[Federal Register Volume 78, Number 241 (Monday, December 16, 2013)]
[Rules and Regulations]
[Pages 76050-76052]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2013-29050]
[[Page 76050]]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2013-0688; Directorate Identifier 2012-NM-221-AD;
Amendment 39-17683; AD 2013-24-09]
RIN 2120-AA64
Airworthiness Directives; EADS CASA (Type Certificate Previously
Held by Construcciones Aeron[aacute]uticas, S.A.) Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
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SUMMARY: We are adopting a new airworthiness directive (AD) for certain
EADS CASA (Type Certificate Previously Held by Construcciones
Aeron[aacute]uticas, S.A.) Model C-212-CB, C-212-CC, C-212-CD, C-212-
CE, and C-212-DF airplanes. This AD was prompted by a report of the
propeller pitch control (PPC) lever becoming disconnected from the
engine due to a missing bolt. This AD requires modifying the PPC lever
attachment system. We are issuing this AD to prevent PPC shaft
disconnection, which could lead to a loss of propeller pitch control,
possibly resulting in uncommanded change to the engine power settings
and consequent reduced controllability of the airplane.
DATES: This AD becomes effective January 21, 2014.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of January 21,
2014.
ADDRESSES: You may examine the AD on the Internet at http://www.regulations.gov/#!docketDetail;D=FAA-2013-0688; or in person at the
U.S. Department of Transportation, Docket Operations, M-30, West
Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE.,
Washington, DC.
For EADS-CASA service information identified in this AD, contact
EADS-CASA, Military Transport Aircraft Division (MTAD), Integrated
Customer Services (ICS), Technical Services, Avenida de Arag[oacute]n
404, 28022 Madrid, Spain; telephone +34 91 585 55 84; fax +34 91 585 55
05; email [email protected]; Internet http://www.eads.net. For Honeywell service information identified in this AD,
contact Honeywell International Inc., 111 S. 34th Street, Phoenix, AZ
85034-2802; Internet: http://portal.honeywell.com; telephone: 800-601-
3099. You may view this referenced service information at the FAA,
Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For
information on the availability of this material at the FAA, call 425-
227-1221.
FOR FURTHER INFORMATION CONTACT: Shahram Daneshmandi, Aerospace
Engineer, International Branch, ANM-116, Transport Airplane
Directorate, FAA, 1601 Lind Avenue SW., Renton, Washington 98057-3356;
telephone (425) 227-1112; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would apply to the specified products.
The NPRM published in the Federal Register on August 13, 2013 (78 FR
49235). The NPRM proposed to correct an unsafe condition for the
specified products.
The European Aviation Safety Agency (EASA), which is the Technical
Agent for the Member States of the European Community, has issued EASA
Airworthiness Directive 2012-0251, dated November 27, 2012 (referred to
after this as the Mandatory Continuing Airworthiness Information, or
``the MCAI''), to correct an unsafe condition for the specified
products. The MCAI states:
An occurrence was reported where the propeller pitch control
(PPC) lever disconnected from the engine (a TPE331-10R-511C) on a C-
212-CC aeroplane.
The result of the subsequent investigation revealed that the PPC
lever disconnection occurred due to a missing bolt, which fixes the
clamp that joins the PPC lever to the PPC rod.
This condition, if not corrected, could lead to a loss of an
affected propeller pitch control, possibly resulting in uncommanded
change to the engine power settings and consequent reduced control
of the aeroplane.
To address this potential unsafe condition, EADS-CASA developed
a modification (mod 10515) that eliminates the possibility of PPC
shaft disconnection and made this available through Service Bulletin
SB-212-76-0009 to be applied in service.
For the reasons described above, this [EASA] AD requires
modification of PPC lever attachment system.
You may examine the MCAI in the AD docket on the Internet at http://www.regulations.gov/#!documentDetail;D=FAA-2013-0688-0002.
Comments
We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM (78 FR 49235, August 13,
2013) or on the determination of the cost to the public.
Explanation of Change Made to the AD
We have changed paragraph (c) of this AD to remove EADS CASA (Type
Certificate previously held by Construcciones Aeron[aacute]uticas,
S.A.) Model C-212-CF airplanes, which were included in the NPRM (78 FR
49235, August 13, 2013) in error.
Conclusion
We reviewed the available data and determined that air safety and
the public interest require adopting this AD as proposed. We have
determined that these minor changes:
Are consistent with the intent that was proposed in the
NPRM (78 FR 49235, August 13, 2013) for correcting the unsafe
condition; and
Do not add any additional burden upon the public than was
already proposed in the NPRM (78 FR 49235, August 13, 2013).
Costs of Compliance
We estimate that this AD affects 42 airplanes of U.S. registry.
We estimate the following costs to comply with this AD:
Estimated Costs
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
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Modification...................... 20 work-hours x $85 per $1,018 $2,718 $114,156
hour = $1,700.
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[[Page 76051]]
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 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);
3. Will not affect intrastate aviation in Alaska; and
4. Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
We prepared a regulatory evaluation of the estimated costs to
comply with this AD and placed it in the AD docket.
Examining the AD Docket
You may examine the MCAI in the AD docket on the Internet at http://www.regulations.gov/#!documentDetail;D=FAA-2013-0688-0002; or in
person at the Docket Operations office 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 Operations office
(telephone (800) 647-5527) is in the ADDRESSES section.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
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:
2013-24-09 EADS CASA (Type Certificate Previously Held by
Construcciones Aeron[aacute]uticas, S.A.): Amendment 39-17683.
Docket No. FAA-2013-0688; Directorate Identifier 2012-NM-221-AD.
(a) Effective Date
This airworthiness directive (AD) becomes effective January 21,
2014.
(b) Affected ADs
None.
(c) Applicability
This AD applies to EADS CASA (Type Certificate previously held
by Construcciones Aeron[aacute]uticas, S.A.) Model C-212-CB, C-212-
CC, C-212-CD, C-212-CE, and C-212-DF airplanes; certificated in any
category; all serial numbers, except those that have been modified
in production to incorporate EADS CASA Modification 10515.
(d) Subject
Air Transport Association (ATA) of America Code 76, Engine
Controls.
(e) Reason
This AD was prompted by a report of the propeller pitch control
(PPC) lever becoming disconnected from the engine due to a missing
bolt. We are issuing this AD to prevent PPC shaft disconnection,
which could lead to a loss of propeller pitch control, possibly
resulting in uncommanded change to the engine power settings and
consequent reduced controllability of the airplane.
(f) Compliance
You are responsible for having the actions required by this AD
performed within the compliance times specified, unless the actions
have already been done.
(g) Modification
Within 24 months after the effective date of this AD, modify the
PCC lever attachment system of the aircraft engine, in accordance
with the Accomplishment Instructions of EADS-CASA Service Bulletin
SB-212-76-0009, Revision 1, dated August 03, 2012.
Note 1 to paragraph (g) of this AD: EADS-CASA Service Bulletin
SB-212-76-0009, Revision 1, dated August 03, 2012, refers to
Honeywell Service Bulletin TPE331-72-2190, dated December 21, 2011,
as an additional source of guidance for modifying the cam assembly.
(h) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager, ANM-
116, International Branch, Transport Airplane Directorate, FAA, has
the authority to approve AMOCs for this AD, if requested using the
procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19,
send your request to your principal inspector or local Flight
Standards District Office, as appropriate. If sending information
directly to the International Branch, send it to ATTN: Shahram
Daneshmandi, Aerospace Engineer, International Branch, ANM-116,
Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton,
Washington 98057-3356; telephone (425) 227-1112; fax (425) 227-1149.
Information may be emailed to: [email protected].
Before using any approved AMOC, notify your appropriate principal
inspector, or lacking a principal inspector, the manager of the
local flight standards district office/certificate holding district
office. The AMOC approval letter must specifically reference this
AD.
(2) Airworthy Product: For any requirement in this AD to obtain
corrective actions from a manufacturer or other source, use these
actions if they are FAA-approved. Corrective actions are considered
FAA-approved if they are approved by the State of Design Authority
(or their delegated agent). You are required to assure the product
is airworthy before it is returned to service.
(i) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) EASA Airworthiness Directive 2012-0251, dated November 27,
2012, for related information. You may examine the MCAI in the AD
docket on the Internet at http://www.regulations.gov/#!documentDetail;D=FAA-2013-0688-0002.
(2) Honeywell service information referenced in this AD can be
obtained from Honeywell International Inc., 111 S. 34th Street,
Phoenix, AZ 85034-2802; Web site: http://portal.honeywell.com; or
call Honeywell toll free at phone: 800-601-3099 (U.S./Canada) or
602-365-3099 (International Direct).
(j) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless this AD specifies otherwise.
(i) EADS-CASA Service Bulletin SB-212-76-0009, Revision 1, dated
August 03, 2012.
(ii) Reserved.
(3) For EADS-CASA service information identified in this AD,
contact EADS-CASA,
[[Page 76052]]
Military Transport Aircraft Division (MTAD), Integrated Customer
Services (ICS), Technical Services, Avenida de Arag[oacute]n 404,
28022 Madrid, Spain; telephone +34 91 585 55 84; fax +34 91 585 55
05; email [email protected]; Internet http://www.eads.net.
(4) You may view this service information at the FAA, Transport
Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For
information on the availability of this material at the FAA, call
425-227-1221.
(5) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued in Renton, Washington, on November 15, 2013.
John Piccola,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2013-29050 Filed 12-13-13; 8:45 am]
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