Airworthiness Directives; Cessna Aircraft Company Models 182Q and 182R Airplanes, 7808-7810 [E9-2993]
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7808
Federal Register / Vol. 74, No. 33 / Friday, February 20, 2009 / Rules and Regulations
eas@airbus.com; Internet https://
www.airbus.com.
(4) You may review copies of the service
information that is incorporated by reference
at the FAA, Transport Airplane Directorate,
1601 Lind Avenue, SW., Renton,
Washington. For information on the
availability of this material at the FAA, call
425–227–1221 or 425–227–1152.
(5) You may also review copies of the
service information 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 18, 2008.
Stephen P. Boyd,
Assistant Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. E9–3276 Filed 2–19–09; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2008–1205; Directorate
Identifier 2008–CE–062–AD; Amendment
39–15811; AD 2009–04–05]
RIN 2120–AA64
Airworthiness Directives; Cessna
Aircraft Company Models 182Q and
182R Airplanes
AGENCY: Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
SUMMARY: We are adopting a new
airworthiness directive (AD) for certain
Cessna Aircraft Company (Cessna)
Models 182Q and 182R airplanes that
´
are equipped with Societe de
´
Motorisations Aeronautiques (SMA)
Aircraft Diesel Engine (ADE) Model
SR305–230–1 or Model SR305–230
converted to Model SR305–230–1
installed under Supplemental Type
Certificate (STC) SA03302AT. This AD
requires you to remove the intercooler
and the intercooler inlet and outlet
hoses, install a reworked intercooler and
new intercooler inlet and outlet hoses,
inspect hoses and clamp torques,
repetitively inspect installation of the
intercooler outlet and inlet hose
assemblies for any displacement or
damage of clamps or hoses, and, if
necessary, replace any damaged clamps
or hoses. This AD results from a report
of two instances of induction hose
disconnection occurring while in
service, resulting in a loss of turbo boost
and a significant loss of engine power.
We are issuing this AD to detect and
correct improper intercooler outlet and
intercooler inlet hose assembly
installations, which could result in loss
of turbo boost and a significant loss of
engine power. This failure could lead to
an inability to maintain constant
altitude in flight.
DATES: This AD becomes effective on
March 27, 2009.
On March 27, 2009, the Director of the
Federal Register approved the
incorporation by reference of certain
publications listed in this AD.
ADDRESSES: For service information
identified in this AD, contact SMA
Customer Service, 10–12 Rue Didier
Daurat, 18021 Bourges, France;
telephone: +33 (0) 2 48 67 56 00; fax:
+33 (0) 2 48 50 01 41; E-mail:
customer_services@smasr.com; Internet:
https://www.smaengines.com.
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. The docket
number is FAA–2008–1205; Directorate
Identifier 2008–CE–062–AD.
FOR FURTHER INFORMATION CONTACT: Don
O. Young, Aerospace Engineer, ACE–
118A, Atlanta Aircraft Certification
Office, One Crown Center, 1895 Phoenix
Blvd., Suite 450, Atlanta, Georgia 30349;
telephone: (770) 703–6079; fax: (770)
703–6097.
SUPPLEMENTARY INFORMATION:
Discussion
On November 6, 2008, we issued a
proposal to amend part 39 of the Federal
Aviation Regulations (14 CFR part 39) to
include an AD that would apply to
certain Cessna Models 182Q and 182R
airplanes that are equipped with SMA
ADE Model SR305–230–1 or Model
SR305–230 converted to Model SR305–
230–1 installed under STC SA03302AT.
This proposal was published in the
Federal Register as a notice of proposed
rulemaking (NPRM) on November 13,
2008 (73 FR 67112). The NPRM
proposed to require you to remove the
intercooler and the intercooler inlet and
outlet hoses, install a reworked
intercooler and new intercooler inlet
and outlet hoses, inspect hoses and
clamp torques, repetitively inspect
installation of the intercooler outlet and
inlet hose assemblies for any
displacement or damage of clamps or
hoses, and, if necessary, replace any
damaged clamps or hoses.
Comments
We provided the public the
opportunity to participate in developing
this AD. We received no comments on
the proposal 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 except for
minor editorial corrections. We have
determined that these minor
corrections:
• Are consistent with the intent that
was proposed in the NPRM for
correcting the unsafe condition; and
• Do not add any additional burden
upon the public than was already
proposed in the NPRM.
Costs of Compliance
We estimate that this AD affects 7
airplanes in the U.S. registry.
We estimate the following costs to do
the replacements:
Labor cost
Parts cost
Total cost per
airplane
Total cost on
U.S. operators
4 work-hours × $80 per hour = $320 ..........................................................................................
$3,436
$3,756
$26,292
We estimate the following costs to do
any inspection of the installation of the
intercooler hose assembly that would be
required:
Labor cost
Parts cost
Total cost per
airplane
2 work-hours × $80 per hour = $160 ...........................................................................
Not Applicable ...........................................
$160
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Federal Register / Vol. 74, No. 33 / Friday, February 20, 2009 / Rules and Regulations
We have no way of determining the
cost of any necessary replacement that
may be required as a result of any
inspection.
SMA will provide warranty credit as
stated in SMA SAFRAN Group Service
Bulletin SB–C182–75–004, Revision No.
Basic Issue, dated July 8, 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 AD.
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 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 summary of the costs
to comply with this AD (and other
information as included in the
Regulatory Evaluation) and placed it in
the AD Docket. You may get a copy of
this summary by sending a request to us
at the address listed under ADDRESSES.
Include ‘‘Docket No. FAA–2008–1205;
Directorate Identifier 2008–CE–062–
AD’’ in your request.
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 Federal Aviation Administration
amends part 39 of the Federal Aviation
Regulations (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.
§ 39.13
7809
[Amended]
2. FAA amends § 39.13 by adding the
following new AD:
■
2009–04–05 Cessna Aircraft Company:
Amendment 39–15811; Docket No.
FAA–2008–1205; Directorate Identifier
2008–CE–062–AD.
Effective Date
(a) This AD becomes effective on March 27,
2009.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Models 182Q and
182R airplanes, all serial numbers,
certificated in any category, that are
equipped with:
´
´
(1) Societe de Motorisations Aeronautiques
(SMA) aircraft diesel engine (ADE) Model
SR305–230–1 installed under Supplemental
Type Certificate (STC) SA03302AT; or
(2) SMA ADE Model SR305–230 converted
to Model SR305–230–1 (by incorporation of
SMA Service Bulletin SB–01–76–002)
installed under STC SA03302AT.
Unsafe Condition
(d) This AD results from a report of two
instances of induction hose disconnection
occurring while in service on the air inlet
manifold circuit, resulting in a loss of turbo
boost and a significant loss of engine power.
We are issuing this AD to detect and correct
improper intercooler hose assembly
installation, which could result in loss of
turbo boost and a significant loss of engine
power. This failure could lead to an inability
to maintain constant altitude in flight.
Compliance
(e) To address this problem, you must do
the following, unless already done:
Actions
Compliance
Procedures
(1) Remove intercooler part number (P/N)
SF01170004–0 and install reworked intercooler P/N SF01170004–1 and remove intercooler inlet and outlet hoses and install new
intercooler inlet hose P/N SF01170083–0 and
intercooler outlet hose P/N SF01170048–0.
(2) Inspect intercooler inlet and outlet hoses
and clamps for displacement and re-torque
clamps. If you find any displacement do the
displacement recovery.
(3) Inspect the installation of the intercooler outlet hose and intercooler inlet hose assembly
for any displacement or damage of clamps or
hoses.
Before further flight as of March 27, 2009 (the
effective date of this AD).
Follow SMA SAFRAN Group Service Bulletin
SB–C182–75–004, Revision No. Basic
Issue, dated July 8, 2008.
Within the next 25 hours time-in-service (TIS)
following installation required by paragraph
(e)(1) of this AD.
Follow SMA SAFRAN Group Service Bulletin
SB–C182–75–004, Revision No. Basic
Issue, dated July 8, 2008.
Initially inspect within the next 100 hours TIS
after the action required by paragraph (e)(1)
of this AD or within the next 12 months
after the action required by paragraph (e)(1)
of this AD, whichever occurs first. Repetitively thereafter inspect at intervals not to
exceed 100 hours TIS or 12 months, whichever occurs first.
Before further flight, after the inspection required by paragraph (e)(3) of this AD where
you found any displacement or damage of
clamps or hoses.
As of March 27, 2009 (the effective date of
this AD).
Follow SMA SAFRAN Group Service Bulletin
SB–C182–75–004, Revision No. Basic
Issue, dated July 8, 2008.
(4) If, as a result of any inspection required by
paragraph (e)(3) of this AD, you find any displacement or damage of clamps or hoses, replace any damaged clamps and hoses.
(5) Do not install any intercooler P/N
SF01170004–0.
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Sfmt 4700
Follow SMA SAFRAN Group Service Bulletin
SB–C182–75–004, Revision No. Basic
Issue, dated July 8, 2008.
Not Applicable.
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Federal Register / Vol. 74, No. 33 / Friday, February 20, 2009 / Rules and Regulations
Special Flight Permit
DEPARTMENT OF TRANSPORTATION)
(f) Under 14 CFR part 39.23, we are
limiting the special flight permits for this AD
by the following conditions:
(1) Before flight, an inspection of hoses and
clamps by a properly certificated mechanic
reveals no damaged or disconnected hoses or
clamps; and
(2) You fly by the most direct route to the
site where the AD can be performed.
Alternative Methods of Compliance
(AMOCs)
(g) The Manager, Atlanta 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: Don
O. Young, Aerospace Engineer, ACE–118A,
Atlanta ACO, One Crown Center, 1895
Phoenix Blvd., Suite 450, Atlanta, Georgia
30349; telephone: (770) 703–6079; fax: (770)
703–6097. 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
(h) You must use SMA SAFRAN Group
Service Bulletin SB–C182–75–004, Revision
No. Basic Issue, dated July 8, 2008, to do the
actions required by this AD, unless the AD
specifies otherwise.
(1) The Director of the Federal Register
approved the incorporation by reference of
this service information under 5 U.S.C.
552(a) and 1 CFR part 51.
(2) For service information identified in
this AD, contact SMA Customer Service, 10–
12 Rue Didier Daurat, 18021 Bourges, France;
telephone: +33 (0) 2 48 67 56 00; fax: +33 (0)
2 48 50 01 41; E-mail:
customer_services@smasr.com; Internet:
https://www.smaengines.com.
(3) You may review copies of the service
information incorporated by reference for
this AD at the FAA, Central Region, Office of
the Regional Counsel, 901 Locust, Kansas
City, Missouri 64106. For information on the
availability of this material at the Central
Region, call (816) 329–3768.
(4) You may also review copies of the
service information incorporated by reference
for this AD 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 Kansas City, Missouri, on
February 6, 2009.
Kim Smith,
Manager, Small Airplane Directorate, Aircraft
Certification Service.
[FR Doc. E9–2993 Filed 2–19–09; 8:45 am]
BILLING CODE 4910–13–P
VerDate Nov<24>2008
16:40 Feb 19, 2009
Jkt 217001
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2009–0146; Directorate
Identifier 2009–CE–009–AD; Amendment
39–15820; AD 2009–04–14]
RIN 2120–AA64
Airworthiness Directives; PILATUS
AIRCRAFT LTD. Model PC–12/47E
Airplanes
AGENCY: Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule; request for
comments.
We are adopting a new
airworthiness directive (AD) for the
products listed above. This AD results
from mandatory continuing
airworthiness information (MCAI)
issued by the aviation authority of
another country to identify and correct
an unsafe condition on an aviation
product. The MCAI describes the unsafe
condition as:
SUMMARY:
Field reports have indicated that during
take-off with light turbulences or after rapid
roll/heading attitude changes soon after takeoff, it is possible that both PFDs (Primary
Flight Display) indicate a roll attitude offset
of up to 10 degrees in the same direction.
This condition has been reported to correct
itself after several minutes of un-accelerated
flight with levelled wings and no sideslip.
This situation, if not corrected, could result
in an undesired bank angle which constitutes
an unsafe condition.
This AD requires actions that are
intended to address the unsafe
condition described in the MCAI.
DATE: This AD becomes effective
February 20, 2009.
We must receive comments on this
AD by March 23, 2009.
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.
Examining the AD Docket
You may examine the AD docket on
the Internet at https://
PO 00000
Frm 00034
Fmt 4700
Sfmt 4700
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:
Doug Rudolph, Aerospace Engineer,
FAA, Small Airplane Directorate, 901
Locust, Room 301, Kansas City,
Missouri 64016; telephone: (816) 329–
4059; fax: (816) 329–4090.
SUPPLEMENTARY INFORMATION:
Discussion
The European Aviation Safety Agency
(EASA), which is the Technical Agent
for the Member States of the European
Community, has issued Emergency AD
No. 2009–0028–E, dated February 11,
2009 (referred to after this as ‘‘the
MCAI’’), to correct an unsafe condition
for the specified products. The MCAI
states:
Field reports have indicated that during
take-off with light turbulences or after rapid
roll/heading attitude changes soon after takeoff, it is possible that both PFDs (Primary
Flight Display) indicate a roll attitude offset
of up to 10 degrees in the same direction.
This condition has been reported to correct
itself after several minutes of un-accelerated
flight with levelled wings and no sideslip.
This situation, if not corrected, could result
in an undesired bank angle which constitutes
an unsafe condition.
For the reason described above, this
Airworthiness Directive (AD) mandates as an
interim measure a revision of the operational
procedures to be inserted into the Pilot’s
Operating Handbook (POH).
You may obtain further information by
examining the MCAI in the AD docket.
FAA’s Determination and Requirements
of the AD
This product has been approved by
the aviation authority of another
country, and is approved for operation
in the United States. Pursuant to our
bilateral agreement with this State of
Design Authority, they have notified us
of the unsafe condition described in the
MCAI and service information
referenced above. We are issuing this
AD because we evaluated all
information provided by the State of
Design Authority and determined the
unsafe condition exists and is likely to
exist or develop on other products of the
same type design.
E:\FR\FM\20FER1.SGM
20FER1
]]>Agencies
[Federal Register Volume 74, Number 33 (Friday, February 20, 2009)]
[Rules and Regulations]
[Pages 7808-7810]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E9-2993]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2008-1205; Directorate Identifier 2008-CE-062-AD;
Amendment 39-15811; AD 2009-04-05]
RIN 2120-AA64
Airworthiness Directives; Cessna Aircraft Company Models 182Q and
182R Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for certain
Cessna Aircraft Company (Cessna) Models 182Q and 182R airplanes that
are equipped with Societ[eacute] de Motorisations A[eacute]ronautiques
(SMA) Aircraft Diesel Engine (ADE) Model SR305-230-1 or Model SR305-230
converted to Model SR305-230-1 installed under Supplemental Type
Certificate (STC) SA03302AT. This AD requires you to remove the
intercooler and the intercooler inlet and outlet hoses, install a
reworked intercooler and new intercooler inlet and outlet hoses,
inspect hoses and clamp torques, repetitively inspect installation of
the intercooler outlet and inlet hose assemblies for any displacement
or damage of clamps or hoses, and, if necessary, replace any damaged
clamps or hoses. This AD results from a report of two instances of
induction hose disconnection occurring while in service, resulting in a
loss of turbo boost and a significant loss of engine power. We are
issuing this AD to detect and correct improper intercooler outlet and
intercooler inlet hose assembly installations, which could result in
loss of turbo boost and a significant loss of engine power. This
failure could lead to an inability to maintain constant altitude in
flight.
DATES: This AD becomes effective on March 27, 2009.
On March 27, 2009, the Director of the Federal Register approved
the incorporation by reference of certain publications listed in this
AD.
ADDRESSES: For service information identified in this AD, contact SMA
Customer Service, 10-12 Rue Didier Daurat, 18021 Bourges, France;
telephone: +33 (0) 2 48 67 56 00; fax: +33 (0) 2 48 50 01 41; E-mail:
customer_services@smasr.com; Internet: https://www.smaengines.com.
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. The docket number is FAA-2008-1205;
Directorate Identifier 2008-CE-062-AD.
FOR FURTHER INFORMATION CONTACT: Don O. Young, Aerospace Engineer, ACE-
118A, Atlanta Aircraft Certification Office, One Crown Center, 1895
Phoenix Blvd., Suite 450, Atlanta, Georgia 30349; telephone: (770) 703-
6079; fax: (770) 703-6097.
SUPPLEMENTARY INFORMATION:
Discussion
On November 6, 2008, we issued a proposal to amend part 39 of the
Federal Aviation Regulations (14 CFR part 39) to include an AD that
would apply to certain Cessna Models 182Q and 182R airplanes that are
equipped with SMA ADE Model SR305-230-1 or Model SR305-230 converted to
Model SR305-230-1 installed under STC SA03302AT. This proposal was
published in the Federal Register as a notice of proposed rulemaking
(NPRM) on November 13, 2008 (73 FR 67112). The NPRM proposed to require
you to remove the intercooler and the intercooler inlet and outlet
hoses, install a reworked intercooler and new intercooler inlet and
outlet hoses, inspect hoses and clamp torques, repetitively inspect
installation of the intercooler outlet and inlet hose assemblies for
any displacement or damage of clamps or hoses, and, if necessary,
replace any damaged clamps or hoses.
Comments
We provided the public the opportunity to participate in developing
this AD. We received no comments on the proposal 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
except for minor editorial corrections. We have determined that these
minor corrections:
Are consistent with the intent that was proposed in the
NPRM for correcting the unsafe condition; and
Do not add any additional burden upon the public than was
already proposed in the NPRM.
Costs of Compliance
We estimate that this AD affects 7 airplanes in the U.S. registry.
We estimate the following costs to do the replacements:
----------------------------------------------------------------------------------------------------------------
Total cost per Total cost on
Labor cost Parts cost airplane U.S. operators
----------------------------------------------------------------------------------------------------------------
4 work-hours x $80 per hour = $320........................... $3,436 $3,756 $26,292
----------------------------------------------------------------------------------------------------------------
We estimate the following costs to do any inspection of the
installation of the intercooler hose assembly that would be required:
------------------------------------------------------------------------
Total cost per
Labor cost Parts cost airplane
------------------------------------------------------------------------
2 work-hours x $80 per hour = Not Applicable...... $160
$160.
------------------------------------------------------------------------
[[Page 7809]]
We have no way of determining the cost of any necessary replacement
that may be required as a result of any inspection.
SMA will provide warranty credit as stated in SMA SAFRAN Group
Service Bulletin SB-C182-75-004, Revision No. Basic Issue, dated July
8, 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 AD.
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 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 summary of the costs to comply with this AD (and
other information as included in the Regulatory Evaluation) and placed
it in the AD Docket. You may get a copy of this summary by sending a
request to us at the address listed under ADDRESSES. Include ``Docket
No. FAA-2008-1205; Directorate Identifier 2008-CE-062-AD'' in your
request.
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 Federal Aviation Administration amends part 39 of the Federal
Aviation Regulations (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. FAA amends Sec. 39.13 by adding the following new AD:
2009-04-05 Cessna Aircraft Company: Amendment 39-15811; Docket No.
FAA-2008-1205; Directorate Identifier 2008-CE-062-AD.
Effective Date
(a) This AD becomes effective on March 27, 2009.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Models 182Q and 182R airplanes, all
serial numbers, certificated in any category, that are equipped
with:
(1) Societ[eacute] de Motorisations A[eacute]ronautiques (SMA)
aircraft diesel engine (ADE) Model SR305-230-1 installed under
Supplemental Type Certificate (STC) SA03302AT; or
(2) SMA ADE Model SR305-230 converted to Model SR305-230-1 (by
incorporation of SMA Service Bulletin SB-01-76-002) installed under
STC SA03302AT.
Unsafe Condition
(d) This AD results from a report of two instances of induction
hose disconnection occurring while in service on the air inlet
manifold circuit, resulting in a loss of turbo boost and a
significant loss of engine power. We are issuing this AD to detect
and correct improper intercooler hose assembly installation, which
could result in loss of turbo boost and a significant loss of engine
power. This failure could lead to an inability to maintain constant
altitude in flight.
Compliance
(e) To address this problem, you must do the following, unless
already done:
------------------------------------------------------------------------
Actions Compliance Procedures
------------------------------------------------------------------------
(1) Remove intercooler part Before further Follow SMA SAFRAN
number (P/N) SF01170004-0 flight as of March Group Service
and install reworked 27, 2009 (the Bulletin SB-C182-75-
intercooler P/N SF01170004- effective date of 004, Revision No.
1 and remove intercooler this AD). Basic Issue, dated
inlet and outlet hoses and July 8, 2008.
install new intercooler
inlet hose P/N SF01170083-0
and intercooler outlet hose
P/N SF01170048-0.
(2) Inspect intercooler Within the next 25 Follow SMA SAFRAN
inlet and outlet hoses and hours time-in- Group Service
clamps for displacement and service (TIS) Bulletin SB-C182-75-
re-torque clamps. If you following 004, Revision No.
find any displacement do installation Basic Issue, dated
the displacement recovery. required by July 8, 2008.
paragraph (e)(1) of
this AD.
(3) Inspect the installation Initially inspect Follow SMA SAFRAN
of the intercooler outlet within the next 100 Group Service
hose and intercooler inlet hours TIS after the Bulletin SB-C182-75-
hose assembly for any action required by 004, Revision No.
displacement or damage of paragraph (e)(1) of Basic Issue, dated
clamps or hoses. this AD or within July 8, 2008.
the next 12 months
after the action
required by
paragraph (e)(1) of
this AD, whichever
occurs first.
Repetitively
thereafter inspect
at intervals not to
exceed 100 hours
TIS or 12 months,
whichever occurs
first.
(4) If, as a result of any Before further Follow SMA SAFRAN
inspection required by flight, after the Group Service
paragraph (e)(3) of this inspection required Bulletin SB-C182-75-
AD, you find any by paragraph (e)(3) 004, Revision No.
displacement or damage of of this AD where Basic Issue, dated
clamps or hoses, replace you found any July 8, 2008.
any damaged clamps and displacement or
hoses. damage of clamps or
hoses.
(5) Do not install any As of March 27, 2009 Not Applicable.
intercooler P/N SF01170004- (the effective date
0. of this AD).
------------------------------------------------------------------------
[[Page 7810]]
Special Flight Permit
(f) Under 14 CFR part 39.23, we are limiting the special flight
permits for this AD by the following conditions:
(1) Before flight, an inspection of hoses and clamps by a
properly certificated mechanic reveals no damaged or disconnected
hoses or clamps; and
(2) You fly by the most direct route to the site where the AD
can be performed.
Alternative Methods of Compliance (AMOCs)
(g) The Manager, Atlanta 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: Don O. Young, Aerospace Engineer, ACE-118A, Atlanta ACO, One
Crown Center, 1895 Phoenix Blvd., Suite 450, Atlanta, Georgia 30349;
telephone: (770) 703-6079; fax: (770) 703-6097. 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
(h) You must use SMA SAFRAN Group Service Bulletin SB-C182-75-
004, Revision No. Basic Issue, dated July 8, 2008, to do the actions
required by this AD, unless the AD specifies otherwise.
(1) The Director of the Federal Register approved the
incorporation by reference of this service information under 5
U.S.C. 552(a) and 1 CFR part 51.
(2) For service information identified in this AD, contact SMA
Customer Service, 10-12 Rue Didier Daurat, 18021 Bourges, France;
telephone: +33 (0) 2 48 67 56 00; fax: +33 (0) 2 48 50 01 41; E-
mail: customer_services@smasr.com; Internet: https://
www.smaengines.com.
(3) You may review copies of the service information
incorporated by reference for this AD at the FAA, Central Region,
Office of the Regional Counsel, 901 Locust, Kansas City, Missouri
64106. For information on the availability of this material at the
Central Region, call (816) 329-3768.
(4) You may also review copies of the service information
incorporated by reference for this AD 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 Kansas City, Missouri, on February 6, 2009.
Kim Smith,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. E9-2993 Filed 2-19-09; 8:45 am]
BILLING CODE 4910-13-P
