72568 Federal Register / Vol. 78, No. 232 / Tuesday, December 3, 2013 / Rules and Regulations 

Costs of Compliance 

We estimate that this AD will affect 

about 59 engines installed on airplanes 

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

will take about eight hours per engine 

to replace the VBV actuator fuel supply 

tube. The cost of this part is about 

$14,310. The average labor rate is $85 

per hour. Based on these figures, we 

estimate the cost of this AD on U.S. 

operators to be $884,410. 

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 

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 

DOT Regulatory Policies and Procedures 

(44 FR 11034, February 26, 1979), 

(3) Will not affect intrastate aviation 

in Alaska to the extent that if 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. 

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): 

2013–23–18 General Electric Company: 

Amendment 39–17673; Docket No. 

FAA–2013–0499; Directorate Identifier 

2013–NE–20–AD. 

(a) Effective Date 

This AD is effective January 7, 2014. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to General Electric 

Company (GE) GE90–110B1 and –115B 

turbofan engines with variable bypass valve 

(VBV) actuator fuel supply tube, part number 

(P/N) 2165M22P01, installed. 

(d) Unsafe Condition 

This AD was prompted by multiple events 

of a leaking VBV actuator fuel supply tube. 

We are issuing this AD to prevent failure of 

the affected fuel supply tube, fuel leakage, 

engine fire, and damage to the airplane. 

(e) Compliance 

(1) Comply with this AD within the 

compliance times specified, unless already 

done. 

(2) At the next shop visit, after the effective 

date of this AD, replace the VBV actuator fuel 

supply tube, P/N 2165M22P01, with a part 

eligible for installation. 

(f) Definition 

For the purpose of this AD, a shop visit is 

the induction of an engine into the shop for 

maintenance or overhaul. The separation of 

engine flanges solely for the purposes of 

transporting the engine without subsequent 

engine maintenance does not constitute an 

engine shop visit. 

(g) Installation Prohibition 

After the effective date of this AD, do not 

install any VBV actuator fuel supply tube, 

P/N 2165M22P01, onto any engine. 

(h) Alternative Methods of Compliance 

(AMOCs) 

The Manager, Engine Certification Office, 

FAA, may approve AMOCs for this AD. Use 

the procedures in 14 CFR 39.19 to make your 

request. 

(i) Related Information 

For more information about this AD, 

contact Jason Yang, Aerospace Engineer, 

Engine Certification Office, FAA, 12 New 

England Executive Park, Burlington, MA 

01803; phone: 781–238–7747; fax: 781–238– 

7199; email: jason.yang@faa.gov. 

(j) Material Incorporated by Reference 

None. 

Issued in Burlington, Massachusetts, on 

November 14, 2013. 

Frank P. Paskiewicz, 

Acting Director, Aircraft Certification Service. 

[FR Doc. 2013–28866 Filed 12–2–13; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2013–0812; Directorate 

Identifier 2013–CE–023–AD; Amendment 

39–17689; AD 2013–24–14] 

RIN 2120–AA64 

Airworthiness Directives; Diamond 

Aircraft Industries GmbH Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for 

Diamond Aircraft Industries GmbH 

Models DA40 and DA40F airplanes. 

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 fatigue strength 

found in the aft main spar does not 

ensure unlimited lifetime structural 

integrity. We are issuing this AD to 

require actions to address the unsafe 

condition on these products. 

DATES: This AD is effective January 7, 

2014. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in the AD 

as of January 7, 2014. 

ADDRESSES: You may examine the AD 

docket on the Internet at http://

www.regulations.gov 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 Diamond Aircraft 

Industries GmbH, N.A. Otto-Str.5, A– 

2700 Wiener Neustadt, Austria; 

telephone: +43 2622 26700; fax: +43 


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Federal Register / Vol. 78, No. 232 / Tuesday, December 3, 2013 / Rules and Regulations 72569 

2622 26780; email: office@diamondair.at; Internet: http://

www.diamondaircraft.com/contact/

technical.php. You may review copies 

of the 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: 

Mike Kiesov, Aerospace Engineer, FAA, 

Small Airplane Directorate, 901 Locust, 

Room 301, Kansas City, Missouri 64106; 

telephone: (816) 329–4144; fax: (816) 

329–4090; email: mike.kiesov@faa.gov. 

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 September 17, 2013 (78 FR 

57104). That NPRM proposed to correct 

an unsafe condition for the specified 

products. The MCAI states: 

Structural fatigue testing of the DA 40 

aeroplane carried out for an extension of the 

Major Structural Inspection (MSI) interval 

has shown that the fatigue strength of the aft 

main spar in the cabin area does not ensure 

unlimited lifetime. 

This condition, if not corrected, could 

adversely affect the structural integrity of the 

aeroplane. 

Diamond Aircraft Industries (DAI) issued 

Mandatory Service Bulletin (MSB) 40–074/

MSB D4–094/MSB F4–028, including Work 

Instruction (WI) WI–MSB 40–074/WI–MSB 

D4–094/WI–MSB F4–028 (published as a 

single document), providing instructions to 

reinforce the aft main spar in the cabin area. 

For the reasons described above, this AD 

requires modification of the aft main spar in 

the cabin area. 

Note: Aeroplanes with modified aft main 

spar are eligible for an increased MSI 

threshold of 6000 flight hours (FH) since first 

flight of the aeroplane and increased MSI 

intervals not to exceed 4000 FH thereafter. 

The MCAI can be found in the AD 

docket on the Internet at: http://

www.regulations.gov/

#!documentDetail;D=FAA-2013-0812- 

0002. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

received no comments on the NPRM (78 

FR 57104, September 17, 2013) 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. We have determined that 

these minor changes: 

• Are consistent with the intent that 

was proposed in the NPRM (78 FR 

57104, September 17, 2013)) for 

correcting the unsafe condition; and 

• Do not add any additional burden 

upon the public than was already 

proposed in the NPRM (78 FR 57104, 

September 17, 2013). 

Costs of Compliance 

We estimate that this AD will affect 

747 products of U.S. registry. We also 

estimate that it would take about 6 

work-hours per product to comply with 

the basic requirements of this AD. The 

average labor rate is $85 per work-hour. 

Required parts would cost about $100 

per product. 

Based on these figures, we estimate 

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

be $455,670, or $610 per product. 

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; 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: 

2013–24–14 Diamond Aircraft Industries 

GmbH: Amendment 39–17689; Docket 

No. FAA–2013–0812; Directorate 

Identifier 2013–CE–023–AD. 

(a) Effective Date 

This airworthiness directive (AD) becomes 

effective January 7, 2014. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to Diamond Aircraft 

Industries Model DA 40 airplanes, serial 

numbers 40.006 through 40.009, 40.011 

through 40.1071, and 40.1073 through 

40.1077; and Model DA 40 F airplanes, serial 

numbers 40.FC001 through 40.FC029; 

certificated in any category. 

(d) Subject 

Air Transport Association of America 

(ATA) Code 57: Wings. 

(e) Reason 

This AD was prompted from 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 


emcdonald on DSK67QTVN1PROD with RULES
72570 Federal Register / Vol. 78, No. 232 / Tuesday, December 3, 2013 / Rules and Regulations 

describes the unsafe condition as fatigue 

strength found in the aft main spar does not 

ensure unlimited lifetime structural integrity. 

We are issuing this AD to modify the aft main 

spar in the cabin area to ensure the structural 

integrity of the airplane. 

(f) Actions and Compliance 

Unless already done, at or before the next 

Major Structural Inspection (MSI) after the 

effective date of this AD or within the next 

114 months after January 7, 2014 (the 

effective date of this AD), whichever occurs 

first, modify the aft main spar in the cabin 

area following the INSTRUCTIONS section of 

Diamond Aircraft Industries GmbH Work 

Instructions WI–MSB 40–074, WI–MSB D4– 

094, and WI–MSB F4–028 (co-published as a 

single document), dated May 10, 2013, as 

specified in Diamond Aircraft Industries 

GmbH Mandatory Service Bulletins (MSB) 

40–074, D4–094, and F4–028 (co-published 

as a single document), dated May 10, 2013. 

(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: Mike Kiesov, Aerospace Engineer, 

FAA, Small Airplane Directorate, 901 Locust, 

Room 301, Kansas City, Missouri 64106; 

telephone: (816) 329–4144; fax: (816) 329– 

4090; email: mike.kiesov@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. 

(h) Related Information 

Refer to MCAI European Aviation Safety 

Agency (EASA), which is the Technical 

Agent for the Member States of the European 

Community, EASA AD No.: 2013–0145, 

dated July 15, 2013, for more information. 

You may examine the AD on the Internet at 

http://www.regulations.gov by searching and 

locating it in Docket No. FAA–2013–0812. 

(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) Diamond Aircraft Industries GmbH 

Mandatory Service Bulletin 40–074, dated 

May 10, 2013. 

(ii) Diamond Aircraft Industries GmbH 

Mandatory Service Bulletin D4–094, dated 

May 10, 2013. 

(iii) Diamond Aircraft Industries GmbH 

Mandatory Service Bulletin F4–028, dated 

May 10, 2013. 

Note 1 to paragraphs (i)(2)(i) through 

(i)(2)(iii) of this AD: Diamond Aircraft 

Industries GmbH Mandatory Service Bulletin 

40–074, dated May 10, 2013; Diamond 

Aircraft Industries GmbH Mandatory Service 

Bulletin D4–094, dated May 10, 2013; 

Diamond Aircraft Industries GmbH 

Mandatory Service Bulletin F4–028, dated 

May 10, 2013; are co-published as one 

document. 

(iv) Diamond Aircraft Industries GmbH 

Work Instruction WI–MSB 40–074, dated 

May 10, 2013. 

(v) Diamond Aircraft Industries GmbH 

Work Instruction WI–MSB D4–094, dated 

May 10, 2013. 

(vi) Diamond Aircraft Industries GmbH 

Work Instruction WI–MSB F4–028, dated 

May 10, 2013. 

Note 2 to paragraphs (i)(2)(iv) through 

(i)(2)(vi) of this AD: Diamond Aircraft 

Industries GmbH Work Instruction WI–MSB 

40–074; Diamond Aircraft Industries GmbH 

Work Instruction WI–MSB F4–028; dated 

May 10, 2013; and Diamond Aircraft 

Industries GmbH Work Instruction WI–MSB 

F4–028 dated May 10, 2013; are co-published 

as one document. 

(3) For Diamond Aircraft Industries service 

information identified in this AD, contact 

Diamond Aircraft Industries GmbH, N.A. 

Otto-Str.5, A–2700 Wiener Neustadt, Austria; 

telephone: +43 2622 26700; fax: +43 2622 

26780; email: office@diamond-air.at; 

Internet: http://www.diamondaircraft.com/

contact/technical.php. 

(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 

November 22, 2013. 

Earl Lawrence, 

Manager, Small Airplane Directorate, Aircraft 

Certification Service. 

[FR Doc. 2013–28746 Filed 12–2–13; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF COMMERCE 

International Trade Administration 

15 CFR Parts 301, 303 

RIN 0625–AB00 

[Docket No.: 131114957–3957–01] 

Import Administration; Change of 

Agency Name for Instruments and 

Apparatus for Educational and 

Scientific Institutions 

AGENCY: Import Administration, 

Commerce. 

ACTION: Final rule; Nomenclature 

change. 

SUMMARY: Effective October 1, 2013, the 

Department of Commerce (Department), 

through internal department 

organizational orders, changed the name 

of ‘‘Import Administration’’ to 

‘‘Enforcement and Compliance.’’ The 

rule also sets forth a Savings Provision 

that preserves, under the new name, all 

actions taken under the name of Import 

Administration and provides that any 

references to Import Administration in 

any document or other communication 

shall be deemed to be references to 

Enforcement and Compliance. 

DATES: This rule is effective December 2, 

2013. 

FOR FURTHER INFORMATION CONTACT: 

Robert Goodyear, Director, Office of 

Operations Support Enforcement & 

Compliance, Telephone: (202) 482– 

5194; Michele D. Lynch, Senior 

Counsel, Office of Chief Counsel for 

Trade Enforcement and Compliance, 

Telephone: (202) 482–2879. 

SUPPLEMENTARY INFORMATION: 

Background 

This rule implements the decision by 

the Department, through internal 

Department Organizational Orders 10–3 

(effective September 18, 2013) and 

Department Organizational Order 40–1, 

(effective September 19, 2013), to 

consolidate and reorganize certain 

department organizational functions 

and revise the name of ‘‘Import 

Administration’’ to ‘‘Enforcement and 

Compliance.’’ The revision more 

accurately reflects the breadth of the 

agency’s activities with respect to the 

enforcement of, and compliance with, 

U.S. trade laws and agreements. 

Consistent with the consolidation and 

name change, this rule makes certain 

changes in parts 301 and 303 of title 15 

of the Code of Federal Regulations. 

Specifically, this rule changes all 

references to ‘‘Import Administration’’ 

wherever they appear in parts 301 and 


emcdonald on DSK67QTVN1PROD with RULES