[Federal Register: January 10, 2007 (Volume 72, Number 6)]
[Rules and Regulations]
[Page 1141-1143]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr10ja07-5]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2006-26128; Directorate Identifier 2006-NE-34-AD;
Amendment 39-14875; AD 2007-01-04]
RIN 2120-AA64
Airworthiness Directives; Turbomeca Artouste III B and III B1
Turboshaft Engines
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; request for comments.
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SUMMARY: We are adopting a new airworthiness directive (AD) for the
products listed above. 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:
3 cases of cracking due to exfoliation corrosion on the unions
of fuel pipes P/N 0 202 12 800 0, connecting the Fuel Control Unit
to the start electrovalve, were reported. These cases of cracking,
if they had not previously been detected, could have caused a loss
of integrity of the union conveying fuel under pressure. A fuel
leakage could then have happened and would have led to an
uncommanded loss of power and to a fire hazard. This AD requires the
fuel pipe to be inspected for cracking.
This AD requires actions that are intended to address the unsafe
condition described in the MCAI.
DATES: This AD becomes effective January 25, 2007.
The Director of the Federal Register approved the incorporation by
reference of Turbomeca Mandatory Service Bulletin No. A218 73 0803,
dated May 2, 2006, listed in the AD as of January 25, 2007.
We must receive comments on this AD by February 9, 2007.
ADDRESSES: You may send comments by any of the following methods:
DOT Docket Web Site: Go to http://dms.dot.gov and follow
the instructions for sending your comments electronically.
Fax: (202) 493-2251.
Mail: Docket Management Facility, U.S. Department of
Transportation, 400 Seventh Street, SW., Nassif Building, Room PL-401,
Washington, DC 20590-0001.
Hand Delivery: Room PL-401 on the plaza level of the
Nassif Building,
[[Page 1142]]
400 Seventh Street, SW., Washington, DC, between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays.
Federal eRulemaking Portal: http://www.regulations.gov.
Follow the instructions for submitting comments.
Examining the AD Docket
You may examine the AD docket on the Internet at http://dms.dot.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 AD, the regulatory evaluation, any comments
received, and other information. The street address for the Docket
Office (telephone (800) 647-5227) is in the ADDRESSES section. Comments
will be available in the AD docket shortly after receipt.
FOR FURTHER INFORMATION CONTACT: Christopher Spinney, Aerospace
Engineer, Engine Certification Office, FAA, Engine & Propeller
Directorate, 12 New England Executive Park, Burlington, MA 01803;
telephone (781) 238-7175; fax (781) 238-7199.
SUPPLEMENTARY INFORMATION:
Streamlined Issuance of AD
The FAA is implementing a new process for streamlining the issuance
of ADs related to MCAI. This streamlined process will allow us to adopt
MCAI safety requirements in a more efficient manner and will reduce
safety risks to the public. This process continues to follow all FAA AD
issuance processes to meet legal, economic, Administrative Procedure
Act, and Federal Register requirements. We also continue to meet our
technical decision-making responsibilities to identify and correct
unsafe conditions on U.S.-certificated products.
This AD references the MCAI and related service information that we
considered in forming the engineering basis to correct the unsafe
condition. The AD contains text copied from the MCAI and for this
reason might not follow our plain language principles.
Discussion
The European Aviation Safety Agency (EASA), which is the aviation
authority for the European Union, has issued Airworthiness Directive
No. 2006-0154, dated June 1, 2006, (referred to after this as ``the
MCAI''), to correct an unsafe condition for the specified products. The
MCAI states:
3 cases of cracking due to exfoliation corrosion on the unions
of fuel pipes P/N 0 202 12 800 0, connecting the Fuel Control Unit
to the start electrovalve, were reported. These cases of cracking,
if they had not previously been detected, could have caused a loss
of integrity of the union conveying fuel under pressure. A fuel
leakage could then have happened and would have led to an
uncommanded loss of power and to a fire hazard. This AD requires the
fuel pipe to be inspected for cracking.
You may obtain further information by examining the MCAI in the AD
docket.
Relevant Service Information
Turbomeca has issued Mandatory Service Bulletin No. A218 73 0803,
dated May 2, 2006. The actions described in this service information
are intended to correct the unsafe condition identified in the MCAI.
FAA's Determination and Requirements of This 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 issuing this AD because we
evaluated all the information provided by the State of Design Authority
and determined the unsafe condition exists and is likely to exist or
develop on other products of the same type design.
Differences Between the 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 required different actions in this AD from those
in the MCAI in order to follow FAA policies. Any such differences are
described in a separate paragraph of the AD. These requirements take
precedence over the actions copied from the MCAI.
FAA's Determination of the Effective Date
An unsafe condition exists that requires the immediate adoption of
this AD. The FAA has found that the risk to the flying public justifies
waiving notice and comment prior to adoption of this rule because
undetected cracking could cause loss of integrity of the union
conveying fuel under pressure. This could result in a fuel leak and an
uncommmanded loss of power and a fire hazard. Therefore, we determined
that notice and opportunity for public comment before issuing this AD
are impracticable and that good cause exists for making this amendment
effective in fewer than 30 days.
Comments Invited
This AD is a final rule that involves requirements affecting flight
safety, and we did not precede it by notice and opportunity for public
comment. We invite you to send any written relevant data, views, or
arguments about this AD. Send your comments to an address listed under
the ADDRESSES section. Include ``Docket No. FAA-2006-26128; Directorate
Identifier 2006-NE-34-AD'' at the beginning of your comments. We
specifically invite comments on the overall regulatory, economic,
environmental, and energy aspects of this AD. We will consider all
comments received by the closing date and may amend this AD because of
those comments.
We will post all comments we receive, without change, to http://dms.dot.gov
, including any personal information you provide. We will
also post a report summarizing each substantive verbal contact we
receive about this AD.
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.
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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); 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 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.
Adoption of the Amendment
0
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:
2007-01-04 Turbomeca: Amendment 39-14875. Docket No. FAA-2006-26128;
Directorate Identifier 2006-NE-34-AD.
Effective Date
(a) This airworthiness directive (AD) becomes effective January
25, 2007.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Artouste III B and III B1 turboshaft
engines fitted with a fuel pipe, part number 0 202 12 800 0. These
engines are installed on SA 315 B LAMA and SA 316 B Alouette III
helicopters.
Reason
(d) European Aviation Safety Agency, (EASA), Airworthiness
Directive No. 2006-0154, dated June 1, 2006, states:
3 cases of cracking due to exfoliation corrosion on the unions
of fuel pipes P/N 0 202 12 800 0, connecting the Fuel Control Unit
to the start electrovalve, were reported. These cases of cracking,
if they had not previously been detected, could have caused a loss
of integrity of the union conveying fuel under pressure. A fuel
leakage could then have happened and would have led to an
uncommanded loss of power and to a fire hazard. This AD requires the
fuel pipe to be inspected for cracking.
FAA AD Differences
(e) None.
Actions and Compliance
(f) At the next maintenance action on the engine or airframe,
but no later than 30 days after the effective date of this AD,
unless already done, do the following action.
(1) Inspect for cracks in the lower union of the flexible fuel
pipe between the electric fuel cock and the start valve.
(2) Use the instructions contained in paragraph 2 of Turbomeca
Mandatory Service Bulletin No. A218 73 0803, dated May 2, 2006, to
do the inspection.
Other FAA AD Provisions
(g) The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
Engine Certification Office, has the authority to approve AMOCs for
this AD, if requested using the procedures found in 14 CFR 39.19.
(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, under the provisions of the Paperwork Reduction Act, the
Office of Management and Budget (OMB) has approved the information
collection requirements and has assigned OMB Control Number 2120-
0056.
Related Information
(h) Refer to the EASA Airworthiness Directive 2006-0154, dated
June 1, 2006, and Turbomeca Mandatory Service Bulletin A218 73 0803,
dated May 2, 2006, for related information.
(i) Contact Christopher Spinney, Aerospace Engineer, Engine
Certification Office, FAA, Engine & Propeller Directorate, 12 New
England Executive Park, Burlington, MA 01803; telephone (781) 238-
7175; fax (781) 238-7199, for more information about this AD.
Material Incorporated by Reference
(j) You must use Turbomeca Mandatory Service Bulletin No. A218
73 0803, dated May 2, 2006, to do the actions required by this AD,
unless the AD specifies otherwise.
(1) The Director of the Federal Register approved the
incorporation by reference of this service information under 5
U.S.C. 552(a) and 1 CFR part 51.
(2) For service information identified in this AD, contact
Turbomeca, 40220 Tarnos, France; telephone (33) 05 59 74 40 00; fax
(33) 05 59 74 45 15.
(3) You may review copies 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/
[fxsp0]federal-register/cfr/[fxsp0]ibr-
locations.html.
Issued in Burlington, Massachusetts, on December 27, 2006.
Ann C. Mollica,
Acting Manager, Engine and Propeller Directorate, Aircraft
Certification Service.
[FR Doc. E6-22533 Filed 1-9-07; 8:45 am]
BILLING CODE 4910-13-P