1774 Federal Register / Vol. 79, No. 7 / Friday, January 10, 2014 / Proposed Rules 

FIGURE 1 TO PARAGRAPH (G) OF THIS AD: ENGINE SHUT-OFF VALVE (FUEL SPAR VALVE) MOV ACTUATOR

INSPECTION—Continued 

AWL No. Task Interval Applicability Description 

1. Make sure both Engine Control Switches 

are in the CUTOFF position. 

2. Inspect the left engine fuel spar valve actuator located in the left rear spar. 

a. Verify the manual override handle on the 

engine fuel spar valve actuator is in the 

CLOSED position. 

b. Repair or replace any MOV actuator that 

is not in the CLOSED position (refer to 

Boeing Airplane Maintenance Manual, 28– 

22–02). 

3. Inspect the right engine fuel spar valve 

actuator located in the right rear spar. 

a. Verify the manual override handle on the 

engine fuel spar valve actuator is in the 

CLOSED position. 

b. Repair or replace any MOV actuator that 

is not in the CLOSED position (refer to 

Boeing Airplane Maintenance Manual, 28– 

22–02). 

(h) No Alternative Actions and Intervals 

After accomplishment of the maintenance 

or inspection program revision required by 

paragraph (g) of this AD, no alternative 

actions (e.g., inspections) or intervals may be 

used unless the actions or intervals are 

approved as an alternative method of 

compliance (AMOC) in accordance with the 

procedures specified in paragraph (i)(1) of 

this AD. 

(i) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, Seattle Aircraft 

Certification Office (ACO) 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 manager of the ACO, send it to the 

attention of the person identified in 

paragraph (j) of this AD. Information may be 

emailed to: 9-ANM-Seattle-ACO-AMOCRequests@faa.gov. 

(2) 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. 

(j) Related Information 

For more information about this AD, 

contact Rebel Nichols, Aerospace Engineer, 

Propulsion Branch, ANM–140S, FAA, Seattle 

Aircraft Certification Office, 1601 Lind 

Avenue SW., Renton, WA 98057–3356; 

phone: (425) 917–6509; fax: (425) 917–6590; 

email: rebel.nichols@faa.gov. 

Issued in Renton, Washington, on 

December 30, 2013. 

John P. Piccola, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2014–00234 Filed 1–9–14; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2008–1088; Directorate 

Identifier 2008–NE–15–AD] 

RIN 2120–AA64 

Airworthiness Directives; Dowty 

Propellers Propellers 

Correction 

In proposed rule document 2013– 

30882, appearing on pages 78290– 

78292, in the issue of Thursday, 

December 26, 2013, make the following 

correction: 

On page 78290, in the first column, 

the subject heading is corrected to read 

as set forth above. 

[FR Doc. C1–2013–30882 Filed 1–9–14; 8:45 am] 

BILLING CODE 1505–01–D 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2013–0164; Directorate 

Identifier 2013–NE–10–AD] 

RIN 2120–AA64 

Airworthiness Directives; Austro 

Engine GmbH Engines 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: We propose to supersede 

airworthiness directive (AD) 2013–14– 

08 that applies to all Austro Engine 

GmbH model E4 engines. AD 2013–14– 

08 requires removing from service 

certain part number (P/N) waste gate 

controllers. Since we issued AD 2013– 

14–08 we received several reports of 

power loss events due to fracture of the 

waste gate controller lever. This 

proposed AD would require removing 

certain P/N waste gate controllers from 

service. We are proposing this AD to 

prevent failure of the waste gate 

controller lever, which could lead to 

damage to one or more engines, loss of 

thrust control, and damage to the 

airplane. 

DATES: We must receive comments on 

this proposed AD by March 11, 2014. 

ADDRESSES: You may send comments, 

using the procedures found in 14 CFR 

11.43 and 11.45, by any of the following 

methods: 

• Federal eRulemaking Portal: Go to 

http://www.regulations.gov. Follow the 

instructions for submitting comments. 

• Fax: 202–493–2251. 

• Mail: U.S. Department of 

Transportation, Docket Operations, M– 

30, West Building Ground Floor, Room 

W12–140, 1200 New Jersey Avenue SE., 

Washington, DC 20590. 

• Hand Delivery: Deliver to Mail 

address above between 9 a.m. and 5 

p.m., Monday through Friday, except 

Federal holidays. 

For service information identified in 

this AD, contact Austro Engine GmbH, 

Rudolf-Diesel-Strasse 11, A–2700 

Weiner Neustadt, Austria; phone: +43 

2622 23000; fax: +43 2622 23000–2711; 

Internet: www.austroengine.at. You may 

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Federal Register / Vol. 79, No. 7 / Friday, January 10, 2014 / Proposed Rules 1775 

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. 

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– 

0164; 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 proposed AD, the 

mandatory continuing airworthiness 

information, the regulatory evaluation, 

any comments received, and other 

information. The street address for the 

Docket Office (phone: 800–647–5527) is 

in the ADDRESSES section. Comments 

will be available in the AD docket 

shortly after receipt. 

FOR FURTHER INFORMATION CONTACT: 

Frederick Zink, Aerospace Engineer, 

Engine Certification Office, FAA, Engine 

& Propeller Directorate, 12 New England 

Executive Park, Burlington, MA 01803; 

phone: 781–238–7779; fax: 781–238– 

7199; email: frederick.zink@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Comments Invited 

We invite you to send any written 

relevant data, views, or arguments about 

this proposed AD. Send your comments 

to an address listed under the 

ADDRESSES section. Include ‘‘Docket No. 

FAA–2013–0164; Directorate Identifier 

2013–NE–10–AD’’ at the beginning of 

your comments. We specifically invite 

comments on the overall regulatory, 

economic, environmental, and energy 

aspects of this proposed AD. We will 

consider all comments received by the 

closing date and may amend this 

proposed AD because of those 

comments. 

We will post all comments we 

receive, without change, to http://

www.regulations.gov, including any 

personal information you provide. We 

will also post a report summarizing each 

substantive verbal contact we receive 

about this proposed AD. 

Discussion 

On July 10, 2013, we issued AD 2013– 

14–08, Amendment 39–17513 (78 FR 

42677, July 17, 2013), (‘‘AD 2013–14– 

08’’), for all Austro Engine GmbH model 

E4 engines. AD 2013–14–08 requires 

removing from service certain P/N waste 

gate controllers. AD 2013–14–08 

resulted from several reports of power 

loss events due to fracture of the waste 

gate controller lever. We issued AD 

2013–14–08 to prevent failure of the 

waste gate controller lever, which could 

lead to damage to one or more engines, 

loss of thrust control, and damage to the 

airplane. 

Actions Since AD 2013–14–08 Was 

Issued 

Since we issued AD 2013–14–08, we 

received notification of additional waste 

gate controller P/Ns that require 

removal from service. Also since we 

issued AD 2013–14–08, the European 

Aviation Safety Agency (EASA) has 

issued AD 2013–0213, dated September 

13, 2013, which requires removal and 

replacement of affected waste gate 

controllers. We also changed the unsafe 

condition statement in AD 2013–14–08 

to clarify the relationship between the 

unsafe condition and the engine. 

Relevant Service Information 

We reviewed Austro Engine 

Mandatory Service Bulletin (MSB) No. 

MSB–E4–007/6, Revision 6, dated 

September 18, 2013. The service 

information describes procedures for 

removal and installation of the waste 

gate controllers. 

FAA’s Determination 

We are proposing this AD because we 

evaluated all the relevant information 

and determined the unsafe condition 

described previously is likely to exist or 

develop in other products of the same 

type design. 

Proposed AD Requirements 

This proposed AD would retain all of 

the requirements of AD 2013–14–08. 

This proposed AD would expand the 

applicability by adding additional P/Ns 

of affected waste gate controllers. 

Costs of Compliance 

We estimate that this proposed AD 

would affect 128 engines installed on 

airplanes of U.S. registry. We also 

estimate that it would take about 0.5 

hours per engine to comply with this 

proposed AD. The average labor rate is 

$85 per hour. Required parts cost about 

$231 per engine. Based on these figures, 

we estimate the total cost of this 

proposed AD to U.S. operators to be 

$35,008. 

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 have determined that this 

proposed AD would not have federalism 

implications under Executive Order 

13132. This proposed AD would 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 the proposed regulation: 

(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. 

List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation 

safety, Incorporation by reference, 

Safety. 

The Proposed Amendment 

Accordingly, under the authority 

delegated to me by the Administrator, 

the FAA proposes to amend 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 

removing airworthiness directive (AD) 

2013–14–08, Amendment 39–17513 (78 

FR 42677, July 17, 2013), and adding the 

following new AD: 

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1776 Federal Register / Vol. 79, No. 7 / Friday, January 10, 2014 / Proposed Rules 

1Because the Secretary of the HHS has delegated 

to the Assistant Secretary for Health of the HHS the 

authority to make domestic drug scheduling 

recommendations, for purposes of this Notice of 

Intent, all subsequent references to ‘‘Secretary’’ 

have been replaced with ‘‘Assistant Secretary.’’ As 

set forth in a memorandum of understanding 

entered into by HHS, the Food and Drug 

Administration (FDA), and the National Institute on 

Drug Abuse (NIDA), FDA acts as the lead agency 

within HHS in carrying out the Assistant 

Secretary’s scheduling responsibilities under the 

CSA, with the concurrence of NIDA. 50 FR 9518, 

Mar. 8, 1985. 

Austro Engine GmbH Engines: Docket No. 

FAA–2013–0164; Directorate Identifier 

2013–NE–10–AD. 

(a) Comments Due Date 

The FAA must receive comments on this 

AD action by March 11, 2014. 

(b) Affected ADs 

This AD supersedes AD 2013–14–08, 

Amendment 39–17513 (78 FR 42677, July 17, 

2013). 

(c) Applicability 

This AD applies to all Austro Engine 

GmbH model E4 engines, with a waste gate 

controller, part number (P/N) E4A–41–120– 

000, Revision 060, or lower revision; or a 

waste gate controller, P/N E4B–41–120–000, 

Revision 010, or lower revision, installed. 

(d) Unsafe Condition 

This AD was prompted by engine power 

loss events due to fracture of the waste gate 

controller lever. We are issuing this AD to 

prevent failure of the waste gate controller 

lever, which could lead to damage to one or 

more engines, loss of thrust control, and 

damage to the airplane. 

(e) Compliance 

(1) Comply with this AD within the 

compliance times specified, unless already 

done. 

(2) At the next maintenance action for any 

reason, or within 110 flight hours after the 

effective date of this AD, or within three 

months after the effective date of this AD, 

whichever occurs first, remove from service 

waste gate controller, P/N E4A–41–120–000, 

Revision 060, or lower revision, and waste 

gate controller, P/N E4B–41–120–000, 

Revision 010 or lower revision. 

(f) Installation Prohibition 

After the effective date of this AD, do not 

install any waste gate controller, P/N E4A– 

41–120–000, Revision 060, or lower revision, 

or waste gate controller, P/N E4B–41–120– 

000, Revision 010, or lower revision, onto 

any engine, nor approve for return to service 

any engine that has either waste gate 

controller installed. 

(g) Alternative Methods of Compliance 

(AMOCs) 

The Manager, Engine Certification Office, 

may approve AMOCs for 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 Frederick Zink, Aerospace Engineer, 

Engine Certification Office, FAA, Engine & 

Propeller Directorate, 12 New England 

Executive Park, Burlington, MA 01803; 

phone: 781–238–7779; fax: 781–238–7199; 

email: frederick.zink@faa.gov. 

(2) Refer to MCAI European Aviation 

Safety Agency AD 2013–0213, dated 

September 13, 2013, for more information. 

You may examine the MCAI on the Internet 

at http://www.regulations.gov/

#!documentDetail;D=FAA-2013-0164-0002. 

(3) Austro Engine Mandatory Service 

Bulletin No. MSB–E4–007/6, Revision 6, 

dated September 18, 2013, which is not 

incorporated by reference in this AD, can be 

obtained from Austro Engine GmbH, using 

the contact information in paragraph (h)(4) of 

this AD. 

(4) For service information identified in 

this AD, contact Austro Engine GmbH, 

Rudolf-Diesel-Strasse 11, A–2700 Weiner 

Neustadt, Austria; phone: +43 2622 23000; 

fax: +43 2622 23000–2711; Internet: 

www.austroengine.at. 

(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. 

Issued in Burlington, Massachusetts, on 

December 31, 2013. 

Colleen M. D’Alessandro, 

Assistant Directorate Manager, Engine & 

Propeller Directorate, Aircraft Certification 

Service. 

[FR Doc. 2014–00169 Filed 1–9–14; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF JUSTICE 

Drug Enforcement Administration 

21 CFR Part 1308 

[Docket No. DEA–385] 

Schedules of Controlled Substances: 

Temporary Placement of Four 

Synthetic Cannabinoids Into 

Schedule I 

AGENCY: Drug Enforcement 

Administration, Department of Justice. 

ACTION: Notice of Intent. 

SUMMARY: The Deputy Administrator of 

the Drug Enforcement Administration 

(DEA) is issuing this notice of intent to 

temporarily schedule four synthetic 

cannabinoids into Schedule I pursuant 

to the temporary scheduling provisions 

of the Controlled Substances Act (CSA). 

The substances are: quinolin-8-yl 1- 

pentyl-1H-indole-3-carboxylate (PB–22; 

QUPIC); quinolin-8-yl 1-(5- 

fluoropentyl)-1H-indole-3-carboxylate 

(5-fluoro-PB–22; 5F–PB–22); N-(1- 

amino-3-methyl-1-oxobutan-2-yl)-1-(4- 

fluorobenzyl)-1H-indazole-3- 

carboxamide (AB–FUBINACA); and N- 

(1-amino-3,3-dimethyl-1-oxobutan-2-yl)- 

1-pentyl-1H-indazole-3-carboxamide 

(ADB–PINACA). This action is based on 

a finding by the Deputy Administrator 

that the placement of these synthetic 

cannabinoids into Schedule I of the CSA 

is necessary to avoid an imminent 

hazard to the public safety. Any final 

order will impose the administrative, 

civil, and criminal sanctions and 

regulatory controls applicable to 

Schedule I substances under the CSA on 

the manufacture, distribution, 

possession, importation, exportation, 

research, and conduct of instructional 

activities of these synthetic 

cannabinoids. 

DATES: January 10, 2014. 

FOR FURTHER INFORMATION CONTACT: 

Ruth A. Carter, Acting Chief, Policy 

Evaluation and Analysis Section, Office 

of Diversion Control, Drug Enforcement 

Administration; Mailing Address: 8701 

Morrissette Drive, Springfield, Virginia 

22152, Telephone (202) 598–6812. 

SUPPLEMENTARY INFORMATION: Any final 

order will be published in the Federal 

Register and may not be effective prior 

to February 10, 2014. 

Background 

Section 201 of the CSA, 21 U.S.C. 811, 

provides the Attorney General with the 

authority to temporarily place a 

substance into Schedule I of the CSA for 

two years without regard to the 

requirements of 21 U.S.C. 811(b) if he 

finds that such action is necessary to 

avoid imminent hazard to the public 

safety. 21 U.S.C. 811(h). In addition, if 

proceedings to control a substance are 

initiated under 21 U.S.C. 811(a)(1), the 

Attorney General may extend the 

temporary scheduling for up to one 

year. 21 U.S.C. 811(h)(2). 

Where the necessary findings are 

made, a substance may be temporarily 

scheduled if it is not listed in any other 

schedule under section 202 of the CSA, 

21 U.S.C. 812, or if there is no 

exemption or approval in effect for the 

substance under section 505 of the 

Federal Food, Drug, and Cosmetic Act 

(FDCA), 21 U.S.C. 355. 21 U.S.C. 

811(h)(1); 21 CFR part 1308. The 

Attorney General has delegated his 

authority under 21 U.S.C. 811 to the 

Administrator of the DEA, who in turn 

has delegated her authority to the 

Deputy Administrator of the DEA. 28 

CFR 0.100, 0.104, Appendix to Subpart 

R of Part 0, Sec. 12. 

Section 201(h)(4) of the CSA (21 

U.S.C. 811(h)(4)) requires the Deputy 

Administrator to notify the Secretary of 

the Department of Health and Human 

Services (HHS) of his intention to 

temporarily place a substance into 

Schedule I of the CSA.1 As PB–22, 5F– 

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