Airworthiness Directives; Cessna Model 680 Airplanes, 395-397 [07-6265]
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Federal Register / Vol. 73, No. 2 / Thursday, January 3, 2008 / Rules and Regulations
per engine. Based on these figures, we
estimate the total cost of the AD to U.S.
operators to be $2,269,168.
1. The authority citation for part 39
continues to read as follows:
I
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 summary of the costs
to comply with this AD and placed it in
the AD Docket. You may get a copy of
this summary at the address listed
under ADDRESSES.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Safety.
jlentini on PROD1PC65 with RULES
Adoption of the Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the Federal Aviation Administration
amends 14 CFR part 39 as follows:
I
VerDate Aug<31>2005
19:37 Jan 02, 2008
Jkt 214001
PART 39—AIRWORTHINESS
DIRECTIVES
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive:
I
2007–26–20 Pratt & Whitney: Amendment
39–15322. Docket No. FAA–2007–27230;
Directorate Identifier 2007–NE–04–AD.
Effective Date
(a) This airworthiness directive (AD)
becomes effective February 7, 2008.
(b) None.
Applicability
(c) This AD applies to Pratt & Whitney
PW4164, PW4168, and PW4168A turbofan
engines with certain low pressure turbine
(LPT) stage 4 disks, part number (P/N)
51N404, that have a serial number (S/N)
listed in the following Table 1, installed.
These engines are installed on, but not
limited to, Airbus A330–200 and A330–300
series airplanes.
TABLE 1.—AFFECTED LPT STAGE 4
DISKS BY SERIAL NUMBER
LPT Stage 4 Disk Serial Nos.
CLDLC01142
CLDLC01143
CLDLC01144
CLDLC01145
CLDLC01146
CLDLC01148
CLDLC01149
CLDLC01150
CLDLC01151
CLDLC01152
CLDLC01181
CLDLC01182
CLDLC01183
CLDLC01185
CLDLC01186
CLDLC01187
Prohibition Against Installing an Affected
Disk
(g) After the effective date of this AD, do
not install any disk, P/N 51N404, that has an
S/N listed in Table 1 of this AD or any disk
removed as specified in paragraph (f) of this
AD except as allowed by paragraph (h) of this
AD.
Alternative Methods of Compliance
(h) The Manager, Engine Certification
Office, has the authority to approve
alternative methods of compliance for this
AD if requested using the procedures found
in 14 CFR 39.19.
Related Information
(j) Contact V. Rose Len, Aerospace
Engineer, Engine Certification Office, FAA,
Engine & Propeller Directorate, 12 New
England Executive Park, Burlington, MA
01803; telephone (781) 238–7772; fax (781)
238–7199, for more information about this
AD.
Material Incorporated by Reference
(k) None.
Issued in Burlington, Massachusetts, on
December 20, 2007.
Peter A. White,
Assistant Manager, Engine and Propeller
Directorate, Aircraft Certification Service.
[FR Doc. E7–25505 Filed 1–2–08; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2007–0379; Directorate
Identifier 2007–NM–331–AD; Amendment
39–15318; AD 2007–26–16]
RIN 2120–AA64
Airworthiness Directives; Cessna
Model 680 Airplanes
Unsafe Condition
(d) This AD results from a report of
improperly manufactured LPT stage 4 disks.
We are issuing this AD to prevent an
uncontained engine failure due to low-cycle
fatigue, which could result in damage to the
airplane.
Compliance
(e) You are responsible for having the
actions required by this AD performed at the
next piece-part exposure after the effective
date of this AD or within 7,500 cycles-sincenew, unless the actions have already been
done.
Frm 00007
Removing the LPT Stage 4 Disk
(f) Remove from service any LPT stage 4
disk that has an S/N listed in Table 1 of this
AD.
Special Flight Permits
(i) Under 14 CFR part 39.23, we are
prohibiting the special flight permits for this
AD.
Affected ADs
PO 00000
395
Fmt 4700
Sfmt 4700
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule; request for
comments.
AGENCY:
SUMMARY: We are adopting a new
airworthiness directive (AD) for certain
Cessna Model 680 airplanes. This AD
requires inspecting the routing of the aft
fairing wire bundle assembly for
adequate separation between the wiring
and the hydraulic line; inspecting for
chafing or damage of the wire bundle
E:\FR\FM\03JAR1.SGM
03JAR1
396
Federal Register / Vol. 73, No. 2 / Thursday, January 3, 2008 / Rules and Regulations
assembly and for damage to the
hydraulic line, and doing corrective
actions if necessary. This AD results
from an incident report which indicated
that a hydraulic leak and wire chafing,
including signs of heat damage, were
found within the lower tail cone fairing
area. Similar wire chafing has also been
found on other airplanes. We are issuing
this AD to detect and correct wire
chafing, and inadequate separation of
the wiring and hydraulic line, which
could lead to electrical arcing and a
hydraulic leak and could result in a
potential source of ignition and
consequent fire.
DATES: This AD is effective January 18,
2008.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in this AD
as of February 7, 2008.
We must receive comments on this
AD by March 3, 2008.
ADDRESSES: You may send comments by
any of the following methods:
• 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 AD, contact Cessna Aircraft Co.,
P.O. Box 7706, Wichita, Kansas 67277.
jlentini on PROD1PC65 with RULES
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 street address for
the Docket Office (telephone 800–647–
5527) is in the ADDRESSES section.
Comments will be available in the AD
docket shortly after receipt.
FOR FURTHER INFORMATION CONTACT:
Jarrett Larrow, Aerospace Engineer,
Electrical Systems and Avionics, ACE–
119W, FAA, Wichita Aircraft
Certification Office, 1801 Airport Road,
Room 100, Mid-Continent Airport,
Wichita, Kansas 67209; telephone (316)
946–4128; fax (316) 946–4107.
VerDate Aug<31>2005
16:54 Jan 02, 2008
Jkt 214001
SUPPLEMENTARY INFORMATION:
Discussion
We received an incident report which
indicated that a hydraulic leak and wire
chafing, including signs of heat damage,
were found within the lower tail cone
fairing area on a Cessna Model 680
airplane. The incident occurred while
the airplane was on the ground. Wire
chafing has also been found on other
airplanes. Chafing of the wiring, and
inadequate separation of the wiring and
hydraulic line, could lead to electrical
arcing and a hydraulic leak and could
result in a potential source of ignition
and consequent fire.
Relevant Service Information
We reviewed Cessna Alert Service
Letter ASL680–24–02, dated October 1,
2007. The service letter describes
procedures for inspecting the routing of
the aft fairing wire bundle assembly for
adequate separation between the wiring
and the hydraulic line; inspecting for
chafing or damage of the wire bundle
assembly and for damage to the
hydraulic line; and corrective actions if
necessary. The corrective actions
include repairing the wiring if any
damage to the wire bundle is found,
replacing the hydraulic line if any
damage is found, and re-routing the
wire bundle so there is a minimum of
two inches from the hydraulic line. The
service letter refers to the Model 680
wiring diagram and maintenance
manuals, which contain the procedures
for doing the corrective actions.
FAA’s Determination and Requirements
of This AD
We are issuing this AD because we
evaluated all the relevant information
and determined the unsafe condition
described previously is likely to exist or
develop in other products of the same
type design. This AD requires
accomplishing the actions specified in
the service information described
previously, except as discussed under
‘‘Differences Between the AD and the
Service Information.’’
Differences Between the AD and the
Service Information
The service information refers only to
an ‘‘inspection’’ for routing and chafing
or damage of the wire bundles and
hydraulic line. We have determined that
the procedures in the service
information should be described as a
‘‘general visual inspection.’’ Note 1 has
been included in this AD to define this
type of inspection.
The Accomplishment Instructions of
the service information describe
procedures for completing a
PO 00000
Frm 00008
Fmt 4700
Sfmt 4700
maintenance transaction report and
submitting a copy to the manufacturer.
This AD would not require that action.
Interim Action
We consider this AD interim action. If
final action is later identified, we might
consider further rulemaking then.
FAA’s Determination of the Effective
Date
An unsafe condition exists that
requires the immediate adoption of this
AD; therefore, providing notice and
opportunity for public comment before
the AD is issued is impracticable, and
good cause exists to make this AD
effective in less than 30 days.
Comments Invited
This AD is a final rule that involves
requirements affecting flight safety, and
we did not provide you with notice and
an opportunity to provide your
comments before it becomes effective.
However, we invite you to send any
written data, views, or arguments about
this AD. Send your comments to an
address listed under the ADDRESSES
section. Include ‘‘Docket No. FAA–
2007–0379; Directorate Identifier 2007–
NM–331–AD’’ at the beginning of your
comments. We specifically invite
comments on the overall regulatory,
economic, environmental, and energy
aspects of this AD. We will consider all
comments received by the closing date
and may amend this AD because 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
about this AD.
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
E:\FR\FM\03JAR1.SGM
03JAR1
Federal Register / Vol. 73, No. 2 / Thursday, January 3, 2008 / Rules and Regulations
products identified in this rulemaking
action.
Regulatory Findings
This AD will not have federalism
implications under Executive Order
13132. This AD will not have a
substantial direct effect on the States, on
the relationship between the national
government and the States, or on the
distribution of power and
responsibilities among the various
levels of government.
For the reasons discussed above, I
certify that this AD:
(1) Is not a ‘‘significant regulatory
action’’ under Executive Order 12866,
(2) Is not a ‘‘significant rule’’ under
DOT Regulatory Policies and Procedures
(44 FR 11034, February 26, 1979), and
(3) Will not have a significant
economic impact, positive or negative,
on a substantial number of small entities
under the criteria of the Regulatory
Flexibility Act.
You can find our regulatory
evaluation and the estimated costs of
compliance in the AD Docket.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
Adoption of the Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
I
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
I
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new AD:
I
2007–26–16 Cessna Aircraft Company:
Amendment 39–15318. Docket No.
FAA–2007–0379; Directorate Identifier
2007–NM–331–AD.
Effective Date
(a) This airworthiness directive (AD) is
effective January 18, 2008.
jlentini on PROD1PC65 with RULES
Affected ADs
(b) None.
Applicability
(c) This AD applies to Cessna Model 680
airplanes, certificated in any category, serial
numbers –0001 through –0152 inclusive,
–0157, and –0158.
Unsafe Condition
(d) This AD results from an incident report
which indicated that a hydraulic leak and
VerDate Aug<31>2005
16:54 Jan 02, 2008
Jkt 214001
wire chafing, including signs of heat damage,
were found within the lower tail cone fairing
area. Similar wire chafing has also been
found on other airplanes. We are issuing this
AD to detect and correct wire chafing, and
inadequate separation of the wiring and
hydraulic line, which could lead to electrical
arcing and a hydraulic leak and could result
in a potential source of ignition and
consequent fire.
Compliance
(e) Comply with this AD within the
compliance times specified, unless already
done.
Inspections/Corrective Actions
(f) Within 10 days after the effective date
of this AD: Do a general visual inspection of
the routing of the aft fairing wire bundle
assembly for adequate separation between
the wiring and the hydraulic line, and do a
general visual inspection for chafing or
damage of the wire bundle assembly and for
damage to the hydraulic line; by doing all of
the actions, including all applicable
corrective actions, specified in the
Accomplishment Instructions of Cessna Alert
Service Letter ASL680–24–02, dated October
1, 2007; except as provided by paragraph (g)
of this AD. Do all applicable corrective
actions before further flight.
Note 1: For the purposes of this AD, a
general visual inspection is: ‘‘A visual
examination of an interior or exterior area,
installation, or assembly to detect obvious
damage, failure, or irregularity. This level of
inspection is made from within touching
distance unless otherwise specified. A mirror
may be necessary to ensure visual access to
all surfaces in the inspection area. This level
of inspection is made under normally
available lighting conditions such as
daylight, hangar lighting, flashlight, or
droplight and may require removal or
opening of access panels or doors. Stands,
ladders, or platforms may be required to gain
proximity to the area being checked.’’
Exception to Alert Service Letter
(g) Although the Accomplishment
Instructions of Cessna Alert Service Letter
ASL680–24–02, dated October 1, 2007,
specify to submit certain information to the
manufacturer, this AD does not include that
requirement.
Alternative Methods of Compliance
(AMOCs)
(h)(1) The Manager, Electrical Systems and
Avionics, ACE–119W, FAA, ATTN: Jarrett
Larrow, Aerospace Engineer, Electrical
Systems and Avionics, ACE–119W, FAA,
Wichita Aircraft Certification Office, 1801
Airport Road, room 100, Mid-Continent
Airport, Wichita, Kansas 67209; telephone
(316) 946–4128; fax (316) 946–4107; has the
authority to approve AMOCs for this AD, if
requested using the procedures found in 14
CFR 39.19.
(2) To request a different method of
compliance or a different compliance time
for this AD, follow the procedures in 14 CFR
39.19. Before using any approved AMOC on
any airplane to which the AMOC applies,
notify your appropriate principal inspector
PO 00000
Frm 00009
Fmt 4700
Sfmt 4700
397
(PI) in the FAA Flight Standards District
Office (FSDO), or lacking a PI, your local
FSDO.
Material Incorporated by Reference
(i) You must use Cessna Alert Service
Letter ASL680–24–02, dated October 1, 2007,
to do the actions required by this AD, unless
the AD specifies otherwise.
(1) The Director of the Federal Register
approved the incorporation by reference of
this service information under 5 U.S.C.
552(a) and 1 CFR part 51.
(2) For service information identified in
this AD, contact Cessna Aircraft Co., P.O. Box
7706, Wichita, Kansas 67277.
(3) You may review copies of the service
information incorporated by reference at the
FAA, Transport Airplane Directorate, 1601
Lind Avenue SW., Renton, Washington; or at
the National Archives and Records
Administration (NARA). For information on
the availability of this material at NARA, call
202–741–6030, or go to: https://
www.archives.gov/federal_register/
code_of_federal_regulations/
ibr_locations.html.
Issued in Renton, Washington, on
December 20, 2007.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 07–6265 Filed 1–2–08; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2007–0378; Directorate
Identifier 2007–SW–04–AD; Amendment 39–
15314; AD 2007–26–12]
RIN 2120–AA64
Airworthiness Directives; Robinson
Helicopter Company Models R22, R22
Alpha, R22 Beta, R22 Mariner, R44 and
R44 II Helicopters
Federal Aviation
Administration, DOT.
ACTION: Final rule; request for
comments.
AGENCY:
SUMMARY: This amendment adopts a
new airworthiness directive (AD) for the
specified Robinson Helicopter Company
(Robinson) helicopters. This action
requires a one-time visual inspection for
skin separation along the leading edge
of blade skin aft of the skin-to-spar bond
line on the lower surface of each blade
and in the tip cap area. This action also
requires a ‘‘tap test’’ for detecting a
separation or void in both bonded areas.
This action also requires repainting any
exposed area of the blades. If any
separation or void is detected, replacing
the blade before further flight is
E:\FR\FM\03JAR1.SGM
03JAR1
]]>Agencies
[Federal Register Volume 73, Number 2 (Thursday, January 3, 2008)]
[Rules and Regulations]
[Pages 395-397]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 07-6265]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2007-0379; Directorate Identifier 2007-NM-331-AD;
Amendment 39-15318; AD 2007-26-16]
RIN 2120-AA64
Airworthiness Directives; Cessna Model 680 Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; request for comments.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for certain
Cessna Model 680 airplanes. This AD requires inspecting the routing of
the aft fairing wire bundle assembly for adequate separation between
the wiring and the hydraulic line; inspecting for chafing or damage of
the wire bundle
[[Page 396]]
assembly and for damage to the hydraulic line, and doing corrective
actions if necessary. This AD results from an incident report which
indicated that a hydraulic leak and wire chafing, including signs of
heat damage, were found within the lower tail cone fairing area.
Similar wire chafing has also been found on other airplanes. We are
issuing this AD to detect and correct wire chafing, and inadequate
separation of the wiring and hydraulic line, which could lead to
electrical arcing and a hydraulic leak and could result in a potential
source of ignition and consequent fire.
DATES: This AD is effective January 18, 2008.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of February 7,
2008.
We must receive comments on this AD by March 3, 2008.
ADDRESSES: You may send comments by any of the following methods:
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 AD, contact Cessna
Aircraft Co., P.O. Box 7706, Wichita, Kansas 67277.
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 street address for
the Docket Office (telephone 800-647-5527) is in the ADDRESSES section.
Comments will be available in the AD docket shortly after receipt.
FOR FURTHER INFORMATION CONTACT: Jarrett Larrow, Aerospace Engineer,
Electrical Systems and Avionics, ACE-119W, FAA, Wichita Aircraft
Certification Office, 1801 Airport Road, Room 100, Mid-Continent
Airport, Wichita, Kansas 67209; telephone (316) 946-4128; fax (316)
946-4107.
SUPPLEMENTARY INFORMATION:
Discussion
We received an incident report which indicated that a hydraulic
leak and wire chafing, including signs of heat damage, were found
within the lower tail cone fairing area on a Cessna Model 680 airplane.
The incident occurred while the airplane was on the ground. Wire
chafing has also been found on other airplanes. Chafing of the wiring,
and inadequate separation of the wiring and hydraulic line, could lead
to electrical arcing and a hydraulic leak and could result in a
potential source of ignition and consequent fire.
Relevant Service Information
We reviewed Cessna Alert Service Letter ASL680-24-02, dated October
1, 2007. The service letter describes procedures for inspecting the
routing of the aft fairing wire bundle assembly for adequate separation
between the wiring and the hydraulic line; inspecting for chafing or
damage of the wire bundle assembly and for damage to the hydraulic
line; and corrective actions if necessary. The corrective actions
include repairing the wiring if any damage to the wire bundle is found,
replacing the hydraulic line if any damage is found, and re-routing the
wire bundle so there is a minimum of two inches from the hydraulic
line. The service letter refers to the Model 680 wiring diagram and
maintenance manuals, which contain the procedures for doing the
corrective actions.
FAA's Determination and Requirements of This AD
We are issuing this AD because we evaluated all the relevant
information and determined the unsafe condition described previously is
likely to exist or develop in other products of the same type design.
This AD requires accomplishing the actions specified in the service
information described previously, except as discussed under
``Differences Between the AD and the Service Information.''
Differences Between the AD and the Service Information
The service information refers only to an ``inspection'' for
routing and chafing or damage of the wire bundles and hydraulic line.
We have determined that the procedures in the service information
should be described as a ``general visual inspection.'' Note 1 has been
included in this AD to define this type of inspection.
The Accomplishment Instructions of the service information describe
procedures for completing a maintenance transaction report and
submitting a copy to the manufacturer. This AD would not require that
action.
Interim Action
We consider this AD interim action. If final action is later
identified, we might consider further rulemaking then.
FAA's Determination of the Effective Date
An unsafe condition exists that requires the immediate adoption of
this AD; therefore, providing notice and opportunity for public comment
before the AD is issued is impracticable, and good cause exists to make
this AD effective in less than 30 days.
Comments Invited
This AD is a final rule that involves requirements affecting flight
safety, and we did not provide you with notice and an opportunity to
provide your comments before it becomes effective. However, we invite
you to send any written data, views, or arguments about this AD. Send
your comments to an address listed under the ADDRESSES section. Include
``Docket No. FAA-2007-0379; Directorate Identifier 2007-NM-331-AD'' at
the beginning of your comments. We specifically invite comments on the
overall regulatory, economic, environmental, and energy aspects of this
AD. We will consider all comments received by the closing date and may
amend this AD because 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 about this AD.
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
[[Page 397]]
products identified in this rulemaking action.
Regulatory Findings
This AD will not have federalism implications under Executive Order
13132. This AD will not have a substantial direct effect on the States,
on the relationship between the national government and the States, or
on the distribution of power and responsibilities among the various
levels of government.
For the reasons discussed above, I certify that this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Is not a ``significant rule'' under DOT Regulatory Policies and
Procedures (44 FR 11034, February 26, 1979), and
(3) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
You can find our regulatory evaluation and the estimated costs of
compliance in the AD Docket.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
0
Accordingly, under the authority delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by adding the following new AD:
2007-26-16 Cessna Aircraft Company: Amendment 39-15318. Docket No.
FAA-2007-0379; Directorate Identifier 2007-NM-331-AD.
Effective Date
(a) This airworthiness directive (AD) is effective January 18,
2008.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Cessna Model 680 airplanes, certificated
in any category, serial numbers -0001 through -0152 inclusive, -
0157, and -0158.
Unsafe Condition
(d) This AD results from an incident report which indicated that
a hydraulic leak and wire chafing, including signs of heat damage,
were found within the lower tail cone fairing area. Similar wire
chafing has also been found on other airplanes. We are issuing this
AD to detect and correct wire chafing, and inadequate separation of
the wiring and hydraulic line, which could lead to electrical arcing
and a hydraulic leak and could result in a potential source of
ignition and consequent fire.
Compliance
(e) Comply with this AD within the compliance times specified,
unless already done.
Inspections/Corrective Actions
(f) Within 10 days after the effective date of this AD: Do a
general visual inspection of the routing of the aft fairing wire
bundle assembly for adequate separation between the wiring and the
hydraulic line, and do a general visual inspection for chafing or
damage of the wire bundle assembly and for damage to the hydraulic
line; by doing all of the actions, including all applicable
corrective actions, specified in the Accomplishment Instructions of
Cessna Alert Service Letter ASL680-24-02, dated October 1, 2007;
except as provided by paragraph (g) of this AD. Do all applicable
corrective actions before further flight.
Note 1: For the purposes of this AD, a general visual inspection
is: ``A visual examination of an interior or exterior area,
installation, or assembly to detect obvious damage, failure, or
irregularity. This level of inspection is made from within touching
distance unless otherwise specified. A mirror may be necessary to
ensure visual access to all surfaces in the inspection area. This
level of inspection is made under normally available lighting
conditions such as daylight, hangar lighting, flashlight, or
droplight and may require removal or opening of access panels or
doors. Stands, ladders, or platforms may be required to gain
proximity to the area being checked.''
Exception to Alert Service Letter
(g) Although the Accomplishment Instructions of Cessna Alert
Service Letter ASL680-24-02, dated October 1, 2007, specify to
submit certain information to the manufacturer, this AD does not
include that requirement.
Alternative Methods of Compliance (AMOCs)
(h)(1) The Manager, Electrical Systems and Avionics, ACE-119W,
FAA, ATTN: Jarrett Larrow, Aerospace Engineer, Electrical Systems
and Avionics, ACE-119W, FAA, Wichita Aircraft Certification Office,
1801 Airport Road, room 100, Mid-Continent Airport, Wichita, Kansas
67209; telephone (316) 946-4128; fax (316) 946-4107; has the
authority to approve AMOCs for this AD, if requested using the
procedures found in 14 CFR 39.19.
(2) To request a different method of compliance or a different
compliance time for this AD, follow the procedures in 14 CFR 39.19.
Before using any approved AMOC on any airplane to which the AMOC
applies, notify your appropriate principal inspector (PI) in the FAA
Flight Standards District Office (FSDO), or lacking a PI, your local
FSDO.
Material Incorporated by Reference
(i) You must use Cessna Alert Service Letter ASL680-24-02, dated
October 1, 2007, to do the actions required by this AD, unless the
AD specifies otherwise.
(1) The Director of the Federal Register approved the
incorporation by reference of this service information under 5
U.S.C. 552(a) and 1 CFR part 51.
(2) For service information identified in this AD, contact
Cessna Aircraft Co., P.O. Box 7706, Wichita, Kansas 67277.
(3) You may review copies of the service information
incorporated by reference at the FAA, Transport Airplane
Directorate, 1601 Lind Avenue SW., Renton, Washington; or at the
National Archives and Records Administration (NARA). For information
on the availability of this material at NARA, call 202-741-6030, or
go to: https://www.archives.gov/federal_register/code_of_federal_
regulations/ibr_locations.html.
Issued in Renton, Washington, on December 20, 2007.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 07-6265 Filed 1-2-08; 8:45 am]
BILLING CODE 4910-13-P
