This section of the FEDERAL REGISTER

contains regulatory documents having general

applicability and legal effect, most of which

are keyed to and codified in the Code of

Federal Regulations, which is published under

50 titles pursuant to 44 U.S.C. 1510.

The Code of Federal Regulations is sold by

the Superintendent of Documents. Prices of

new books are listed in the first FEDERAL

REGISTER issue of each week.

Rules and Regulations Federal Register

21845 

Vol. 79, No. 75 

Friday, April 18, 2014 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 25 

[Docket No. FAA–2010–1175; Amdt. No. 25– 

137] 

RIN 2120–AJ83 

Installed Systems and Equipment for 

Use by the Flightcrew; Correction 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; corrections. 

SUMMARY: The Federal Aviation 

Administration (FAA) published in the 

Federal Register of May 3, 2013 a 

document amending the design 

requirements in the airworthiness 

standards for transport category 

airplanes to minimize the occurrence of 

design-related flightcrew errors. This 

document corrects an inadvertent 

amendment number that appears in the 

heading of the publication of that final 

rule. 

DATES: This correction is effective April 

18, 2014. 

FOR FURTHER INFORMATION CONTACT: 

Ralen Gao, Office of Rulemaking, ARM– 

209, Federal Aviation Administration, 

800 Independence Avenue SW., 

Washington, DC 20591; telephone (202) 

267–3168; fax (202) 267–5075; email 

ralen.gao@faa.gov. 

SUPPLEMENTARY INFORMATION: The FAA 

published a final rule in the Federal 

Register of May 3, 2013 (78 FR 25840), 

amending the design requirements in 

the airworthiness standards for 

transport category airplanes to minimize 

the occurrence of design-related 

flightcrew errors. This document 

corrects an inadvertent amendment 

number that appears in the heading of 

the publication of that final rule. 

In FR Doc. 2013–10554, beginning on 

page 25840 in the Federal Register of 

May 3, 2013, make the following 

correction: 

On page 25840, in the first column 

heading, change the amendment 

number from ‘‘25–138’’ to ‘‘25–137’’. 

Issued in Washington, DC, on April 10, 

2014. 

Lirio Liu, 

Director, Office of Rulemaking. 

[FR Doc. 2014–08565 Filed 4–17–14; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2013–0884; Directorate 

Identifier 2013–NE–31–AD; Amendment 39– 

17829; AD 2014–08–05] 

RIN 2120–AA64 

Airworthiness Directives; Rolls-Royce 

Deutschland Ltd & Co KG Turbofan 

Engines 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for all 

Rolls-Royce Deutschland Ltd & Co KG 

(RRD) BR700–715A1–30, BR700– 

715B1–30, and BR700–715C1–30 

turbofan engines. This AD requires 

replacement of the low-pressure 

compressor (LPC) case ice impact 

panels. This AD was prompted by a 

report of a partial de-bonding of the LPC 

case ice impact panels during an engine 

shop visit. We are issuing this AD to 

prevent failure of the LPC case ice 

impact panels, which could result in 

damage to the engine and loss of control 

of the airplane. 

DATES: This AD becomes effective May 

23, 2014. 

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. 

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–2013– 

0884; 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 mandatory 

continuing airworthiness information 

(MCAI), 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. 

FOR FURTHER INFORMATION CONTACT: Rose 

Len, Aerospace Engineer, Engine 

Certification Office, FAA, Engine & 

Propeller Directorate, 12 New England 

Executive Park, Burlington, MA 01803; 

phone: 781–238–7772; fax: 781–238– 

7199; email: rose.len@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 by adding an AD that would 

apply to the specified products. The 

NPRM was published in the Federal 

Register on December 23, 2013 (78 FR 

77382). The NPRM proposed to correct 

an unsafe condition for the specified 

products. The MCAI states: 

Partial de-bonding of the low-pressure 

compressor case ice impact panels was 

reported during engine shop visit. 

This condition, if not corrected, could lead 

to ice impact panel de-bonding, resulting, in 

case of an impact event and release of 

particles, in blockage of the outlet guide vane 

and consequent potential loss of thrust or 

reduced fan flutter margin. 

To address this potential unsafe condition, 

RRD issued Alert Non Modification Service 

Bulletin (NMSB) SB–BR700–72–A900281 to 

provide instructions for a one-time ice 

impact panel replacement using an improved 

repair method. 

You may examine the MCAI in the 

AD docket on the Internet at http://

www.regulations.gov/#!document

Detail;D=FAA-2013-0884-0002. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

received no comments on the NPRM (78 

FR 77382, December 23, 2013). 

Conclusion 

We reviewed the available data and 

determined that air safety and the 

public interest require adopting this AD 

as proposed. 


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21846 Federal Register / Vol. 79, No. 75 / Friday, April 18, 2014 / Rules and Regulations 

Costs of Compliance 

We estimate that this AD will affect 

about 232 engines installed on aircraft 

of U.S. registry. We also estimate that it 

will take about 24 hours per engine to 

comply with this AD. The average labor 

rate is $85 per hour. Required parts will 

cost about $9,268 per engine. Based on 

these figures, we estimate the cost of 

this AD on U.S. operators to be 

$2,623,456. 

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), 

(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. 

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 

Accordingly, under the authority 

delegated to me by the Administrator, 

the FAA amends 14 CFR part 39 as 

follows: 

PART 39—AIRWORTHINESS 

DIRECTIVES 

■ 1. The authority citation for part 39 

continues to read as follows: 

Authority: 49 U.S.C. 106(g), 40113, 44701. 

§ 39.13 [Amended] 

■ 2. The FAA amends § 39.13 by adding 

the following new airworthiness 

directive (AD): 

2014–08–05 Rolls-Royce Deutschland Ltd & 

Co KG (Type Certificate previously held 

by Rolls-Royce Deutschland GmbH and 

BMW Rolls-Royce GmbH): Amendment 

39–17829; Docket No. FAA–2013–0884; 

Directorate Identifier 2013–NE–31–AD. 

(a) Effective Date 

This AD becomes effective May 23, 2014. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to all Rolls-Royce 

Deutschland Ltd & Co KG (RRD) BR700– 

715A1–30, BR700–715B1–30, and BR700– 

715C1–30 turbofan engines. 

(d) Reason 

This AD was prompted by a report of a 

partial de-bonding of the low-pressure 

compressor (LPC) case ice impact panels 

during an engine shop visit. We are issuing 

this AD to prevent failure of the LPC case ice 

impact panels, which could result in damage 

to the engine and loss of control of the 

airplane. 

(e) Actions and Compliance 

Unless already done, after the effective 

date of this AD, at the next engine shop visit 

or within 12,500 engine flight cycles since 

the last shop visit, whichever occurs first, 

replace the four LPC ice impact panels with 

panels eligible for installation. 

(f) Definitions 

(1) For the purposes of this AD, an ‘‘engine 

shop visit’’ is the induction of an engine into 

the shop for maintenance involving the 

separation of pairs of major mating engine 

flanges. The separation of engine flanges 

solely for the purpose of transportation 

without subsequent engine maintenance does 

not constitute an engine shop visit. 

(2) For the purposes of this AD, a panel 

that is ‘‘eligible for installation’’ is a new LPC 

impact panel or one that has been repaired 

using RRD Alert Non-Modification Service 

Bulletin (NMSB) No. ALERT SB–BR700–72– 

A900281, dated July 1, 2013. 

(g) Alternative Methods of Compliance 

(AMOCs) 

The Manager, Engine Certification Office, 

FAA, may approve AMOCs to this AD. Use 

the procedures found in 14 CFR 39.19 to 

make your request. 

(h) Related Information 

(1) For more information about this AD, 

contact Rose Len, Aerospace Engineer, 

Engine Certification Office, FAA, Engine & 

Propeller Directorate, 12 New England 

Executive Park, Burlington, MA 01803; 

phone: 781–238–7772; fax: 781–238–7199; 

email: rose.len@faa.gov. 

(2) Refer to MCAI European Aviation 

Safety Agency AD 2013–0231, dated 

September 24, 2013, for more information. 

You may examine the MCAI in the AD 

docket on the Internet at http:// 

www.regulations.gov/ 

#!documentDetail;D=FAA-2013-0884-0002. 

(3) RRD Alert NMSB No. ALERT SB– 

BR700–72–A900281, dated July 1, 2013, 

which is not incorporated by reference in this 

AD, can be obtained from RRD using the 

contact information in paragraph (h)(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 

33–7086–1944; fax: 49 33–7086–3276. 

(5) You may view this service information 

at the FAA, Engine & Propeller Directorate, 

12 New England Executive Park, Burlington, 

MA. For information on the availability of 

this material at the FAA, call 781–238–7125. 

(i) Material Incorporated by Reference 

None. 

Issued in Burlington, Massachusetts, on 

April 8, 2014. 

Ann C. Mollica, 

Acting Assistant Directorate Manager, Engine 

& Propeller Directorate, Aircraft Certification 

Service. 

[FR Doc. 2014–08733 Filed 4–17–14; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 71 

[Docket No. FAA–2013–0588; Airspace 

Docket No. 13–ASW–12] 

Amendment of Class E Airspace; 

Paragould, AR 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: This action amends Class E 

airspace at Paragould, AR. 

Decommissioning of the Paragould nondirectional radio beacon (NDB) at Kirk 

Field Airport has made reconfiguration 

necessary for standard instrument 

approach procedures and for the safety 


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