
[Federal Register Volume 79, Number 50 (Friday, March 14, 2014)]
[Proposed Rules]
[Pages 14447-14449]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2014-05612]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2014-0156; Directorate Identifier 2014-CE-001-AD]
RIN 2120-AA64


Airworthiness Directives; Costruzioni Aeronautiche Tecnam srl 
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 
Costruzioni Aeronautiche Tecnam srl Model P2006T airplanes. 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 a cracked engine mount. We are 
issuing this proposed AD to require actions to address the unsafe 
condition on these products.

DATES: We must receive comments on this proposed AD by April 28, 2014.

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; email: m.oliva@tecnam.com or g.paduano@tecnam.com; Internet: 
www.tecnam.com/it-IT/documenti/service-bulletins.aspx. 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 by searching for and locating Docket No. FAA-2014-
0156; 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; email: 
albert.mercado@faa.gov.

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-2014-0156; 
Directorate Identifier 2014-CE-001-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

[[Page 14448]]

proposed AD because of those comments.
    We will post all comments we receive, without change, to http://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 AD 
No.: 2014-0001, dated January 6, 2014 (referred to after this as ``the 
MCAI''), to correct an unsafe condition for Costruzioni Aeronautiche 
Tecnam srl Model P2006T airplanes. The MCAI states:

    During a ``100 hours'' inspection of a P2006T aeroplane, one 
engine mount Part Number (P/N) 26-7-1200-000 was found cracked on a 
node.
    This condition, if not detected and corrected, could lead to 
engine damage, possibly resulting in damage to the aeroplane and 
injury to the occupants.
    To address this potential unsafe condition, TECNAM issued 
Service Bulletin (SB) 138-CS-Rev0, providing inspection 
instructions.
    For the reasons described above, this AD requires a one-time 
inspection of each engine mount P/N 26-7-1200-000 and, depending on 
findings, replacement of the engine mount(s).
    This AD is considered an interim action and further AD action 
may follow.

    You may examine the MCAI on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2014-
0156.

Relevant Service Information

    Costruzioni Aeronautiche Tecnam srl has issued Service Bulletin No. 
SB 138-CS, Rev. 0, dated November 25, 2013. The actions described in 
this 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.

Interim Action

    We consider this AD interim action. We are proposing requiring 
inspection of the left hand and right hand engine mounts with a report 
to the manufacturer of the results if cracks or deformation are found. 
We will work with the type certificate holder to evaluate the report 
results to determine repetitive inspection intervals and subsequent 
terminating action. Based on this evaluation, we may initiate further 
rulemaking action to address the unsafe condition identified in this 
AD.

Costs of Compliance

    We estimate that this proposed AD will affect 10 products of U.S. 
registry. We also estimate that it would take about 6 work-hours per 
product to comply with the basic requirements of this proposed AD. The 
average labor rate is $85 per work-hour.
    Based on these figures, we estimate the cost of the proposed AD on 
U.S. operators to be $5,100, or $510 per product.
    In addition, we estimate that any necessary follow-on actions would 
take about 18 work-hours and require parts costing $1,570 (per engine 
mount), for a cost of $3,100 per product. We have no way of determining 
the number of products that may need these actions.

Paperwork Reduction Act

    A federal agency may not conduct or sponsor, and a person is not 
required to respond to, nor shall a person be subject to penalty for 
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 control 
number for the collection of information required by this AD is 2120-
0056. The paperwork cost associated with this AD has been detailed in 
the Costs of Compliance section of this document and includes time for 
reviewing instructions, as well as completing and reviewing the 
collection of information. Therefore, all reporting associated with 
this AD is 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.

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),
    (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.

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

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. Amend Sec.  39.13 by adding the following new AD:

Costruzioni Aeronautiche Tecnam srl: Docket No. FAA-2014-0156; 
Directorate Identifier 2014-CE-001-AD.

[[Page 14449]]

(a) Comments Due Date

    We must receive comments by April 28, 2014.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Costruzioni Aeronautiche Tecnam srl Model 
P2006T airplanes, all serial numbers, certificated in any category.

(d) Subject

    Air Transport Association of America (ATA) Code 71: Power Plant.

(e) Reason

    This AD was prompted by 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 a cracked engine 
mount. We are issuing this AD to detect and correct cracked or 
deformed engine mounts, which could lead to engine damage, possibly 
resulting in damage to the airplane and injury to the occupants.

(f) Actions and Compliance

    Unless already done, do the following actions as specified in 
paragraphs (f)(1) through (f)(3) of this AD:
    (1) For airplanes with 600 hours time-in-service (TIS) or more 
as of the effective date of this AD: Within the next 25 hours TIS 
after the effective date of this AD or within the next 30 days after 
the effective date of this AD, whichever occurs first, inspect the 
left hand and right hand engine mounts, part number (P/N) 26-7-1200-
000, for cracks and deformation following Costruzioni Aeronautiche 
TECNAM Service Bulletin No. SB 138-CS, Rev. 0, dated November 25, 
2013.
    (2) For airplanes with less than 600 hours TIS as of the 
effective date of this AD: After accumulating 600 hours TIS but 
before exceeding 625 hours TIS, inspect the left hand and right hand 
engine mounts, P/N 26-7-1200-000, for cracks and deformation 
following Costruzioni Aeronautiche TECNAM Service Bulletin No. SB 
138-CS, Rev. 0, dated November 25, 2013.
    (3) If a crack or any other deformation is found during the 
inspection required by paragraph (f)(1) or (f)(2) of this AD, before 
further flight, you must contact Costruzioni Aeronautiche Tecnam srl 
to obtain FAA-approved repair instructions approved specifically for 
compliance with this AD and incorporate those instructions. You can 
find contact information for Costruzioni Aeronautiche Tecnam srl in 
paragraph (h) of this AD. Use the occurrence report in Costruzioni 
Aeronautiche TECNAM Service Bulletin No. SB 138-CS, Rev. 0, dated 
November 25, 2013.

(g) Other FAA AD Provisions

    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; email: 
albert.mercado@faa.gov. Before using any approved AMOC on any 
airplane to which the AMOC applies, notify your appropriate 
principal inspector (PI) in the FAA Flight Standards District Office 
(FSDO), or lacking a PI, your local FSDO.
    (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 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.

(h) Related Information

    MCAI European Aviation Safety Agency (EASA) AD No.: 2014-0001, 
dated January 6, 2014, for related information. You may examine the 
MCAI on the Internet at http://www.regulations.gov by searching for 
and locating Docket No. FAA-2014-0156. 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; email: 
m.oliva@tecnam.com or g.paduano@tecnam.com; Internet: 
www.tecnam.com/it-IT/documenti/service-bulletins.aspx. You may 
review this 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 7, 2014.
Steven W. Thompson,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2014-05612 Filed 3-13-14; 8:45 am]
BILLING CODE 4910-13-P


