7262 Federal Register / Vol. 78, No. 22 / Friday, February 1, 2013 / Rules and Regulations 

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. 

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 the NPRM (77 FR 63268, 

October 16, 2012), 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. 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 

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 AD: 

2013–02–11 Airbus: Amendment 39–17332. 

Docket No. FAA–2012–1071; Directorate 

Identifier 2012–NM–070–AD. 

(a) Effective Date 

This airworthiness directive (AD) becomes 

effective March 8, 2013. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to all Airbus Model A310– 

203 airplanes, certificated in any category. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 71, Powerplant. 

(e) Reason 

This AD was prompted by a report of an 

analysis that demonstrated a reduced fatigue 

life for the side link bolts, center sway link 

bolts, and thrust link bolts on the forward 

engine mounts. We are issuing this AD to 

prevent deterioration of the structural 

integrity of the bolts, which could result in 

possible damage to an engine or wing. 

(f) Compliance 

You are responsible for having the actions 

required by this AD performed within the 

compliance times specified, unless the 

actions have already been done. 

(g) Actions 

Within 18 months after the effective date 

of this AD, replace all side link bolts on left 

hand (LH) and right hand (RH) side of the 

engines, and all center sway link bolts and 

thrust link bolts of both engines, having any 

part number (P/N) identified in paragraphs 

(g)(1) through (g)(6) of this AD, with new 

bolts having the same part number, in 

accordance with the Accomplishment 

Instructions of Airbus Mandatory Service 

Bulletin A310–71–2037, including 

Appendices 01 and 02, dated September 30, 

2011. Repeat the bolt replacements thereafter 

at intervals not exceeding 134 months. 

(1) P/N 9021M88P01. 

(2) P/N 9021M88P02. 

(3) P/N 9205M81P01. 

(4) P/N 9021M88P03. 

(5) P/N 9021M88P04. 

(6) P/N 9205M82P01. 

(h) 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: 

Dan Rodina, Aerospace Engineer, 

International Branch, ANM–116, Transport 

Airplane Directorate, FAA, 1601 Lind 

Avenue SW., Renton, WA 98057–3356; 

telephone (425) 227–2125; fax (425) 227– 

1147. 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) Airworthy Product: For any requirement 

in this AD to obtain corrective actions from 

a manufacturer or other source, use these 

actions if they are FAA-approved. Corrective 

actions are considered FAA-approved if they 

are approved by the State of Design Authority 

(or their delegated agent). You are required 

to assure the product is airworthy before it 

is returned to service. 

(i) Related Information 

Refer to MCAI European Aviation Safety 

Agency Airworthiness Directive 2012–0056, 

dated April 3, 2012; and Airbus Mandatory 

Service Bulletin A310–71–2037, including 

Appendices 01 and 02, dated September 30, 

2011; for related information. 

(j) 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 the AD specifies otherwise. 

(i) Airbus Mandatory Service Bulletin 

A310–71–2037, including Appendices 01 

and 02, dated September 30, 2011. 

(ii) Reserved. 

(3) For service information identified in 

this AD, contact Airbus SAS—EAW 

(Airworthiness Office), 1 Rond Point Maurice 

Bellonte, 31707 Blagnac Cedex, France; 

telephone +33 5 61 93 36 96; fax +33 5 61 

93 44 51; email account.airwortheas@airbus.com; Internet http:// 

www.airbus.com. 

(4) You may review copies of the 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 January 

17, 2013. 

Michael Kaszycki, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2013–01820 Filed 1–31–13; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2012–1102; Directorate 

Identifier 2012–NM–062–AD; Amendment 

39–17333; AD 2013–02–12] 

RIN 2120–AA64 

Airworthiness Directives; EADS CASA 

(Type Certificate Previously Held by 

Construcciones Aerona ́uticas, S.A.) 

Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 


srobinson on DSK4SPTVN1PROD with RULES
Federal Register / Vol. 78, No. 22 / Friday, February 1, 2013 / Rules and Regulations 7263 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for all 

EADS CASA (Type Certificate 

previously held by Construcciones 

Aerona ́uticas, S.A.) Model CN–235, CN– 

235–100, CN–235–200, and CN–235– 

300 airplanes. This AD was prompted 

by reports of incorrect electrical polarity 

connections on engine fire 

extinguishing discharge cartridges. This 

AD requires a one-time inspection to 

identify the correct polarity for each 

pair of electrical connectors on each 

engine fire extinguisher cartridge, and 

repair if necessary. We are issuing this 

AD to detect and correct incorrect 

polarity connections, which could 

prevent the actuation of the discharge 

cartridge in case of automatic fire 

detection or manual initiation during a 

potential engine fire, and could result in 

damage to the airplane and injury to 

passengers. 

DATES: This AD becomes effective 

March 8, 2013. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of March 8, 2013. 

ADDRESSES: You may examine the AD 

docket on the Internet at http:// 

www.regulations.gov or in person at the 

U.S. Department of Transportation, 

Docket Operations, M–30, West 

Building Ground Floor, Room W12–140, 

1200 New Jersey Avenue SE., 

Washington, DC. 

FOR FURTHER INFORMATION CONTACT: 

Shahram Daneshmandi, Aerospace 

Engineer, International Branch, ANM– 

116, Transport Airplane Directorate, 

FAA, 1601 Lind Avenue SW., Renton, 

WA 98057–3356; telephone (425) 227– 

1112; fax (425) 227–1149. 

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 October 18, 2012 (77 FR 

64053). That NPRM proposed to correct 

an unsafe condition for the specified 

products. The Mandatory Continuing 

Airworthiness Information (MCAI) 

states: 

Reports have been received of finding 

wrong electrical polarity connections of 

engine fire extinguishing discharge cartridges 

on CASA CN–235 aeroplanes. The results of 

the subsequent investigation showed that the 

incorrect discharge cartridge assembly was 

caused by production line errors. 

This condition, if not detected and 

corrected, could prevent the actuation of the 

discharge cartridge in case of automatic fire 

detection or manual initiation in case of 

engine fire, possibly resulting in damage to 

the aeroplane and injury to occupants. 

To address this potential unsafe condition, 

EADS CASA (Airbus Military) developed 

instructions to identify erroneous wiring 

polarity installation. 

For the reasons described above this 

[European Aviation Safety Agency] AD 

requires a one-time inspection to verify 

proper electrical polarity of wiring of each 

engine fire extinguisher discharge cartridge 

and, depending on findings, corrective action 

[accomplish the repair]. 

You may obtain further information by 

examining the MCAI in the AD docket. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

received no comments on the NPRM (77 

FR 64053, October 18, 2012) or on the 

determination of the cost to the public. 

Conclusion 

We reviewed the available data and 

determined that air safety and the 

public interest require adopting the AD 

as proposed. 

Costs of Compliance 

We estimate that this AD will affect 6 

products of U.S. registry. We also 

estimate that it will take about 4 workhours per product to comply with the 

basic requirements of this AD. The 

average labor rate is $85 per work-hour. 

Based on these figures, we estimate the 

cost of this AD to the U.S. operators to 

be $2,040, or $340 per product. 

We have received no definitive data 

that would enable us to provide cost 

estimates for the on-condition actions 

specified in this AD. 

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. 

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 the NPRM (77 FR 64053, 

October 18, 2012), 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. 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 

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 AD: 

2013–02–12 EADS CASA (Type Certificate 

previously held by Construcciones 

Aerona ́uticas, S.A.): Amendment 39– 


srobinson on DSK4SPTVN1PROD with RULES
7264 Federal Register / Vol. 78, No. 22 / Friday, February 1, 2013 / Rules and Regulations 

17333. Docket No. FAA–2012–1102; 

Directorate Identifier 2012–NM–062–AD. 

(a) Effective Date 

This airworthiness directive (AD) becomes 

effective March 8, 2013. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to all EADS CASA (Type 

Certificate previously held by Construcciones 

Aerona ́uticas, S.A.) Model CN–235, CN–235– 

100, CN–235–200, and CN–235–300 

airplanes, certificated in any category, all 

serial numbers. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 26, Fire protection. 

(e) Reason 

This AD was prompted by reports of 

incorrect electrical polarity connections on 

engine fire extinguishing discharge 

cartridges. We are issuing this AD to detect 

and correct incorrect polarity connections, 

which could prevent the actuation of the 

discharge cartridge in case of automatic fire 

detection or manual initiation during a 

potential engine fire, and could result in 

damage to the airplane and injury to 

passengers. 

(f) Compliance 

You are responsible for having the actions 

required by this AD performed within the 

compliance times specified, unless the 

actions have already been done. 

(g) Inspection 

Within 30 days after the effective date of 

this AD, do a one-time inspection to identify 

the correct polarity for each pair of electrical 

connectors on each engine fire extinguisher 

cartridge, in accordance with the Instructions 

of Airbus Military All Operator Letter 235– 

020, dated March 9, 2012. 

(h) Corrective Action 

If, during the inspection required by 

paragraph (g) of this AD, erroneous wiring 

polarity is detected: Before further flight, 

repair in accordance with a method approved 

by the Manager, International Branch, ANM– 

116, Transport Airplane Directorate, FAA; or 

European Aviation Safety Agency (EASA) (or 

its delegated agent). 

(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: 

Shahram Daneshmandi, Aerospace Engineer, 

International Branch, ANM–116, Transport 

Airplane Directorate, FAA, 1601 Lind 

Avenue SW., Renton, WA 98057–3356; 

telephone (425) 227–1112; 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) Airworthy Product: For any requirement 

in this AD to obtain corrective actions from 

a manufacturer or other source, use these 

actions if they are FAA-approved. Corrective 

actions are considered FAA-approved if they 

are approved by the State of Design Authority 

(or their delegated agent). You are required 

to assure the product is airworthy before it 

is returned to service. 

(j) Related Information 

Refer to MCAI EASA Airworthiness 

Directive 2012–0045, dated March 21, 2012, 

and Airbus Military All Operator Letter 235– 

020, dated March 9, 2012, for related 

information. 

(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 the AD specifies otherwise. 

(i) Airbus Military All Operator Letter 235– 

020, dated March 9, 2012. 

(ii) Reserved. 

(3) For service information identified in 

this AD, contact EADS–CASA, Military 

Transport Aircraft Division (MTAD), 

Integrated Customer Services (ICS), 

Technical Services, Avenida de Arago ́n 404, 

28022 Madrid, Spain; telephone +34 91 585 

55 84; fax +34 91 585 55 05; email 

MTA.TechnicalService@casa.eads.net; 

Internet http://www.eads.net. 

(4) You may review copies of the 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 January 

23, 2013. 

Ali Bahrami, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2013–02074 Filed 1–31–13; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF THE TREASURY 

Internal Revenue Service 

26 CFR Part 1 

[TD 9611] 

RIN 1545–BL49 

Health Insurance Premium Tax Credit 

AGENCY: Internal Revenue Service (IRS), 

Treasury. 

ACTION: Final regulations. 

SUMMARY: This document contains final 

regulations relating to the health 

insurance premium tax credit enacted 

by the Patient Protection and Affordable 

Care Act and the Health Care and 

Education Reconciliation Act of 2010. 

These final regulations provide 

guidance to individuals related to 

employees who may enroll in eligible 

employer-sponsored coverage and who 

wish to enroll in qualified health plans 

through Affordable Insurance Exchanges 

(Exchanges) and claim the premium tax 

credit. 

DATES: Effective date: These regulations 

are effective on February 1, 2013. 

Applicability date: For date of 

applicability, see § 1.36B–1(o). 

FOR FURTHER INFORMATION CONTACT: 

Andrew S. Braden, (202) 622–4960 (not 

a toll-free number). 

SUPPLEMENTARY INFORMATION: 

Background 

This document contains final 

regulations that amend the Income Tax 

Regulations (26 CFR part 1) under 

section 36B of the Internal Revenue 

Code (Code) regarding whether health 

coverage under an employer-sponsored 

plan is affordable for individuals who 

are eligible to enroll in the plan by 

reason of their relationship to an 

employee (related individuals). 

On August 17, 2011, a notice of 

proposed rulemaking (REG–131491–10) 

was published in the Federal Register 

(76 FR 50931). On May 23, 2012, final 

regulations (TD 9590) were published in 

the Federal Register (77 FR 30377). The 

final regulations reserved a rule 

(§ 1.36B–2(c)(3)(v)(A)(2)) for 

determining affordability of employersponsored coverage for related 

individuals. Written comments 

responding to the proposed and final 

regulations were received. The 

comments are available for public 

inspection at www.regulations.gov or on 

request. A public hearing was held on 

November 17, 2011. After consideration 

of all the comments, the proposed rule 

is adopted without change by this 

Treasury decision. 


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