[Federal Register Volume 75, Number 105 (Wednesday, June 2, 2010)]
[Rules and Regulations]
[Pages 30687-30689]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2010-13133]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2007-27009; Directorate Identifier 2007-NE-02-AD; 
Amendment 39-16322; AD 2007-19-09R1]
RIN 2120-AA64


Airworthiness Directives; Turbomeca Arriel 2B1 Turboshaft Engines

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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SUMMARY: We are revising an existing 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:

    Since the issuance of AD 2007-0126 Turbomeca has released 
modification TU157 which consists in modifying the pressure relief 
valve of the HMU by introducing a damping device into the valve. 
Introduction of this device has demonstrated to decrease the 
pressure fluctuations in the system, therefore reducing 
significantly the risk of wear of the delta-P diaphragm fabric. This 
will delete the need for a periodical replacement of the delta-P 
diaphragm before overhaul of the HMU. The modification TU157 is 
therefore considered as the terminating action for this AD.

We are issuing this AD to prevent the loss of automatic control mode 
coupled with the deteriorated performance of the backup mode, which can 
lead to the inability to continue safe flight, forced autorotation 
landing, or an accident.

DATES: This AD becomes effective July 7, 2010.

ADDRESSES: The Docket Operations office is located at Docket Management 
Facility, U.S. Department of Transportation, 1200 New Jersey Avenue, 
SE., West Building Ground Floor, Room W12-140, Washington, DC 20590-
0001.

FOR FURTHER INFORMATION CONTACT: Kevin Dickert, Aerospace Engineer, 
Engine Certification Office, FAA, Engine & Propeller Directorate, 12 
New England Executive Park, Burlington, MA 01803; e-mail: 
[email protected]; telephone (781) 238-7117; fax (781) 238-7199.

SUPPLEMENTARY INFORMATION: 

Discussion

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR 
part 39 to include an AD that would apply to the specified products. 
That NPRM was published in the Federal Register on March 22, 2010 (75 
FR 13451). That NPRM proposed to correct an unsafe condition for the 
specified products. The MCAI states that:

    Since the issuance of AD 2007-0126 Turbomeca has released 
modification TU157 which consists in modifying the pressure relief 
valve of the HMU by introducing a damping device into the valve. 
Introduction of this device has demonstrated to decrease the 
pressure fluctuations in the system, therefore reducing 
significantly the risk of wear of the delta-P diaphragm fabric. This 
will delete the need for a periodical replacement of the delta-P 
diaphragm before overhaul of the HMU. The modification TU157 is 
therefore considered as the terminating action for this AD.

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.

Mandatory Service Bulletin Reference Added

    Since we issued the proposed AD, Turbomeca issued Mandatory Service 
Bulletin (MSB) No. 292 73 2818, Version C, dated January 29, 2009. We 
added that reference to paragraph (e)(2)(iii) of the AD.

Conclusion

    We reviewed the available data and determined that air safety and 
the public interest require adopting the AD with the change described 
previously.

[[Page 30688]]

Differences Between This AD and the MCAI or Service Information

    The MCAI applies to the ARRIEL 2B1 and 2B1A engines. The ARRIEL 
2B1A engine is not type certificated in the United States, so this AD 
applies to the ARRIEL 2B1 engine model only.

Costs of Compliance

    Based on the service information, we estimate that this AD will 
affect about 103 products of U.S. registry. We also estimate that it 
will take about 0.75 work-hour per product to comply with this AD. The 
average labor rate is $85 per work-hour. Required parts will cost about 
$10,550 per product. Based on these figures, we estimate the cost of 
the AD on U.S. operators to be $1,093,216.

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); 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.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://www.regulations.gov; or in person at the Docket Operations office 
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 Operations office (phone (800) 647-5527) is provided 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, 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 removing amendment 39-15200 (72 FR 
53112, September 18, 2007), and adding the following new AD:

2007-19-09R1 Turbomeca: Amendment 39-16322. Docket No. FAA-2007-
27009; Directorate Identifier 2007-NE-02-AD.

Effective Date

    (a) This airworthiness directive (AD) becomes effective July 7, 
2010.

Affected ADs

    (b) This AD revises AD 2007-19-09, Amendment 39-15200.

Applicability

    (c) This AD applies to Turbomeca ARRIEL 2B1 turboshaft engines 
that don't incorporate modification TU157. These engines are 
installed on, but not limited to, Eurocopter AS 350 B3 and EC 130 B4 
helicopters.

Reason

    (d) European Aviation Safety Agency (EASA) AD No. 2009-0091, 
dated May 4, 2009, states:
    Since the issuance of AD 2007-0126 Turbomeca has released 
modification TU157 which consists in modifying the pressure relief 
valve of the HMU by introducing a damping device into the valve. 
Introduction of this device has demonstrated to decrease the 
pressure fluctuations in the system, therefore reducing 
significantly the risk of wear of the delta-P diaphragm fabric. This 
will delete the need for a periodical replacement of the delta-P 
diaphragm before overhaul of the HMU. The modification TU157 is 
therefore considered as the terminating action for this AD.

We are issuing this AD to prevent the loss of automatic control mode 
coupled with the deteriorated performance of the backup mode, which 
can lead to the inability to continue safe flight, forced 
autorotation landing, or an accident.

Actions and Compliance

    (e) Unless already done, do the following actions.
    (1) For ARRIEL 2B1 engines that incorporate modification TU157, 
no further action is required.
    (2) For all other ARRIEL 2B1 engines do the following:
    (i) Replace the hydromechanical metering unit (HMU) with a 
serviceable HMU before the HMU accumulates 1,500 hours-since-new, 
hours-since-last-overhaul (HSO), or since incorporation of Turbomeca 
Service Bulletin (SB) No. 292 73 2105, whichever occurs later.
    (ii) Thereafter, replace the HMU with a serviceable HMU at every 
1,500 hours-since new, since last overhaul, or since incorporation 
of Turbomeca SB No. 292 73 2105, whichever occurs later.
    (iii) For the purposes of this AD, a serviceable HMU is an HMU 
fitted with a new constant delta P diaphragm in accordance with 
Turbomeca Mandatory Service Bulletin (MSB) No. 292 73 2818, Original 
Issue, Dated October 18, 2006, Update No. 1, dated April 3, 2007, or 
Version C, dated January 29, 2009.

Optional Terminating Action

    (3) Replacing the HMU with an HMU that has been modified to 
TU157 terminates the repetitive requirement of paragraph (e)(2)(ii) 
of this AD.

FAA AD Differences

    (f) This AD differs from the Mandatory Continuing Airworthiness 
Information (MCAI) because the MCAI applies to the ARRIEL 2B1 and 
2B1A engines. The ARRIEL 2B1A engine is not type certificated in the 
United States, so this proposed AD applies to the ARRIEL 2B1 engine 
model only.

Alternative Methods of Compliance (AMOCs)

    (g) The Manager, Engine Certification Office, FAA, has the 
authority to approve AMOCs for this AD, if requested using the 
procedures found in 14 CFR 39.19.

Related Information

    (h) Contact Kevin Dickert, Aerospace Engineer, Engine 
Certification Office, FAA, Engine & Propeller Directorate, 12 New 
England Executive Park, Burlington, MA 01803; e-mail: 
[email protected]; telephone (781) 238-7117; fax (781) 238-7199, 
for more information about this AD.

Material Incorporated by Reference

    (i) None.



[[Page 30689]]


    Issued in Burlington, Massachusetts, on May 24, 2010.
Peter A. White,
Assistant Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. 2010-13133 Filed 6-1-10; 8:45 am]
BILLING CODE 4910-13-P