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[Federal Register: April 2, 2010 (Volume 75, Number 63)]
[Rules and Regulations]               
[Page 16655-16657]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr02ap10-6]                         

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2005-19559; Directorate Identifier 2004-NE-03-AD; 
Amendment 39-16254; AD 2010-07-09]
RIN 2120-AA64

 
Airworthiness Directives; Rolls-Royce plc RB211-Trent 700 Series 
Turbofan Engines

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

ACTION: Final rule.

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SUMMARY: The FAA is superseding an existing airworthiness directive 
(AD) for Rolls-Royce plc RB211-Trent 700 series turbofan engines. That 
AD currently requires initial and repetitive borescope inspections of 
the high-pressure-and-intermediate pressure (HP-IP) turbine internal 
and external oil vent tubes for coking and carbon buildup, and cleaning 
or replacing the vent tubes if necessary. This AD requires the same 
actions, but adds additional inspections of the vent flow restrictor. 
This AD results from further analysis that the cleaning of the vent 
tubes required by AD 2007-02-05 could lead to loosened carbon 
fragments, causing a blockage downstream in the vent flow restrictor. 
We are issuing this AD to prevent internal oil fires due to coking and 
carbon buildup that could cause uncontained engine failure and damage 
to the airplane.

DATES: This AD becomes effective May 7, 2010. The Director of the 
Federal Register approved the incorporation by reference of certain 
publications listed in the regulations as of May 7, 2010.

ADDRESSES: You can get the service information identified in this AD 
from Rolls-Royce plc, P.O. Box 31, Derby, England; telephone: 011-44-
1332-249428; fax: 011-44-1332-249223.
    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: 
james.lawrence@faa.gov; telephone (781) 238-7176; fax (781) 238-7199.

SUPPLEMENTARY INFORMATION: The FAA proposed to amend 14 CFR part 39 by 
superseding AD 2007-02-05, Amendment 39-14892 (72 FR 2603, January 22, 
2007), with a proposed AD. The proposed AD applies to Rolls-Royce plc 
RB211-Trent 700 series turbofan engines. We published the proposed AD 
in the Federal Register on October 26, 2009 (74 FR 54940). That action 
proposed to require initial and repetitive borescope inspections of the 
HP-IP turbine internal and external oil vent tubes for coking and 
carbon buildup, cleaning or replacing the vent tubes if necessary, and 
inspections of the vent flow restrictor.

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,

[[Page 16656]]

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.

Comments

    We provided the public the opportunity to participate in the 
development of this AD. We have considered the comments received.

Request to Reference the Latest Service Bulletin

    One commenter, Rolls-Royce plc, requests that we incorporate by 
reference the latest alert service bulletin (ASB) in the AD, which is 
ASB No. RB.211-72-AE302, Revision 8, dated October 21, 2009.
    We agree. We changed the AD to incorporate by reference Revision 8 
of that ASB.

Request To Allow Previous Credit

    Rolls-Royce plc requests that we allow previous credit to operators 
that performed the initial inspections specified in paragraph (f) of 
the proposed AD before the AD effective date, using Revision 4, 
Revision 5, Revision 6, or Revision 7 of ASB No. RB.211-72-AE302.
    We agree and added a previous credit paragraph to the AD.

Request to Change Initial Inspection Threshold

    Rolls-Royce plc requests that we change the initial inspection 
threshold from 3 months to 2 months, to agree with the ASB.
    We agree and changed the AD.

Clarification of AD Compliance Section

    We clarified paragraphs (g) and (h) of the AD compliance section to 
better align with the Rolls-Royce plc ASB.

Conclusion

    We have carefully reviewed the available data, including the 
comments received, and determined that air safety and the public 
interest require adopting the AD with the changes described previously. 
We have determined that these changes will neither increase the 
economic burden on any operator nor increase the scope of the AD.

Costs of Compliance

    Based on the service information, we estimate that this AD will 
affect about 33 engines 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 $68,640.

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 have 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 that this AD:
    (1) Is not a ``significant regulatory action'' under Executive 
Order 12866;
    (2) Is not a ``significant rule'' under 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 summary of the costs to comply with this AD and 
placed it in the AD Docket. You may get a copy of this summary at the 
address listed under ADDRESSES.

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 Federal Aviation Administration 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 39-14892 (72 FR 
2603, January 22, 2007), and by adding a new airworthiness directive, 
Amendment 39-16254, to read as follows:

2010-07-09 Rolls-Royce plc: Amendment 39-16254. Docket No. FAA-2005-
19559; Directorate Identifier 2004-NE-03-AD.

Effective Date

    (a) This airworthiness directive (AD) becomes effective May 7, 
2010.

Affected ADs

    (b) This AD supersedes AD 2007-02-05, Amendment 39-14892.

Applicability

    (c) This AD applies to Rolls-Royce plc RB211-Trent 768-60, 
RB211-Trent 772-60, and RB211-Trent 772B-60 series turbofan engines. 
These engines are installed on, but not limited to, Airbus A330-243, 
-341, -342 and -343 series airplanes.

Unsafe Condition

    (d) This AD results from further analysis that the cleaning of 
the vent tubes required by AD 2007-02-05 could lead to loosened 
carbon fragments, causing a blockage downstream in the vent flow 
restrictor. We are issuing this AD to prevent internal oil fires due 
to coking and carbon buildup that could cause uncontained engine 
failure and damage to the airplane.

Compliance

    (e) You are responsible for having the actions required by this 
AD performed within the compliance times specified unless the 
actions have already been done.

Initial Inspections, Cleaning, and Replacements

    (f) Using the schedule in Table 1 of this AD, borescope-inspect 
and clean as necessary, the high-pressure-and-intermediate pressure 
(HP-IP) turbine internal oil vent tubes, external oil vent tubes, 
and bearing chamber.

[[Page 16657]]



                  Table 1--Initial Inspection Schedule
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     If the engine or the 05 Module           Then initially inspect
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Has reached 10,000 hours time-since-new  Within 2 months after the
 (TSN) or reached 2,500 cycles-since-     effective date of this AD.
 new (CSN) on the effective date of
 this AD.
Has fewer than 10,000 hours TSN and      Within 2 months after reaching
 fewer than 2,500 CSN on the effective    10,000 hours TSN or 2,500 CSN,
 date of this AD.                         whichever occurs first.
Is returned for an engine shop visit...  Before returning to service.
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    (1) If after cleaning, there is still carbon in the vent tube 
that prevents cleaning tool number HU80298 from passing through the 
tube, then replace the internal oil vent tube within 10 cycles-in-
service (CIS).
    (2) If after cleaning, there is still carbon of visible 
thickness in either of the two external oil vent tubes, then replace 
the external oil vent tube before further flight.
    (3) Use paragraphs 3.A. through 3.A.(7) of the Accomplishment 
Instructions and Appendix A of Rolls-Royce plc Alert Service 
Bulletin (ASB) No. RB.211-72-AE302, Revision 8, dated October 21, 
2009, to do the borescope inspections and cleaning of the oil vent 
tubes and bearing chamber.

Initial Visual Inspection of the Vent Flow Restrictor

    (g) For engines that, on the effective date of this AD, have not 
accumulated 25 service cycles since the last cleaning and inspection 
specified in paragraphs (f) through (f)(3) of this AD, visually 
inspect the vent flow restrictor:
    (1) Either after a high-power ground run immediately following 
the cleaning and inspection; or
    (2) Within 25 service cycles of the last cleaning and 
inspection.
    (h) For engines that, on the effective date of this AD, have 
accumulated 25 or more service cycles since the last cleaning and 
inspection specified in paragraphs (f) through (f)(3) of this AD, 
visually inspect the vent flow restrictor within 25 service cycles 
after the effective date of this AD.
    (i) Use paragraph 3.A.(8) of the Accomplishment Instructions of 
Rolls-Royce plc ASB No. RB.211-72-AE302, Revision 8, dated October 
21, 2009, to do the visual inspections.

Repetitive Inspections, Cleaning, and Replacements

    (j) Within 6,400 hours time-in-service since last inspection and 
cleaning, or within 1,600 cycles-since-last inspection and cleaning, 
or at the next engine shop visit, whichever occurs first, borescope-
inspect the HP-IP turbine internal and external oil vent tubes and 
bearing chamber, and clean the oil vent tubes as necessary.
    (1) If after cleaning there is still carbon in the internal oil 
vent tube that prevents cleaning tool, number HU80298, from passing 
through the tube, then replace the internal oil vent tube within 10 
CIS.
    (2) If after cleaning there is still carbon of visible 
thickness, in either of the two external oil vent tubes, then 
replace the external oil vent tube before further flight.
    (3) Use paragraphs 3.A. through 3.A.(7) of the Accomplishment 
Instructions and Appendix A of Rolls-Royce plc ASB No. RB.211-72-
AE302, Revision 8, dated October 21, 2009, to do the borescope 
inspections and cleaning of the oil vent tubes and bearing chamber.
    (k) Visually inspect the vent flow restrictor either after a 
high-power ground run or within 25 service cycles after performing 
the cleaning and inspection specified in paragraph (f) through 
(f)(3) of this AD. Use paragraph 3.A.(8) of the Accomplishment 
Instructions of Rolls-Royce plc ASB No. RB.211-72-AE302, Revision 8, 
dated October 21, 2009, to do the visual inspection.

Definition

    (l) For the purpose of this AD, an engine shop visit is 
induction of the engine into the engine shop for any cause.

Previous Credit

    (m) Initial inspections specified in paragraph (f) of this AD 
and performed before the effective date of this AD using Rolls-Royce 
plc ASB No. RB.211-72-AE302, Revision 4, dated April 30, 2007, or 
Revision 5, dated May 22, 2007, or Revision 6, dated January 29, 
2009, or Revision 7, dated April 30, 2009, satisfy the initial 
inspection requirements in paragraph (f) of this AD.

Alternative Methods of Compliance

    (n) The Manager, Engine Certification Office, has the authority 
to approve alternative methods of compliance for this AD, if 
requested using the procedures found in 14 CFR 39.19.

Related Information

    (o) European Aviation Safety Agency AD 2007-0201, dated August 
1, 2007, and AD 2007-0202 (corrected August 8, 2007), also address 
the subject of this AD.
    (p) Contact James Lawrence, Aerospace Engineer, Engine 
Certification Office, FAA, Engine & Propeller Directorate, 12 New 
England Executive Park, Burlington, MA 01803; e-mail: 
james.lawrence@faa.gov; telephone (781) 238-7176; fax (781) 238-
7199, for more information about this AD.

Material Incorporated by Reference

    (q) You must use Rolls-Royce plc Alert Service Bulletin No. 
RB.211-72-AE302, Revision 8, dated October 21, 2009, including 
Appendix A, to perform the actions required by this AD. The Director 
of the Federal Register approved the incorporation by reference of 
this service bulletin in accordance with 5 U.S.C. 552(a) and 1 CFR 
part 51. Contact Rolls-Royce plc, P.O. Box 31, Derby, England; 
telephone: 011-44-1332-249428; fax: 011-44-1332-249223 for a copy of 
this service information. 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 25, 2010.
Robert J. Ganley,
Acting Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. 2010-7283 Filed 4-1-10; 8:45 am]
BILLING CODE 4910-13-P
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