preamble attached >>>
ADs updated daily at www.Tdata.com
2015-02-09 COSTRUZIONI AERONAUTICHE TECNAM SRL: Amendment 39-18076; Docket No. FAA-2014-0876; Directorate Identifier 2014-CE-032-AD.
(a) EFFECTIVE DATE

    This airworthiness directive (AD) becomes effective March 5, 2015.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This  AD  applies  to  Costruzioni Aeronautiche Tecnam srl P2006T air-
    planes, all serial numbers, certificated in any category.

(d) SUBJECT

    Air Transport Association of America (ATA) Code 78: Engine Exhaust.

(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  cracking found in  the engine
    exhaust pipe.  We are  issuing this  AD to  detect and correct cracked
    engine  exhaust pipes,  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 para-
    graphs (f)(1) through (f)(3) of this AD:

(1) Within 25 hours time-in-service (TIS) after  March 5, 2015 (the effec-
    tive date of this AD) or within  the next 30 days after March 5,  2015
    (the effective date of this AD), whichever occurs first, do a detailed
    inspection  of  all  engine  exhaust  pipes  following  the inspection
    instructions in Costruzioni  Aeronautiche TECNAM Service  Bulletin No.
    SB 170-CS-Ed 1, Rev 1, dated September 25, 2014.

(2) If any deformation, cracks,  or  any other defects are detected during
    the inspection  as required  by paragraph  (f)(1) of  this AD,  before
    further flight, replace  the affected pipe  with an airworthy  part or
    contact  Costruzioni  Aeronautiche  TECNAM  for  FAA-approved   repair
    instructions approved  specifically for  compliance with  this AD  and
    incorporate  those  instructions.  Use  the  information  in paragraph
    (i)(3) of this AD to contact Costruzioni Aeronautiche TECNAM.

(3) Within 30 days after the  inspection  required  by paragraph (f)(1) of
    this AD or within 30 days  after March 5, 2015 (the effective  date of
    this AD),  whichever occurs  later, report  the results  (including no
    findings) by using the  occurrence report in Costruzioni  Aeronautiche
    TECNAM Service Bulletin No. SB 170-CS-Ed 1, Rev 1, dated September 25,
    2014.

(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 re-
    quested 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;  tele-
    phone: (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

    Refer  to  European Aviation Safety Agency (EASA)  AD  No.: 2014-0220,
    dated  September 30, 2014,  for  related information.  The MCAI can be
    found in the AD docket on the Internet at: http://www.regulations.gov/
    #!documentDetail;D=FAA-2014-0876-0002.

(i) 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 the AD specifies otherwise.

(i) Costruzioni Aeronautiche TECNAM  Service Bulletin  No. SB 170-CS-Ed 1,
    Rev 1, dated September 25, 2014.

(ii) Reserved.

(3) For  Costruzioni Aeronautiche TECNAM service information identified in
    this AD, contact Costruzioni Aeronautiche Tecnam Airworthiness Office,
    Via Maiorise-81043 Capua (CE) Italy;  telephone: +39 0823 997538; fax:
    +39 0823 622899; email: technical.support@tecnam.com;  Internet: http:
    //www.tecnam.com/Customer-Care/Service-Bulletins.aspx.

(4) You may review this referenced  service information at the FAA,  Small
    Airplane Directorate, 901 Locust, Kansas City, Missouri 64106. For in-
    formation on the availability of this material at the FAA,  call (816)
    329-4148. In addition,  you can access this service information on the
    Internet  at  http://www.regulations.gov by searching for and locating
    Docket No. FAA-2014-0876.

(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 Kansas City, Missouri,  on January 14, 2015. Kelly  A. Broadway,
Acting  Manager,  Small   Airplane  Directorate,  Aircraft   Certification
Service.

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.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2014-0876; Directorate Identifier 2014-CE-032-AD;
Amendment 39-18076; AD 2015-02-09]
RIN 2120-AA64

Airworthiness Directives; Costruzioni Aeronautiche Tecnam srl
Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).

ACTION: Final rule.

-----------------------------------------------------------------------

SUMMARY: We are adopting a new airworthiness directive (AD) for
Costruzioni Aeronautiche Tecnam srl Model P2006T airplanes. This AD
results from mandatory continuing airworthiness information (MCAI)
issued 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 cracking found in the engine exhaust pipe. We
are issuing this AD to require actions to address the unsafe condition
on these products.

DATES: This AD is effective March 5, 2015.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in the AD as of March 5,
2015.

ADDRESSES: You may examine the AD docket on the Internet at http://www.
regulations.gov by searching for and locating Docket No. FAA-2014-
0876; or in person at Document Management Facility, U.S. Department of
Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590.
For service information identified in this AD, contact Costruzioni
Aeronautiche Tecnam Airworthiness Office, Via Maiorise-81043 Capua (CE)
Italy; telephone: +39 0823 997538; fax: +39 0823 622899; email:
technical.support@tecnam.com; Internet: http://www.tecnam.com/Customer-
Care/Service-Bulletins.aspx. You may view 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.

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:

Discussion

We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to add an AD that would apply to Costruzioni Aeronautiche
Tecnam srl Model P2006T airplanes. The NPRM was published in the
Federal Register on October 29, 2014 (79 FR 64347). The NPRM proposed
to correct an unsafe condition for the specified products and was based
on mandatory continuing airworthiness information (MCAI) originated by
an aviation authority of another country. The MCAI states:

During a pre-flight inspection of a P2006T aeroplane, which
included the opening of engine nacelle, a crack was found on the
engine exhaust pipe Part Number (P/N) 26-7-1800-1.
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, Costruzioni
Aeronautiche TECNAM issued Service Bulletin (SB) SB 170-CS-Ed 1
Rev1.
For the reason described above, this AD requires a one-time
inspection of the affected engine exhaust pipes and, depending on
findings, replacement.

The MCAI can be found in the AD docket on the Internet at: http://www.regulations.gov/#!documentDetail;D=FAA-2014-0876-0002.

Comments

We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM or on the determination of
the cost to the public.

Conclusion

We reviewed the relevant data and determined that air safety and
the public interest require adopting the AD as proposed except for
minor editorial changes. We have determined that these minor changes:
Are consistent with the intent that was proposed in the
NPRM (79 FR 64347, October 29, 2014) for correcting the unsafe
condition; and
Do not add any additional burden upon the public than was
already proposed in the NPRM.

Relative Service Information

We reviewed Costruzioni Aeronautiche TECNAM Service Bulletin No. SB
170-CS-Ed 1, Rev 1, dated September 25, 2014. The service bulletin
describes procedures for inspecting and replacing (as necessary) the
engine exhaust pipes. You can find this service information on the
Internet at http://www.regulations.gov by searching for and locating
Docket No. FAA-2014-0876.

Costs of Compliance

We estimate that this AD will affect 10 products of U.S. registry.
We also estimate that it would take about .5 work-hour per product to
comply with the basic requirements of this AD. The average labor rate
is $85 per work-hour.
Based on these figures, we estimate the cost of this AD on U.S.
operators to be $425, or $42.50 per product.
In addition, we estimate that any necessary follow-on actions would
take about .5 work-hour and require parts costing $343, for a cost of
$385.50 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 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 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.

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-
0876; 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 the NPRM, 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.

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

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: