Federal Register / Vol. 80, No. 13 / Wednesday, January 21, 2015 / Rules and Regulations 2817 

Design Organization Approval (DOA). If 

approved by the DOA, the approval must 

include the DOA-authorized signature. 

(j) Related Information 

Refer to Mandatory Continuing 

Airworthiness Information (MCAI) EASA 

Airworthiness Directive 2014–0021, dated 

January 20, 2014, for related information. 

This MCAI may be found in the AD docket 

on the Internet at http://

www.regulations.gov/

#!documentDetail;D=FAA-2014-0626-0002. 

(k) Material Incorporated by Reference 

(1) The Director of the Federal Register 

approved the incorporation by reference 

(IBR) of the service information listed in this 

paragraph under 5 U.S.C. 552(a) and 1 CFR 

part 51. 

(2) You must use this service information 

as applicable to do the actions required by 

this AD, unless this AD specifies otherwise. 

(i) Chapter 5–40, Airworthiness 

Limitations, DGT 131028, Revision 15, dated 

March 2012, of the Dassault Aviation Falcon 

20 Maintenance Manual. The document 

revision level can only be found on the title 

page, Note to Users page, and pages 1 and 2 

of 9 of this document. 

(ii) Reserved. 

(3) For service information identified in 

this AD, contact Dassault Falcon Jet, P.O. Box 

2000, South Hackensack, NJ 07606; 

telephone 201–440–6700; Internet http://

www.dassaultfalcon.com. 

(4) You may view this service information 

at the FAA, Transport Airplane Directorate, 

1601 Lind Avenue SW., Renton, WA. For 

information on the availability of this 

material at the FAA, call 425–227–1221. 

(5) You may view this service information 

that is incorporated by reference 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/ibrlocations.html. 

Issued in Renton, Washington, on 

December 19, 2014. 

Michael Kaszyski, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2014–30917 Filed 1–20–15; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2014–0530; Directorate 

Identifier 2014–NM–062–AD; Amendment 

39–18057; AD 2014–26–06] 

RIN 2120–AA64 

Airworthiness Directives; ATR—GIE 

Avions de Transport Re ́gional 

Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 

ATR—GIE Avions de Transport 

Re ́gional Model ATR42–500 airplanes, 

and Model ATR72–212A airplanes. This 

AD was prompted by a report that, 

during an inspection of an airplane on 

the production line, interference was 

detected between the electrical harness 

and a bonding lead due to an incorrect 

installation of the affected bonding lead. 

This AD requires a detailed inspection 

for damage or incorrect routing of the 

bonding lead routing above the 120VU 

shelf, and if any damage or incorrect 

routing is found, repairing damage or 

modifying the bonding lead routing. We 

are issuing this AD to detect and correct 

installation of the bonding lead, which 

could cause arcing and chafing, and 

could possibly result in an uncontrolled 

fire. 

DATES: This AD becomes effective 

February 25, 2015. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in this AD 

as of February 25, 2015. 

ADDRESSES: You may examine the AD 

docket on the Internet at http:// 

www.regulations.gov/ 

#!docketDetail;D=FAA-2014-0530 or in 

person at the Docket Management 

Facility, U.S. Department of 

Transportation, Docket Operations, M– 

30, West Building Ground Floor, Room 

W12–140, 1200 New Jersey Avenue SE., 

Washington, DC. 

For service information identified in 

this AD, contact ATR—GIE Avions de 

Transport Re ́gional, 1, Alle ́e Pierre 

Nadot, 31712 Blagnac Cedex, France; 

telephone +33 (0) 5 62 21 62 21; fax +33 

(0) 5 62 21 67 18; email 

continued.airworthiness@atr.fr; Internet 

http://www.aerochain.com. You may 

view this referenced service information 

at the FAA, Transport Airplane 

Directorate, 1601 Lind Avenue SW., 

Renton, WA. For information on the 

availability of this material at the FAA, 

call 425–227–1221. 

FOR FURTHER INFORMATION CONTACT: Tom 

Rodriguez, Aerospace Engineer, 

International Branch, ANM–116, 

Transport Airplane Directorate, FAA, 

1601 Lind Avenue SW., Renton, WA 

98057–3356; telephone 425–227–1137; 

fax 425–227–1149. 

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 certain ATR—GIE Avions de 

Transport Re ́gional Model ATR42–500 

airplanes, and Model ATR72–212A 

airplanes. The NPRM published in the 

Federal Register on August 13, 2014 (79 

FR 47390). 

The European Aviation Safety Agency 

(EASA), which is the Technical Agent 

for the Member States of the European 

Community, has issued Airworthiness 

Directive 2014–0056, dated March 7, 

2014 (referred to after this as the 

Mandatory Continuing Airworthiness 

Information, or ‘‘the MCAI’’), to correct 

an unsafe condition for certain ATR— 

GIE Avions de Transport Re ́gional 

Model ATR42–500 airplanes, and Model 

ATR72–212A airplanes. The MCAI 

states: 

During inspection of an aeroplane on the 

production line, interference was detected 

between electrical harnesses (2M–2S–6M) 

and a bonding lead, located in zone 214, 

positioned above and forward of the 120VU 

shelf. Subsequent investigation revealed that 

the interference was a result of an incorrect 

installation of the affected bonding lead. 

This condition, if not detected and 

corrected, could lead to arcing and chafing, 

possibly resulting in an uncontrolled fire. 

To address this potential unsafe condition, 

ATR issued Service Bulletin (SB) ATR42–92– 

0025 and SB ATR72–92–1034, as applicable 

to aeroplane model, to provide inspection 

instructions. 

For the reasons described above, this 

[EASA] AD requires a one-time [detailed] 

inspection [for damage or incorrect routing of 

the bonding lead routing above the 120VU 

shelf] of the electrical harness 2M–2S–6M in 

zone 214 and, depending on findings, 

accomplishment of corrective action(s) 

[repairing damage or modifying the bonding 

lead routing]. 

You may examine the MCAI in the 

AD docket on the Internet at http:// 

www.regulations.gov/ 

#!documentDetail;D=FAA-2014-0530- 

0002. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

received no comments on the NPRM (79 


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2818 Federal Register / Vol. 80, No. 13 / Wednesday, January 21, 2015 / Rules and Regulations 

FR 47390, August 13, 2014) or on the 

determination of the cost to the public. 

Clarification of Corrective Actions 

In paragraph (h) of the NPRM (79 FR 

47390, August 13, 2014), we specify 

modifying the bonding lead routing if 

any damage or incorrect routing is 

found and we refer to ATR Service 

Bulletin ATR42–92–0025, dated 

November 7, 2013; and ATR Service 

Bulletin ATR72–92–1034, dated 

November 7, 2013; as the appropriate 

sources of service information. 

However, ATR Service Bulletin ATR42– 

92–0025, dated November 7, 2013; and 

ATR Service Bulletin ATR72–92–1034, 

dated November 7, 2013, only provide 

corrective action if incorrect routing is 

found. Therefore, operators would have 

to contact the FAA for corrective action 

if any damage is found. 

We have re-designated paragraph (h) 

of the NPRM (79 FR 47390, August 13, 

2014) as paragraph (h)(1) of this AD. In 

paragraph (h)(1) of this AD, we specify 

modifying the bonding lead routing if 

any incorrect routing is found, in 

accordance with ATR Service Bulletin 

ATR42–92–0025, dated November 7, 

2013; or ATR Service Bulletin ATR72– 

92–1034, dated November 7, 2013. We 

have also added paragraph (h)(2) to this 

AD to specify doing a repair if any 

damage is found, in accordance with a 

method approved by the Manager, 

International Branch, ANM–116, 

Transport Airplane Directorate, FAA. 

Conclusion 

We reviewed the relevant data and 

determined that air safety and the 

public interest require adopting this AD 

with the change described previously 

and except for minor editorial changes. 

We have determined that these minor 

changes: 

• Are consistent with the intent that 

was proposed in the NPRM (79 FR 

47390, August 13, 2014) for correcting 

the unsafe condition; and 

• Do not add any additional burden 

upon the public than was already 

proposed in the NPRM (79 FR 47390, 

August 13, 2014). 

Costs of Compliance 

We estimate that this AD affects 5 

airplanes of U.S. registry. 

We also estimate that it will take 

about 2 work-hours per product to 

comply with the basic requirements of 

this AD. The average labor rate is $85 

per work-hour. Required parts will cost 

about $0 per product. Based on these 

figures, we estimate the cost of this AD 

on U.S. operators to be $850, or $170 

per product. 

In addition, we estimate that any 

necessary follow-on actions will take 

about 2 work-hours and require parts 

costing $0, for a cost of $170 per 

product. We have no way of 

determining the number of aircraft that 

might need this action. 

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 that 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; 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. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http:// 

www.regulations.gov/ 

#!docketDetail;D=FAA-2014-0530; or in 

person at the Docket Management 

Facility 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 in the ADDRESSES

section. 

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): 

2014–26–06 ATR—GIE Avions de 

Transport Re ́gional: Amendment 39– 

18057. Docket No. FAA–2014–0530; 

Directorate Identifier 2014–NM–062–AD. 

(a) Effective Date 

This AD becomes effective February 25, 

2015. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to ATR—GIE Avions de 

Transport Re ́gional airplanes, certificated in 

any category, as identified in paragraph (c)(1) 

and (c)(2) of this AD. 

(1) Model ATR42–500 airplanes, 

manufacturer serial numbers 669 through 

1005 inclusive. 

(2) Model ATR72–212A airplanes, 

manufacturer serial numbers 773, 774, 776 

through 1094 inclusive, 1096 through 1099 

inclusive, and 1101. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 92, Electrical Routing. 

(e) Reason 

This AD was prompted by a report that, 

during an inspection of an airplane on the 

production line, interference was detected 

between the electrical harness and a bonding 

lead due to an incorrect installation of the 

affected bonding lead. We are issuing this AD 

to detect and correct installation of the 

bonding lead, which could cause arcing and 

chafing, and could possibly result in an 

uncontrolled fire. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 


wreier-aviles on DSK4TPTVN1PROD with RULES
Federal Register / Vol. 80, No. 13 / Wednesday, January 21, 2015 / Rules and Regulations 2819 

(g) Inspection 

Within 1,000 flight hours after the effective 

date of this AD: Do a detailed inspection of 

the bonding lead routing above the 120VU 

shelf for damage (i.e., wire chafing, evidence 

of burning) or incorrect routing, in 

accordance with the Accomplishment 

Instructions of ATR Service Bulletin ATR42– 

92–0025, dated November 7, 2013 (for Model 

ATR42–500 airplanes); or ATR Service 

Bulletin ATR72–92–1034, dated November 7, 

2013 (for Model ATR72–212A airplanes). 

(h) Corrective Actions 

(1) If, during the inspection required by 

paragraph (g) of this AD, any incorrect 

routing is found: Before further flight, modify 

the bonding lead routing above the 120VU 

shelf, in accordance with the 

Accomplishment Instructions of ATR Service 

Bulletin ATR42–92–0025, dated November 7, 

2013 (for Model ATR42–500 airplanes); or 

ATR Service Bulletin ATR72–92–1034, dated 

November 7, 2013 (for Model ATR72–212A 

airplanes). 

(2) If, during the inspection required by 

paragraph (g) of this AD, any damage (i.e., 

wire chafing, evidence of burning) is found: 

Before further flight, repair using a method 

approved by the Manager, International 

Branch, ANM–116, Transport Airplane 

Directorate, FAA. 

(i) Other FAA AD Provisions 

The following provisions also apply to this 

AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, International 

Branch, ANM–116, Transport Airplane 

Directorate, FAA, has the authority to 

approve AMOCs for this AD, if requested 

using the procedures found in 14 CFR 39.19. 

In accordance with 14 CFR 39.19, send your 

request to your principal inspector or local 

Flight Standards District Office, as 

appropriate. If sending information directly 

to the International Branch, send it to ATTN: 

Tom Rodriguez, Aerospace Engineer, 

International Branch, ANM–116, Transport 

Airplane Directorate, FAA, 1601 Lind 

Avenue SW., Renton, WA 98057–3356; 

telephone 425–227–1137; fax 425–227–1149. 

Information may be emailed to: 9-ANM-116- 

AMOC-REQUESTS@faa.gov. Before using 

any approved AMOC, notify your appropriate 

principal inspector, or lacking a principal 

inspector, the manager of the local flight 

standards district office/certificate holding 

district office. The AMOC approval letter 

must specifically reference this AD. 

(2) Contacting the Manufacturer: For any 

requirement in this AD to obtain corrective 

actions from a manufacturer, the action must 

be accomplished using a method approved 

by the Manager, International Branch, ANM– 

116, Transport Airplane Directorate, FAA; or 

the European Aviation Safety Agency 

(EASA); or ATR—GIE Avions de Transport 

Re ́gional’s EASA Design Organization 

Approval (DOA). If approved by the DOA, 

the approval must include the DOAauthorized signature. 

(j) Related Information 

Refer to Mandatory Continuing 

Airworthiness Information (MCAI) European 

Aviation Safety Agency Airworthiness 

Directive 2014–0056, dated March 7, 2014, 

for related information. This MCAI may be 

found in the AD docket on the Internet at 

http://www.regulations.gov/ 

#!documentDetail;D=FAA-2014-0530-0002. 

(k) Material Incorporated by Reference 

(1) The Director of the Federal Register 

approved the incorporation by reference 

(IBR) of the service information listed in this 

paragraph under 5 U.S.C. 552(a) and 1 CFR 

part 51. 

(2) You must use this service information 

as applicable to do the actions required by 

this AD, unless this AD specifies otherwise. 

(i) ATR Service Bulletin ATR42–92–0025, 

dated November 7, 2013. 

(ii) ATR Service Bulletin ATR72–92–1034, 

dated November 7, 2013. 

(3) For service information identified in 

this AD, contact ATR—GIE Avions de 

Transport Re ́gional, 1, Alle ́e Pierre Nadot, 

31712 Blagnac Cedex, France; telephone +33 

(0) 5 62 21 62 21; fax +33 (0) 5 62 21 67 18; 

email continued.airworthiness@atr.fr; 

Internet http://www.aerochain.com. 

(4) You may view this service information 

at the FAA, Transport Airplane Directorate, 

1601 Lind Avenue SW., Renton, WA. For 

information on the availability of this 

material at the FAA, call 425–227–1221. 

(5) You may view this service information 

that is incorporated by reference 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/ibrlocations.html. 

Issued in Renton, Washington, on 

December 19, 2014. 

Michael Kaszycki, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2014–30914 Filed 1–20–15; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF JUSTICE 

28 CFR Part 50 

[Docket No. 145; AG Order No. 3486–2015] 

Policy Regarding Obtaining 

Information From, or Records of, 

Members of the News Media; and 

Regarding Questioning, Arresting, or 

Charging Members of the News Media 

AGENCY: Office of the Attorney General, 

Department of Justice. 

ACTION: Final rule. 

SUMMARY: This rule amends the policy 

of the Department of Justice regarding 

the use of subpoenas, certain court 

orders, and search warrants, to obtain 

information from, or records of, 

members of the news media. The rule 

also amends the Department’s policy 

regarding questioning, arresting, or 

charging members of the news media. 

DATES: This rule is effective on January 

21, 2015. 

FOR FURTHER INFORMATION CONTACT: 

Monique Roth, Director, Office of 

Enforcement Operations, Criminal 

Division, (202) 514–6809. 

SUPPLEMENTARY INFORMATION: 

Discussion 

On February 21, 2014, the Attorney 

General issued revisions to the 

Department’s policy regarding obtaining 

information from, or records of, 

members of the news media; and 

regarding questioning, arresting, or 

charging members of the news media. In 

response to comments from federal 

prosecutors and other interested parties, 

including news media representatives, 

the Attorney General is issuing this final 

rule to revise the existing provisions in 

the Department’s regulations at 28 CFR 

50.10. 

Most of the revisions are intended to 

ensure both consistent interpretation 

and application of the policy and the 

highest level of oversight when 

members of the Department seek to 

obtain information from, or records of, 

a member of the news media. Other 

substantive revisions are intended to 

clarify the scope of the policy. 

Regulatory Certifications 

Administrative Procedure Act, 5 U.S.C. 

553 

Because, for purposes of the 

Administrative Procedure Act, this 

regulation concerns general statements 

of policy, or rules of agency 

organization, procedure, or practice, 

notice and comment and a delayed 

effective date are not required. See 5 

U.S.C. 553(b)(A). 

Regulatory Flexibility Act 

Because this final rule is not 

promulgated as a final rule under 5 

U.S.C. 553 and was not required under 

that section to be published as a 

proposed rule, the requirements for the 

preparation of a regulatory flexibility 

analysis under 5 U.S.C. 604(a) do not 

apply. In any event, the Attorney 

General, in accordance with 5 U.S.C. 

605(b), has reviewed this regulation and 

by approving it certifies that this 

regulation will not have a significant 

economic impact on a substantial 

number of small entities because it 

pertains to administrative matters 

affecting the Department. 


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