AD 2015-02-09
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Costruzioni Aeronautiche Tecnam srl | P2006T | Airworthiness Directives; Costruzioni Aeronautiche Tecnam srl Airplanes |
Unsafe Condition
Cracking found in the engine exhaust pipe Part Number (P/N) 26-7-1800-1.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect all engine exhaust pipes following Costruzioni Aeronautiche TECNAM Service Bulletin No. SB 170-CS-Ed 1, Rev 1. If any deformation, cracks, or defects are detected, replace the affected pipe with an airworthy part or use FAA-approved repair instructions.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 25 hours time-in-service (TIS) after March 5, 2015, or within the next 30 days after March 5, 2015, whichever occurs first.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Costruzioni Aeronautiche Tecnam srl Model P2006T airplanes, all serial numbers, certificated in any category.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
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.
Applicability Source Text
Show captured applicability text from the source AD
(c) Applicability
This AD applies to Costruzioni Aeronautiche Tecnam srl P2006T
airplanes, all serial numbers, certificated in any category.
Document Text
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[Federal Register Volume 80, Number 19 (Thursday, January 29, 2015)]
[Rules and Regulations]
[Pages 4767-4769]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2015-00992]
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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.
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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 <a href="http://www.regulations.gov">http://www.regulations.gov</a> 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:
<a href="/cdn-cgi/l/email-protection#a8dccdcbc0c6c1cbc9c486dbddd8d8c7dadce8dccdcbc6c9c586cbc7c5"><span class="__cf_email__" data-cfemail="225647414a4c4b41434e0c515752524d5056625647414c434f0c414d4f">[email protected]</span></a>; Internet: <a href="http://www.tecnam.com/Customer-Care/Service-Bulletins.aspx">http://www.tecnam.com/Customer-Care/Service-Bulletins.aspx</a>. 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:
<a href="/cdn-cgi/l/email-protection#51303d333423257f3c34233230353e113730307f363e27"><span class="__cf_email__" data-cfemail="afcec3cdcadddb81c2caddcccecbc0efc9cece81c8c0d9">[email protected]</span></a>.
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: <a href="http://www.regulations.gov/#!documentDetail">http://www.regulations.gov/#!documentDetail</a>;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:
<bullet> Are consistent with the intent that was proposed in the
NPRM (79 FR 64347, October 29, 2014) for correcting the unsafe
condition; and
<bullet> 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 <a href="http://www.regulations.gov">http://www.regulations.gov</a> 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
[[Page 4768]]
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 <a href="http://www.regulations.gov">http://www.regulations.gov</a> 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
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:
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
airplanes, 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
paragraphs (f)(1) through (f)(3) of this AD:
(1) Within 25 hours time-in-service (TIS) after March 5, 2015
(the effective 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 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:
<a href="/cdn-cgi/l/email-protection#d0b1bcb2b5a2a4febdb5a2b3b1b4bf90b6b1b1feb7bfa6"><span class="__cf_email__" data-cfemail="5a3b36383f282e74373f28393b3e351a3c3b3b743d352c">[email protected]</span></a>. 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: <a href="http://www.regulations.gov/#!documentDetail">http://www.regulations.gov/#!documentDetail</a>;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
[[Page 4769]]
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:
<a href="/cdn-cgi/l/email-protection#720617111a1c1b11131e5c010702021d0006320617111c131f5c111d1f"><span class="__cf_email__" data-cfemail="afdbcaccc7c1c6cccec381dcdadfdfc0dddbefdbcaccc1cec281ccc0c2">[email protected]</span></a>; Internet: <a href="http://www.tecnam.com/Customer-Care/Service-Bulletins.aspx">http://www.tecnam.com/Customer-Care/Service-Bulletins.aspx</a>.
(4) 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. In addition, you can access this service
information on the Internet at <a href="http://www.regulations.gov">http://www.regulations.gov</a> 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: <a href="http://www.archives.gov/federal-register/cfr/ibr-locations.html">http://www.archives.gov/federal-register/cfr/ibr-locations.html</a>.
Issued in Kansas City, Missouri, on January 14, 2015.
Kelly A. Broadway,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2015-00992 Filed 1-28-15; 8:45 am]
BILLING CODE 4910-13-P
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Retrieved: Apr 6, 2026
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