Federal Register / Vol. 79, No. 77 / Tuesday, April 22, 2014 / Rules and Regulations 22369 

3200 Corrosion Prevention and Control 

Programme, Manual Ref. JS/CPCP/01, 

Revision 6, dated November 15, 2010. 

(3) If any discrepancy, particularly 

corrosion, is found during any inspections or 

tasks required by paragraphs (f)(1) and (f)(2) 

of this AD, within the compliance time 

specified, repair or replace, as applicable, all 

damaged structural parts and components 

and do the maintenance procedures for 

corrective action following BAE Systems 

(Operations) Limited Jetstream Series 3100 & 

3200 Corrosion Prevention and Control 

Programme, Manual Ref. JS/CPCP/01, 

Revision 6, dated November 15, 2010. If no 

compliance time is defined, do the applicable 

corrective action before further flight. 

(4) You may comply with the requirements 

of paragraphs (f)(1) and (f)(2) of this AD by 

incorporating BAE Systems (Operations) 

Limited Jetstream Series 3100 & 3200 

Corrosion Prevention and Control 

Programme, Manual Ref. JS/CPCP/01, 

Revision 6, dated November 15, 2010, into 

your maintenance program (instructions for 

continued airworthiness) and complying 

with that program. 

(g) Other FAA AD Provisions 

The following provisions also apply to this 

AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, Standards Office, 

FAA, has the authority to approve AMOCs 

for this AD, if requested using the procedures 

found in 14 CFR 39.19. Send information to 

ATTN: Taylor Martin, Aerospace Engineer, 

FAA, Small Airplane Directorate, 901 Locust, 

Room 301, Kansas City, Missouri 64106; 

telephone: (816) 329–4138; fax: (816) 329– 

4090; email: taylor.martin@faa.gov. Before 

using any approved AMOC on any airplane 

to which the AMOC applies, notify your 

appropriate principal inspector (PI) in the 

FAA Flight Standards District Office (FSDO), 

or lacking a PI, your local FSDO. 

(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. 

(3) Reporting Requirements: For any 

reporting requirement in this AD, a federal 

agency may not conduct or sponsor, and a 

person is not required to respond to, nor 

shall a person be subject to a penalty for 

failure to comply with a collection of 

information subject to the requirements of 

the Paperwork Reduction Act unless that 

collection of information displays a current 

valid OMB Control Number. The OMB 

Control Number for this information 

collection is 2120–0056. Public reporting for 

this collection of information is estimated to 

be approximately 5 minutes per response, 

including the time for reviewing instructions, 

completing and reviewing the collection of 

information. All responses to this collection 

of information are mandatory. Comments 

concerning the accuracy of this burden and 

suggestions for reducing the burden should 

be directed to the FAA at: 800 Independence 

Ave. SW., Washington, DC 20591, Attn: 

Information Collection Clearance Officer, 

AES–200. 

(h) Related Information 

MCAI European Aviation Safety Agency 

(EASA) AD No.: 2012–0036, dated March 12, 

2012, for related information. The MCAI can 

be found in the AD docket on the Internet at: 

http://www.regulations.gov/

#!documentDetail;D=FAA-2014-0042-0002. 

(i) 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) BAE Systems (Operations) Limited 

Jetstream Series 3100 & 3200 Corrosion 

Prevention and Control Programme, Manual 

Ref: JS/CPCP/01, Revision 6, dated November 

15, 2010. 

(ii) Reserved. 

(3) For British Aerospace Regional Aircraft 

service information identified in this AD, 

contact BAE Systems (Operations) Limited, 

Customer Information Department, Prestwick 

International Airport, Ayrshire, KA9 2RW, 

Scotland, United Kingdom; telephone: +44 

1292 675207; fax: +44 1292 675704; email: 

RApublications@baesystems.com; Internet: 

http://www.baesystems.com/Businesses/

RegionalAircraft/. 

(4) You may view this service information 

at the FAA, Small Airplane Directorate, 901 

Locust, Kansas City, Missouri 64106. For 

information on the availability of this 

material at the FAA, call (816) 329–4148. 

(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 Kansas City, Missouri, on April 

4, 2014. 

Earl Lawrence, 

Manager, Small Airplane Directorate, Aircraft 

Certification Service. 

[FR Doc. 2014–08142 Filed 4–21–14; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2014–0018; Directorate 

Identifier 2013–CE–049–AD; Amendment 

39–17822; AD 2014–07–08] 

RIN 2120–AA64 

Airworthiness Directives; Centrair 

Gliders 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for Centrair 

Model 101, 101A, 101AP, and 101P 

gliders. This AD results from mandatory 

continuing airworthiness information 

(MCAI) issued by an aviation authority 

of another country to identify and 

correct an unsafe condition on an 

aviation product. The MCAI describes 

the unsafe condition as structural 

damage to the fuselage. We are issuing 

this AD to require actions to address the 

unsafe condition on these products. 

DATES: This AD is effective May 27, 

2014. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in the AD 

as of May 27, 2014. 

ADDRESSES: You may examine the AD 

docket on the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2014– 

0018; or in person at Document 

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 20590. 

For service information identified in 

this AD, contact Socie ́te ́ Nouvelle 

CENTRAIR, Aerodrome B.P. 44, F36300 LeBlanc, France; telephone: 

+33(0)254370796, fax: +33(0)254374864, 

email: contact@sncentrair.com; Internet: 

none. You may view this referenced 

service information at the FAA, Small 

Airplane Directorate, 901 Locust, 

Kansas City, Missouri 64106. For 

information on the availability of this 

material at the FAA, call (816) 329– 

4148. 

FOR FURTHER INFORMATION CONTACT: Jim 

Rutherford, Aerospace Engineer, FAA, 

Small Airplane Directorate, 901 Locust, 

Room 301, Kansas City, Missouri 64106; 

telephone: (816) 329–4165; fax: (816) 

329–4090; email: jim.rutherford@

faa.gov. 

SUPPLEMENTARY INFORMATION: 


ehiers on DSK2VPTVN1PROD with RULES
22370 Federal Register / Vol. 79, No. 77 / Tuesday, April 22, 2014 / Rules and Regulations 

Discussion 

We issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 by adding an AD that would 

apply to Centrair Model 101, 101A, 

101AP, and 101P airplanes. The NPRM 

was published in the Federal Register 

on January 15, 2014 (79 FR 2593). The 

NPRM proposed to correct an unsafe 

condition for the specified products and 

was based on mandatory continuing 

airworthiness information (MCAI) 

originated by an aviation authority of 

another country. The MCAI states: 

Occurrences of structural damage were 

reported on several Centrair 101 sailplane 

fuselage. The results of the subsequent 

investigations identified that these findings 

were accidental damage related and not 

identified in time during routine 

maintenance, due to inadequate maintenance 

instructions. 

This condition, if not detected and 

corrected, could reduce the structural 

integrity of the sailplane. 

To address this potential unsafe condition, 

Socie ́te ́ Nouvelle (SN) Centrair issued Service 

Bulletin (SB) 101–06 to provide instructions 

for structural inspections and Direction 

Ge ́ne ́rale de l’Aviation Civile (DGAC) of 

France issued AD 85–21–(A) to mandate the 

fuselage inspections described in that SB. 

Since that AD was issued, SN Centrair 

issued SB 101–06 at revision (rev.) 1 to 

provide improved instructions to identify 

accidental structural damages. 

For the reasons described above, this AD 

retains the requirements of DGAC France AD 

85–21–(A), which is superseded, but requires 

accomplishment of those fuselage structural 

inspections in accordance with improved 

instructions. 

The MCAI can be found in the AD 

docket on the Internet at: http://

www.regulations.gov/

#!documentDetail;D=FAA-2014-0018- 

0002. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

received no comments on the NPRM (79 

FR 2593, January 15, 2014) or on the 

determination of the cost to the public. 

Conclusion 

We reviewed the relevant data and 

determined that air safety and the 

public interest require adopting the AD 

as proposed 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 2593, 

January 15, 2014) for correcting the 

unsafe condition; and 

• Do not add any additional burden 

upon the public than was already 

proposed in the NPRM. 

Costs of Compliance 

We estimate that this AD will affect 

43 products of U.S. registry. We also 

estimate that it would take about 3 

work-hours 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 on U.S. operators to 

be $10,965, or $255 per product. 

Since there are currently no repair 

instructions available if discrepancies 

are found during the required 

inspections, we have no way of 

determining the number of products 

that may need follow-on actions or what 

the cost per product would be. 

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, 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 by searching for 

and locating Docket No. FAA–2014– 

0018; 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 the NPRM, the regulatory 

evaluation, any comments received, and 

other information. The street address for 

the Docket 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: 

2014–07–08 Centrair: Amendment 39– 

17822; Docket No. FAA–2014–0018; 

Directorate Identifier 2013–CE–049–AD. 

(a) Effective Date 

This airworthiness directive (AD) becomes 

effective May 27, 2014. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to CENTRAIR Models 101, 

101A, 101P, and 101AP gliders, all serial 

numbers, certificated in any category. 

(d) Subject 

Air Transport Association of America 

(ATA) Code 53: Fuselage. 

(e) Reason 

This AD was prompted by mandatory 

continuing airworthiness information (MCAI) 

originated by an aviation authority of another 

country to identify and correct an unsafe 

condition on an aviation product. The MCAI 

describes the unsafe condition as structural 

damage to the fuselage. We are issuing this 

AD to detect and correct structural damage 

not identified during routine maintenance 

inspections, which could lead to reduced 

structural integrity of the glider. 


ehiers on DSK2VPTVN1PROD with RULES
Federal Register / Vol. 79, No. 77 / Tuesday, April 22, 2014 / Rules and Regulations 22371 

1Non-Application of Previously Withdrawn 

Regulatory Provisions Governing Targeted Dumping 

Continued 

(f) Actions and Compliance 

Unless already done, do the following 

actions in paragraphs (f)(1) through (f)(3) of 

this AD: 

(1) Within 25 days after May 27, 2014 (the 

effective date of this AD) and repetitively 

thereafter at intervals not to exceed every 12 

months, inspect all fuselage frames and ribs 

following the instructions in Socie ́te ́

Nouvelle CENTRAIR Mandatory Service 

Bulletin 101–06, Revision 1, dated August 5, 

2013. 

(2) If structural damage is detected during 

any inspection required by paragraph (f)(1) of 

this AD, before further flight, contact Socie ́te ́

Nouvelle CENTRAIR at the address specified 

in paragraph (i) of this AD to obtain FAAapproved repair instructions approved 

specifically for this AD, and before further 

flight, repair the glider using these repair 

instructions. 

(3) Accomplishment of a repair, as required 

by paragraph (f)(2) of this AD, does not 

constitute terminating action for the 

inspection required by paragraph (f)(1) of this 

AD. 

Note 1 to paragraph (f) of this AD: We 

recommend that you also inspect the fuselage 

frames and ribs after the occurrence of any 

of the following events following the 

instructions in Socie ́te ́ Nouvelle CENTRAIR 

Mandatory Service Bulletin 101–06, Revision 

1, dated August 5, 2013: Landing with 

retracted gear, landing gear retraction during 

landing run, ground looping during take-off 

or landing, hard landing, or damage of 

internal structure of the fuselage. If structural 

damage is detected during any of these 

inspections, we recommend you contact 

Socie ́te ́ Nouvelle CENTRAIR at the address 

specified in paragraph (i) of this AD for FAAapproved repair instructions. 

(g) Other FAA AD Provisions 

The following provisions also apply to this 

AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, Standards Office, 

FAA, has the authority to approve AMOCs 

for this AD, if requested using the procedures 

found in 14 CFR 39.19. Send information to 

ATTN: Jim Rutherford, Aerospace Engineer, 

FAA, Small Airplane Directorate, 901 Locust, 

Room 301, Kansas City, Missouri 64106; 

telephone: (816) 329–4165; fax: (816) 329– 

4090; email: jim.rutherford@faa.gov. Before 

using any approved AMOC on any airplane 

to which the AMOC applies, notify your 

appropriate principal inspector (PI) in the 

FAA Flight Standards District Office (FSDO), 

or lacking a PI, your local FSDO. 

(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. 

(3) Reporting Requirements: For any 

reporting requirement in this AD, a federal 

agency may not conduct or sponsor, and a 

person is not required to respond to, nor 

shall a person be subject to a penalty for 

failure to comply with a collection of 

information subject to the requirements of 

the Paperwork Reduction Act unless that 

collection of information displays a current 

valid OMB Control Number. The OMB 

Control Number for this information 

collection is 2120–0056. Public reporting for 

this collection of information is estimated to 

be approximately 5 minutes per response, 

including the time for reviewing instructions, 

completing and reviewing the collection of 

information. All responses to this collection 

of information are mandatory. Comments 

concerning the accuracy of this burden and 

suggestions for reducing the burden should 

be directed to the FAA at: 800 Independence 

Ave. SW., Washington, DC 20591, Attn: 

Information Collection Clearance Officer, 

AES–200. 

(h) Related Information 

Refer to MCAI European Aviation Safety 

Agency (EASA) AD No.: 2013–0258, dated 

October 25, 2013, for related information. 

The MCAI can be found in the AD docket on 

the Internet at: http://www.regulations.gov/

#!documentDetail;D=FAA-2014-0018-0002. 

(i) 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) Socie ́te ́ Nouvelle CENTRAIR Mandatory 

Service Bulletin 101–06, Revision 1, dated 

August 5, 2013. 

(ii) Reserved. 

(3) For Centrair Gliders service information 

identified in this AD, contact Socie ́te ́

Nouvelle CENTRAIR, Aerodrome B.P. 44, F– 

36300 LeBlanc, France; telephone: 

+33(0)254370796, fax: +33(0)254374864, 

email: contact@sncentrair.com; Internet: 

none. 

(4) You may view this service information 

at the FAA, Small Airplane Directorate, 901 

Locust, Kansas City, Missouri 64106. For 

information on the availability of this 

material at the FAA, call (816) 329–4148. 

(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 Kansas City, Missouri, on April 

4, 2014. 

Earl Lawrence, 

Manager, Small Airplane Directorate, Aircraft 

Certification Service. 

[FR Doc. 2014–08074 Filed 4–21–14; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF COMMERCE 

International Trade Administration 

19 CFR Part 351 

[Docket No. 130917809–4303–02] 

RIN 0625–AA96 

Non-Application of Previously 

Withdrawn Regulatory Provisions 

Governing Targeted Dumping in 

Antidumping Duty Investigations 

AGENCY: Enforcement and Compliance, 

International Trade Administration, 

Department of Commerce. 

ACTION: Final rule. 

SUMMARY: Enforcement and Compliance 

(formerly Import Administration), 

International Trade Administration, 

Department of Commerce (the 

Department), hereby publishes this 

Final Rule not to apply the previously 

withdrawn regulatory provisions 

governing targeted dumping in lessthan-fair-value investigations. Following 

the Court of International Trade’s 

decision in Gold East (Jiangsu) Paper 

Co. v. United States, 918 F. Supp. 2d 

1317 (Ct. Int’l Trade 2013), the 

Department sought clarification of the 

status of the previously withdrawn 

targeted dumping regulations and input 

on whether to reinstate the regulations 

or to continue to treat them as 

withdrawn. The Department has 

considered the comments received and, 

as explained below, determines to 

continue not to apply the withdrawn 

targeted dumping regulations in lessthan-fair-value investigations. Rather, 

the Department will continue to 

determine whether to apply an 

alternative comparison method as 

appropriate based upon the particular 

facts in each case. 

DATES: This Final Rule is effective May 

22, 2014, and will apply to all less-thanfair-value investigations initiated on or 

after May 22, 2014. 

FOR FURTHER INFORMATION CONTACT: 

James Maeder (202) 482–3330; Charles 

Vannatta (202) 482–4036; or Melissa 

Brewer (202) 482–1096. 

SUPPLEMENTARY INFORMATION: 

Background 

On October 1, 2013, the Department 

published its proposed rulemaking and 

request for comments regarding the 

Department’s proposal not to apply the 

previously withdrawn regulatory 

provisions governing targeted dumping 

in less-than-fair-value investigations.1 In 


ehiers on DSK2VPTVN1PROD with RULES