[Federal Register Volume 76, Number 66 (Wednesday, April 6, 2011)]
[Proposed Rules]
[Pages 18964-18966]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2011-8070]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2011-0326; Directorate Identifier 2011-CE-006-AD]
RIN 2120-AA64
Airworthiness Directives; Costruzioni Aeronautiche Tecnam srl
Model P2006T Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Notice of proposed rulemaking (NPRM).
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SUMMARY: We propose to adopt a new airworthiness directive (AD) for the
products listed above. This proposed AD results from mandatory
continuing airworthiness information (MCAI) originated by an aviation
authority of another country to identify and correct an unsafe
condition on an aviation product. The MCAI describes the unsafe
condition as:
During Landing Gear retraction/extension ground checks performed
on the P2006T, a loose Seeger ring was found on the nose landing
gear hydraulic actuator cap.
The manufacturer has identified the root cause of this
discrepancy in a design deficiency of the hydraulic actuator caps.
This condition, if not corrected, could determine uncommanded
and improper extension of the nose or main landing gear.
The proposed AD would require actions that are intended to address the
unsafe condition described in the MCAI.
DATES: We must receive comments on this proposed AD by May 23, 2011.
ADDRESSES: You may send comments by any of the following methods:
Federal eRulemaking Portal: Go to http://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
Costruzioni Aeronautiche TECNAM Airworthiness Office, Via Maiorise--
81043 Capua (CE) Italy; telephone: +39 0823 620134; fax: +39 0823
622899; e-mail: [email protected], [email protected]; Internet:
http://www.tecnam.com. You may review copies of the referenced service
information at the FAA, Small Airplane Directorate, 901 Locust, Kansas
City, Missouri 64106. For information on the availability of this
material at the FAA, call 816-329-4148.
Examining the AD Docket
You may examine the AD docket on the Internet at http://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 proposed 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: Albert Mercado, Aerospace Engineer,
FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City,
Missouri 64106; telephone: (816) 329-4119; fax: (816) 329-4090.
SUPPLEMENTARY INFORMATION:
Comments Invited
We invite you to send any written relevant data, views, or
arguments about this proposed AD. Send your comments to an address
listed under the ADDRESSES section. Include ``Docket No. FAA-2011-0326;
Directorate Identifier 2011-CE-006-AD'' at the beginning of your
comments. We specifically invite comments on the overall regulatory,
economic, environmental, and energy aspects of this proposed AD. We
will consider all comments received by the closing date and may amend
this proposed AD because of those comments.
We will post all comments we receive, without change, to http://www.regulations.gov, including any personal information you provide. We
will also post a report summarizing each substantive verbal contact we
receive about this proposed AD.
Discussion
The European Aviation Safety Agency (EASA), which is the Technical
Agent for the Member States of the European Community, has issued EASA
AD No.: 2011-0042, dated March 11, 2011 (referred to after this as
``the MCAI''), to correct an unsafe condition for the specified
products. The MCAI states:
During Landing Gear retraction/extension ground checks performed
on the P2006T, a loose Seeger ring was found on the nose landing
gear hydraulic actuator cap.
The manufacturer has identified the root cause of this
discrepancy in a design deficiency of the hydraulic actuator caps.
This condition, if not corrected, could determine uncommanded
and improper extension of the nose or main landing gear. To prevent
this condition, this AD requires modifying each nose and main
landing gear hydraulic actuator by installing security rings.
You may obtain further information by examining the MCAI in the AD
docket.
Relevant Service Information
Costruzioni Aeronautiche Tecnam has issued Service Bulletin No. SB
036-CS, 1st Edition, Rev 1, dated December 15, 2010. The actions
described in this
[[Page 18965]]
service information are intended to correct the unsafe condition
identified in the MCAI.
FAA's Determination and Requirements of the Proposed 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 proposing this AD because
we evaluated all information and determined the unsafe condition exists
and is likely to exist or develop on other products of the same type
design.
Differences Between This Proposed AD and the MCAI or Service
Information
We have reviewed the MCAI and related service information and, in
general, agree with their substance. But we might have found it
necessary to use different words from those in the MCAI to ensure the
AD is clear for U.S. operators and is enforceable. In making these
changes, we do not intend to differ substantively from the information
provided in the MCAI and related service information.
We might also have proposed different actions in this AD from those
in the MCAI in order to follow FAA policies. Any such differences are
highlighted in a Note within the proposed AD.
Costs of Compliance
We estimate that this proposed AD will affect 1 product of U.S.
registry. We also estimate that it would take about 2 work-hours per
product to comply with the basic requirements of this proposed AD. The
average labor rate is $85 per work-hour. Required parts would cost
about $80 per product.
Based on these figures, we estimate the cost of the proposed AD on
U.S. operators to be $250, or $250 per product.
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 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 this 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.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, 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:
Costruzioni Aeronautiche Tecnam srl: Docket No. FAA-2011-0326;
Directorate Identifier 2011-CE-006-AD.
Comments Due Date
(a) We must receive comments by May 23, 2011.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Costruzioni Aeronautiche Tecnam srl
P2006T airplanes, serial numbers 01 through 046, 047/US, and 049,
certificated in any category.
Subject
(d) Air Transport Association of America (ATA) Code 32: Landing
Gear.
Reason
(e) The mandatory continuing airworthiness information (MCAI)
states:
During Landing Gear retraction/extension ground checks performed
on the P2006T, a loose Seeger ring was found on the nose landing
gear hydraulic actuator cap.
The manufacturer has identified the root cause of this
discrepancy in a design deficiency of the hydraulic actuator caps.
This condition, if not corrected, could determine uncommanded
and improper extension of the nose or main landing gear. To prevent
this condition, this AD requires modifying each nose and main
landing gear hydraulic actuator by installing security rings.
Actions and Compliance
(f) Unless already done, within 50 hours time-in-service after
the effective date of this AD or within 60 days after the effective
date of this AD, whichever occurs first, modify each nose and main
landing gear hydraulic actuator in accordance with Costruzioni
Aeronautiche Tecnam Service Bulletin No. SB 036-CS, 1st Edition, Rev
1, dated December 15, 2010.
FAA AD Differences
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,
Standards 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: Albert Mercado, Aerospace Engineer, FAA, Small
Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri
64106; telephone: (816) 329-4119; fax: (816) 329-4090. 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, a federal agency may not conduct or sponsor, and a person
is not required to respond to, nor shall a person be subject to a
penalty for
[[Page 18966]]
failure to comply with a collection of information subject to the
requirements of the Paperwork Reduction Act unless that collection
of information displays a current valid OMB Control Number. The OMB
Control Number for this information collection is 2120-0056. Public
reporting for this collection of information is estimated to be
approximately 5 minutes per response, including the time for
reviewing instructions, completing and reviewing the collection of
information. All responses to this collection of information are
mandatory. Comments concerning the accuracy of this burden and
suggestions for reducing the burden should be directed to the FAA
at: 800 Independence Ave. SW., Washington, DC 20591, Attn:
Information Collection Clearance Officer, AES-200.
Related Information
(h) Refer to MCAI European Aviation Safety Agency (EASA) AD No.:
2011-0042, dated March 11, 2011; and Costruzioni Aeronautiche Tecnam
Service Bulletin No. SB 036-CS, 1st Edition, Rev 1, dated December
15, 2010, for related information. For service information related
to this AD, contact Costruzioni Aeronautiche TECNAM Airworthiness
Office, Via Maiorise--81043 Capua (CE) Italy; telephone: +39 0823
620134; fax: +39 0823 622899; e-mail: [email protected],
[email protected]; Internet: http://www.tecnam.com. You may
review copies of the referenced service information at the FAA,
Small Airplane Directorate, 901 Locust, Kansas City, Missouri 64106.
For information on the availability of this material at the FAA,
call 816-329-4148.
Issued in Kansas City, Missouri, on March 29, 2011.
Earl Lawrence,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2011-8070 Filed 4-5-11; 8:45 am]
BILLING CODE 4910-13-P