cessna Model
208B airplanes. Improper installation of wire bundle supporting
hardware can cause chafed wiring in the affected bundles. We are
proposing this AD to detect and correct damaged wiring of the auto-
control wing de-ice system, fuel quantity indication, and low fuel
annunciation systems. This condition, if not corrected, could result in
incorrect fuel quantity indications, loss of low fuel quantity
annunciations, or loss of the auto-control wing de-ice system.
Relevant Service Information
We have reviewed Cessna Aircraft Company Service Bulletin CAB08-02,
dated February 4, 2008.
The service information describes procedures for:
Inspecting the left and right wing electrical wire
bundles;
Repairing and properly attaching damaged wires; and
Properly securing loosely attached wires.
FAA's Determination and Requirements of the Proposed AD
We are proposing this AD because we evaluated all information and
determined the unsafe condition described previously is likely to exist
or develop on other products of the same type design. This proposed AD
would require the inspection of the wire harness and repair or
replacement of damaged wire.
Costs of Compliance
We estimate that this proposed AD would affect 512 airplanes in the
U.S. registry.
We estimate the following costs to do the proposed inspection:
----------------------------------------------------------------------------------------------------------------
Total cost per Total cost on
Labor cost Parts cost airplane U.S. operators
----------------------------------------------------------------------------------------------------------------
1 work-hour x $80 per hour = $80............. Not Applicable................. $80 $40,960
----------------------------------------------------------------------------------------------------------------
We estimate the following costs to do any necessary repairs or
replacements that would be required based on the results of the
proposed inspection. We have no way of determining the number of
airplanes that may need this repair/replacement:
------------------------------------------------------------------------
Total cost per
Labor cost Parts cost airplane
------------------------------------------------------------------------
1 work-hour x $80 per hour = $80...... $10 $90
------------------------------------------------------------------------
Warranty credit will be given to the extent specified in Cessna
Aircraft Company Service Bulletin CAB08-02, dated February 4, 2008.
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 proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would not
have a substantial direct effect on the States, on the relationship
between the national Government and the States, or on the distribution
of power and responsibilities among the various levels of government.
For the reasons discussed above, I certify that the proposed
regulation:
1. Is not a ``significant regulatory action'' under Executive Order
12866;
2. Is not a ``significant rule'' under the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979); and
3. Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
We prepared a regulatory evaluation of the estimated costs to
comply with this proposed AD and placed it in the AD docket.
Examining the AD Docket
You may examine the AD docket that contains the proposed AD, the
regulatory evaluation, any comments received, and other information 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 Docket Office (telephone (800) 647-5527)
is located at the street address stated in the ADDRESSES section.
Comments will be available in the AD docket shortly after receipt.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Safety.
The Proposed Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 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.
Sec. 39.13 [Amended]
2. The FAA amends Sec. 39.13 by adding the following new AD:
[[Page 14193]]
Cessna Aircraft Company: Docket No. FAA-2008-0331; Directorate
Identifier 2008-CE-009-AD.
Comments Due Date
(a) We must receive comments on this airworthiness directive
(AD) action by May 16, 2008.
Affected ADs
(b) None.
Applicability
(c) This AD applies to the following airplane models and serial
numbers that are certificated in any category:
------------------------------------------------------------------------
Models Serial Nos.
------------------------------------------------------------------------
208.............................. 20800001 through 20800415.
208B............................. 208B0001 through 208B1299.
------------------------------------------------------------------------
Unsafe Condition
(d) This AD results from reports of chafed wiring found on wire
bundles in the left and right wings containing the auto-control wing
de-ice system, fuel quantity indication, and low fuel annunciation
on several Cessna Model 208B airplanes. We are proposing this AD to
detect and correct damaged wiring of the auto-control wing de-ice
system, fuel quantity indication, and low fuel annunciation systems.
This condition, if not corrected, could result in incorrect fuel
quantity indications, loss of low fuel quantity annunciations, or
loss of the auto-control wing de-ice system.
Compliance
(e) To address this problem, you must do the following, unless
already done:
------------------------------------------------------------------------
Actions Compliance Procedures
------------------------------------------------------------------------
(1) Inspect the left and Within the next 200 Follow Cessna
right wing electrical wire hours time-in- Aircraft Company
bundles at the anchor service after the Service Bulletin
attach points for loose and effective date of CAB08-02, dated
damaged wiring. this AD, or within February 4, 2008.
12 months after the
effective date of
this AD, whichever
comes first.
(2) If, as a result of the Before further Follow Cessna
inspection required by flight after the Aircraft Company
paragraph (e)(1) of this inspection required Service Bulletin
AD, damaged wires are by paragraph (e)(1) CAB08-02, dated
found, repair or replace of this AD. February 4, 2008.
damaged wires and properly
attach wire bundle.
(3) If, as a result of the Before further Follow Cessna
inspection required by flight after the Aircraft Company
paragraph (e)(1) of this inspection required Service Bulletin
AD, loosely attached wires by paragraph (e)(1) CAB08-02, dated
were found, secure any of this AD. February 4, 2008.
wires that are loosely
attached and properly
attach wire bundle
supporting hardware.
------------------------------------------------------------------------
Alternative Methods of Compliance (AMOCs)
(f) The Manager, Wichita Aircraft Certification Office, 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: Daniel
Hilton, Aerospace Engineer, FAA, Wichita ACO, 1801 Airport Road,
Room 100, Wichita, Kansas 67209; telephone: 316-946-4173; e-mail
address: daniel.hilton@faa.gov. Before using any approved AMOC on
any airplane to which the AMOC applies, notify your appropriate
principal inspector (PI) in the FAA Flight Standards District Office
(FSDO), or lacking a PI, your local FSDO.
Related Information
(g) To get copies of the service information referenced in this
AD, contact Cessna Aircraft Company, One Cessna Boulevard, P.O. Box
7706, Wichita, KS 67277-7704; telephone: (316) 517-5800; fax: (316)
942-9006. To view the AD docket, go to U.S. Department of
Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC 20590, or
on the Internet at https://www.regulations.gov.
Issued in Kansas City, Missouri, on March 11, 2008.
David R. Showers,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E8-5269 Filed 3-14-08; 8:45 am]
BILLING CODE 4910-13-P
