Document ID: FAA-2016-4551-0001
Agency: faa
Document Type: Proposed Rule
Title: Airworthiness Directives: Rolls-Royce Deutschland Ltd and Co KG Turbofan Engines
Posted Date: 2016-04-01T04:00Z

[Federal Register Volume 81, Number 63 (Friday, April 1, 2016)]
[Proposed Rules]
[Pages 18806-18808]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2016-07378]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2016-4551; Directorate Identifier 2016-NE-07-AD]
RIN 2120-AA64

Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG 
Turbofan Engines

AGENCY: Federal Aviation Administration (FAA), DOT.

[[Page 18807]]

ACTION: Notice of proposed rulemaking (NPRM).

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SUMMARY: We propose to adopt a new airworthiness directive (AD) for 
certain Rolls-Royce Deutschland Ltd & Co KG (RRD) BR700-710A1-10, -
710A2-20, and -710C4-11 turbofan engines. This proposed AD was prompted 
by a seized low-pressure turbine (LPT) fuel shut-off pawl carrier 
caused by corrosion of the pawl carrier pivot pin. This proposed AD 
would require removing the pawl carrier pivot pins, part number (P/N) 
BRR17117, from service and replacing them with parts eligible for 
installation. We are proposing this AD to prevent failure of the fuel 
shut-off mechanism, uncontained part release, damage to the engine, and 
damage to the airplane.

DATES: We must receive comments on this proposed AD by May 31, 2016.

ADDRESSES: You may send comments by any of the following methods:
     Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments.
     Mail: Docket Management Facility, U.S. Department of 
Transportation, 1200 New Jersey Avenue SE., West Building Ground Floor, 
Room W12-140, Washington, DC 20590-0001.
     Hand Delivery: Deliver to Mail address above between 9 
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
     Fax: 202-493-2251.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-
4551; 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 proposed AD, the mandatory continuing airworthiness 
information (MCAI), the regulatory evaluation, any comments received, 
and other information. The address for the Docket Office (phone: 800-
647-5527) is in the ADDRESSES section. Comments will be available in 
the AD docket shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Philip Haberlen, Aerospace Engineer, 
Engine Certification Office, FAA, Engine & Propeller Directorate, 1200 
District Avenue, Burlington, MA 01803; phone: 781-238-7770; fax: 781-
238-7199; email: philip.haberlen@faa.gov.

SUPPLEMENTARY INFORMATION: 

Comments Invited

    We invite you to send any written relevant data, views, or 
arguments about this NPRM. Send your comments to an address listed 
under the ADDRESSES section. Include ``Docket No. FAA-2016-4551; 
Directorate Identifier 2016-NE-07-AD'' at the beginning of your 
comments. We specifically invite comments on the overall regulatory, 
economic, environmental, and energy aspects of this NPRM. We will 
consider all comments received by the closing date and may amend this 
NPRM based on those comments.
    We will post all comments we receive, without change, to http://www.regulations.gov, including any personal information you provide. We 
will also post a report summarizing each substantive verbal contact 
with FAA personnel concerning this NPRM.

Discussion

    The European Aviation Safety Agency (EASA), which is the Technical 
Agent for the Member States of the European Community, has issued EASA 
AD 2016-0034, dated February 24, 2016 (referred to hereinafter as ``the 
MCAI''), to correct an unsafe condition for the specified products. The 
MCAI states:

    Seizing of a fuel shut-off mechanism pawl carrier was reported. 
The subsequent investigation determined that corrosion of the pawl 
carrier pivot pin P/N BRR17117, was the failure cause.
    This condition, if not corrected, could lead to loss of the fuel 
shut-off mechanism functionality and loss of the engine over-speed 
protection, possibly resulting in release of high-energy debris, 
with consequent damage to, and/or reduced control of the airplane.

    You may obtain further information by examining the MCAI in the AD 
docket on the Internet at http://www.regulations.gov by searching for 
and locating Docket No. FAA-2016-4551.

FAA's Determination and Requirements of This Proposed AD

    This product has been approved by the aviation authority of 
Germany, and is approved for operation in the United States. Pursuant 
to our bilateral agreement with the European Community, EASA has 
notified us of the unsafe condition described in the MCAI and service 
information referenced above. We are proposing this AD because we 
evaluated all information provided by EASA and determined the unsafe 
condition exists and is likely to exist or develop on other products of 
the same type design. This NPRM would require removing the pawl carrier 
pivot pin, P/N BRR17117, from service and replacing with a part 
eligible for installation.

Related Service Information

    RRD has issued ASB SB-BR700-72-A101523, Revision 3, dated December 
10, 2015. The service information describes procedures for replacing 
the pawl carrier pivot pins. This service information is reasonably 
available because the interested parties have access to it through 
their normal course of business or by the means identified in the 
ADDRESSES section.

Costs of Compliance

    We estimate that this proposed AD affects 4 engines installed on 
airplanes of U.S. registry. We also estimate that it would take about 3 
hours per engine to comply with this proposed AD. The average labor 
rate is $85 per hour. Required parts cost about $860 per engine. Based 
on these figures, we estimate the cost of this proposed AD on U.S. 
operators to be $4,460.

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 proposed AD would not have federalism 
implications under Executive Order 13132. This proposed AD would 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 proposed 
regulation:
    (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),

[[Page 18808]]

    (3) Will not affect intrastate aviation in Alaska to the extent 
that it justifies making a regulatory distinction, 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.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by 
reference, Safety.

The Proposed Amendment

    Accordingly, under the authority delegated to me by the 
Administrator, the FAA proposes to amend 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 airworthiness 
directive (AD):

Rolls-Royce Deutschland GmbH (Type Certificate previously held by 
Rolls-Royce Deutschland GmbH, formerly BMW Rolls-Royce GmbH): Docket 
No. FAA-2016-4551; Directorate Identifier 2016-NE-07-AD.

(a) Comments Due Date

    We must receive comments by May 31, 2016.

(b) Affected ADs

    None.

(c) Applicability

    (1) This AD applies to:
    (i) Rolls-Royce Deutschland (RRD) BR700-710A1-10 engines with 
serial number (S/N) 11505 and below and with a low-pressure turbine 
(LPT) module, part number (P/N) M51-104 or P/N M51-111, installed;
    (ii) RRD BR700-710A2-20 engines with S/N 12492 and below and 
with an LPT module, P/N M51-108 or P/N M51-111, installed;
    (iii) RRD BR700-710C4-11 engines with S/N 15277 and below, with 
configuration standard 710C4-11 engraved on the engine data plate 
and with an LPT module, P/N M51-112, installed; and
    (iv) RRD BR700-710C4-11 engines with S/N 15329 and below, with 
configuration standard 710C4-11/10 engraved on the engine data plate 
and with an LPT module, P/N M51-112, installed.
    (2) Reserved.

(d) Reason

    This AD was prompted by a seized LPT fuel shut-off pawl carrier 
caused by corrosion of the pawl carrier pivot pin. We are issuing 
this AD to prevent failure of the fuel shut-off mechanism, 
uncontained part release, damage to the engine, and damage to the 
airplane.

(e) Actions and Compliance

    Comply with this AD within the compliance times specified, 
unless already done.
    (1) Within 6 months after the effective date of this AD, remove 
each pawl carrier pivot pin, P/N BRR17117, from service and replace 
with a part eligible for installation.
    (2) Reserved.

(f) Alternative Methods of Compliance (AMOCs)

    The Manager, Engine Certification Office, FAA, may approve AMOCs 
for this AD. Use the procedures found in 14 CFR 39.19 to make your 
request. You may email your request to: ANE-AD-AMOC@faa.gov.

(g) Related Information

    (1) For more information about this AD, contact Philip Haberlen, 
Aerospace Engineer, Engine Certification Office, FAA, Engine & 
Propeller Directorate, 1200 District Avenue, Burlington, MA 01803; 
phone: 781-238-7770; fax: 781-238-7199; email: 
philip.haberlen@faa.gov.
    (2) Refer to MCAI European Aviation Safety Agency AD 2016-0034, 
dated February 24, 2016, for more information. You may examine the 
MCAI in the AD docket on the Internet at http://www.regulations.gov 
by searching for and locating it in Docket No. FAA-2016-4551.
    (3) RRD Alert Service Bulletin SB-BR700-72-A101523, Revision 3, 
dated December 10, 2015, can be obtained from RRD using the contact 
information in paragraph (g)(4) of this AD.
    (4) For service information identified in this AD, contact 
Rolls-Royce Deutschland Ltd & Co KG, Eschenweg 11, Dahlewitz, 15827 
Blankenfelde-Mahlow, Germany; phone: +49 (0) 33 7086 2673; fax: +49 
(0) 33 7086 3276.
    (5) You may view this service information at the FAA, Engine & 
Propeller Directorate, 1200 District Avenue, Burlington, MA 01803. 
For information on the availability of this material at the FAA, 
call 781-238-7125.

    Issued in Burlington, Massachusetts, on March 25, 2016.
Colleen M. D'Alessandro,
Manager, Engine & Propeller Directorate, Aircraft Certification 
Service.
[FR Doc. 2016-07378 Filed 3-31-16; 8:45 am]
 BILLING CODE 4910-13-P