[Federal Register Volume 75, Number 59 (Monday, March 29, 2010)]
[Rules and Regulations]
[Pages 15321-15322]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2010-5788]
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Rules and Regulations
Federal Register
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Federal Register / Vol. 75, No. 59 / Monday, March 29, 2010 / Rules
and Regulations
[[Page 15321]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2009-1004; Directorate Identifier 2009-NE-36-AD;
Amendment 39-16239; AD 2010-06-14]
RIN 2120-AA64
Airworthiness Directives; Rolls-Royce plc RB211-Trent 800 Series
Turbofan Engines
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
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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:
During 2004, an incident was reported involving uncontained
multiple intermediate-pressure (IP) turbine blade release on a Trent
700 engine. The blade release was the result of an overspeed of the
IP turbine rotor that was initiated by an internal fire in the high-
pressure/intermediate-pressure (HP/IP) bearing chamber. Post-
incident analysis and investigation has established that blockage of
the HP/IP turbine bearing oil vent tube due to carbon deposits was a
significant factor in the failure sequence. The Trent 800 has a
similar type design standard to that of the Trent 700 and has also
been found in service to be susceptible to carbon deposits in the
oil vent tube.
We are issuing this AD to prevent internal oil fires due to coking and
carbon buildup in the HP/IP turbine bearing oil vent tube that could
cause uncontained engine failure and damage to the airplane.
DATES: This AD becomes effective May 3, 2010. The Director of the
Federal Register approved the incorporation by reference of certain
publications listed in this AD as of May 3, 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: James Lawrence, Aerospace Engineer,
Engine Certification Office, FAA, Engine and Propeller Directorate, 12
New England Executive Park, Burlington, MA 01803; e-mail:
[email protected]; telephone (781) 238-7176; 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 January 5, 2010 (75
FR 264). That NPRM proposed to correct an unsafe condition for the
specified products. The MCAI states:
During 2004, an incident was reported involving uncontained
multiple IP turbine blade release on a Trent 700 engine. The blade
release was the result of an overspeed of the IP turbine rotor that
was initiated by an internal fire in the HP/IP bearing chamber.
Post-incident analysis and investigation has established that
blockage of the HP/IP turbine bearing oil vent tube due to carbon
deposits was a significant factor in the failure sequence. The Trent
800 has a similar type design standard to that of the Trent 700 and
has also been found in service to be susceptible to carbon deposits
in the oil vent tube.
Comments
We gave the public the opportunity to participate in developing
this AD. We considered the comment received. The commenter supports the
NPRM.
Conclusion
We reviewed the available data, including the comment received, and
determined that air safety and the public interest require adopting the
AD as proposed.
Costs of Compliance
Based on the service information, we estimate that this AD will
affect about 138 RB211 Trent 800 series turbofan engines installed on
airplanes of U.S. registry. We also estimate that it will take about
one work-hour per engine to comply with this AD. The average labor rate
is $80 per work-hour. Required parts will cost about $2,000 per engine.
Based on these figures, we estimate the cost of the AD on U.S.
operators to be $287,040.
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.
[[Page 15322]]
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 (telephone (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, 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:
2010-06-14 Rolls-Royce plc: Amendment 39-16239. Docket No. FAA-2009-
1004; Directorate Identifier 2009-NE-36-AD.
Effective Date
(a) This airworthiness directive (AD) becomes effective May 3,
2010.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Rolls-Royce plc models RB211-Trent 875-
17, Trent 877-17, Trent 884-17, Trent 884B-17, Trent 892-17, Trent
892B-17, and Trent 895-17 turbofan engines. These engines are
installed on, but not limited to, Boeing 777 series airplanes.
Reason
(d) During 2004, an incident was reported involving uncontained
multiple intermediate-pressure (IP) turbine blade release on a Trent
700 engine. The blade release was the result of an overspeed of the
IP turbine rotor that was initiated by an internal fire in the high-
pressure/intermediate-pressure (HP/IP) bearing chamber. Post-
incident analysis and investigation has established that blockage of
the HP/IP turbine bearing oil vent tube due to carbon deposits was a
significant factor in the failure sequence. The Trent 800 has a
similar type design standard to that of the Trent 700 and has also
been found in service to be susceptible to carbon deposits in the
oil vent tube.
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. We are issuing this AD to prevent internal oil fires due to
coking and carbon buildup in the HP/IP turbine bearing oil vent tube
that could cause uncontained engine failure and damage to the
airplane.
Actions and Compliance
(e) Unless already done, do the following actions.
(1) At the next engine shop visit after the effective date of
this AD and thereafter at each engine shop visit, using the
Accomplishment Instructions of Rolls-Royce plc Alert Service
Bulletin No. RB.211-72-AE362, Revision 1, dated April 3, 2009:
(i) Inspect the HP/IP turbine bearing internal and external oil
vent tubes and bearing chamber for carbon buildup.
(ii) Clean and flush the tubes and bearing chamber as required.
(iii) Reject any oil vent tubes that do not meet inspection
requirements after cleaning.
(2) This AD does not require reporting of inspection results, as
does paragraphs 3.B.(4)(g) and 3.C.(9) of Rolls-Royce plc Alert
Service Bulletin No. RB.211-72-AE362, Revision 1, dated April 3,
2009.
FAA AD Differences
(f) None.
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) Refer to MCAI European Aviation Safety Agency AD 2009-0071
(corrected April 14, 2009), for related information.
(i) Contact James Lawrence, Aerospace Engineer, Engine
Certification Office, FAA, Engine and Propeller Directorate, 12 New
England Executive Park, Burlington, MA 01803; e-mail:
[email protected]; telephone (781) 238-7176; fax (781) 238-
7199, for more information about this AD.
Material Incorporated by Reference
(j) You must use Rolls-Royce plc Alert Service Bulletin No.
RB.211-72-AE362, Revision 1, dated April 3, 2009, 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
Rolls-Royce plc, PO Box 31, Derby, England; telephone: 011-44-1332-
249428; fax: 011-44-1332-249223.
(3) You may review copies at the FAA, New England Region, 12 New
England Executive Park, Burlington, MA; or 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 Burlington, Massachusetts on March 9, 2010.
Peter A. White,
Assistant Manager, Engine and Propeller Directorate, Aircraft
Certification Service.
[FR Doc. 2010-5788 Filed 3-26-10; 8:45 am]
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