Federal Register / Vol. 84, No. 19 / Tuesday, January 29, 2019 / Rules and Regulations 443 

(5) Non-application of no-load mode 

requirements. The no-load mode energy 

efficiency standards established in 

paragraph (w)(1) of this section shall not 

apply to an external power supply 

that— 

* * * * * 

[FR Doc. 2019–00228 Filed 1–28–19; 8:45 am] 

BILLING CODE 6450–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2018–1066; Product 

Identifier 2018–NM–176–AD; Amendment 

39–19540; AD 2019–01–01] 

RIN 2120–AA64 

Airworthiness Directives; The Boeing 

Company Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; correction. 

SUMMARY: The FAA is correcting an 

airworthiness directive (AD) that 

published in the Federal Register. That 

AD applies to The Boeing Company 

Model 787–8 airplanes powered by 

Rolls-Royce plc (RR) Trent 1000–A 

(including –A/01 and –A/01A), Trent 

1000–AE (including –AE/01A), Trent 

1000–C (including –C/01 and –C/01A), 

Trent 1000–CE (including –CE/01A), 

Trent 1000–D (including –D/01 and 

–D/01A), Trent 1000–E (including –E/01 

and –E/01A), Trent 1000–G (including 

–G/01 and –G/01A), and Trent 1000–H 

(including –H/01 and H/01A) turbofan 

engines. As published, a document 

referenced in the regulatory text was 

incorrectly identified. This document 

corrects that error. In all other respects, 

the original document remains the 

same. 

DATES: This correction is effective 

February 4, 2019. 

ADDRESSES: 

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 this AD, the regulatory 

evaluation, any comments received, and 

other information. The address for 

Docket Operations (phone: 800–647– 

5527) is 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 20590. 

FOR FURTHER INFORMATION CONTACT: 

Rebel Nichols, Aerospace Engineer, 

Propulsion Section, FAA, Seattle ACO 

Branch, 2200 South 216th St., Des 

Moines, WA 98198; phone and fax: 206– 

231–3556; email: Rebel.Nichols@

faa.gov. 

SUPPLEMENTARY INFORMATION: As 

published, Airworthiness Directive 

2019–01–01, Amendment 39–19540 (84 

FR 129, January 18, 2019) (‘‘AD 2019– 

01–01’’), requires revising the airplane 

flight manual (AFM) to limit extended 

operations (ETOPS) for The Boeing 

Company Model 787–8 airplanes 

powered by RR Trent 1000–A (including 

–A/01 and –A/01A), Trent 1000–AE 

(including –AE/01A), Trent 1000–C 

(including –C/01 and –C/01A), Trent 

1000–CE (including –CE/01A), Trent 

1000–D (including –D/01 and –D/01A), 

Trent 1000–E (including –E/01 and 

–E/01A), Trent 1000–G (including –G/ 

01 and –G/01A), and Trent 1000–H 

(including –H/01 and H/01A) turbofan 

engines. 

Need for the Correction 

As published, a document specified 

in the regulatory text is incorrect. 

Specifically, a service bulletin that is 

referenced in figure 1 to paragraph (g) of 

AD 2019–01–01 was incorrectly 

identified as Rolls Royce Non 

Modification Service Bulletin Trent 

1000 ‘‘72–AK132.’’ The correct number 

is ‘‘72–K132.’’ Service bulletin ‘‘72– 

AK132’’ does not exist, and therefore, 

operators cannot directly comply with 

the AD requirement that refers to that 

service bulletin. 

Correction of Publication 

The error appeared in figure 1 to 

paragraph (g) of AD 2019–01–01. 

Although no other part of the preamble 

or regulatory information has been 

corrected, we are publishing the entire 

rule in the Federal Register. 

The effective date of this AD remains 

February 4, 2019. 

List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation 

safety, Incorporation by reference, 

Safety. 

Adoption of the Correction 

Accordingly, pursuant to the 

authority delegated to me by the 

Administrator, the Federal Aviation 

Administration amends part 39 of the 

Federal Aviation Regulations (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 [Corrected] 

■ 2. The FAA amends § 39.13 by adding 

the following new airworthiness 

directive (AD): 

2019–01–01 The Boeing Company: 

Amendment 39–19540; Docket No. 

FAA–2018–1066; Product Identifier 

2018–NM–176–AD. 

(a) Effective Date 

This AD is effective February 4, 2019. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to The Boeing Company 

Model 787–8 airplanes, certificated in any 

category, powered by Rolls-Royce plc (RR) 

Trent 1000–A (including –A/01 and –A/01A), 

Trent 1000–AE (including –AE/01A), Trent 

1000–C (including –C/01 and –C/01A), Trent 

1000–CE (including –CE/01A), Trent 1000–D 

(including –D/01 and –D/01A), Trent 1000– 

E (including –E/01 and –E/01A), Trent 1000– 

G (including –G/01 and –G/01A), and Trent 

1000–H (including –H/01 and H/01A) 

turbofan engines. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 71, Power plant. 

(e) Unsafe Condition 

This AD was prompted by a report from 

the engine manufacturer indicating that after 

an engine failure, prolonged operation at 

high thrust settings on the remaining engine 

during an extended-operation (ETOPS) 

diversion may result in failure of the 

remaining engine before the diversion can be 

safely completed. We are issuing this AD to 

address unrecoverable thrust loss on both 

engines, which could lead to a forced 

landing. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Revision of Limitations Chapter in 

Airplane Flight Manual (AFM) 

Within 7 days after the effective date of 

this AD, revise the Certificate Limitations 

chapter of the applicable Boeing AFM Engine 

Appendix by incorporating the information 

in figure 1 to paragraph (g) of this AD. This 

may be accomplished by inserting a copy of 

this AD into the AFM. When information 

identical to that in figure 1 to paragraph (g) 

of this AD has been included in the 

Certificate Limitations chapter of the general 

revisions of the AFM, the general revisions 

may be inserted into the AFM, and the copy 

of this AD may be removed from the AFM. 

Note 1 to paragraph (g) of this AD: The 

Boeing AFM for the aircraft affected by this 

444 Federal Register / Vol. 84, No. 19 / Tuesday, January 29, 2019 / Rules and Regulations 

AD is required to be furnished with the 

aircraft, per 14 CFR 25.1581. Further, 

operators of the aircraft affected by this AD 

must operate in accordance with the 

limitations specified in the AFM, per 14 CFR 

91.9. 

(h) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, Seattle ACO Branch, 

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 

certification office, send it to the attention of 

the person identified in paragraph (i) of this 

AD. Information may be emailed to: 9-ANMSeattle-ACO-AMOC-Requests@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. 

(3) An AMOC that provides an acceptable 

level of safety may be used for any repair, 

modification, or alteration required by this 

AD if it is approved by the Boeing 

Commercial Airplanes Organization 

Designation Authorization (ODA) that has 

been authorized by the Manager, Seattle ACO 

Branch, to make those findings. To be 

approved, the repair method, modification 

deviation, or alteration deviation must meet 

the certification basis of the airplane, and the 

approval must specifically refer to this AD. 

(i) Related Information 

For more information about this AD, 

contact Rebel Nichols, Aerospace Engineer, 

Propulsion Section, FAA, Seattle ACO 

Branch, 2200 South 216th St., Des Moines, 

WA 98198; phone and fax: 206–231–3556; 

email: Rebel.Nichols@faa.gov. 

(j) Material Incorporated by Reference 

None. 

Issued in Des Moines, Washington, on 

January 23, 2019. 

Jeffrey E. Duven, 

Director, System Oversight Division, Aircraft 

Certification Service. 

[FR Doc. 2019–00297 Filed 1–28–19; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF JUSTICE 

Drug Enforcement Administration 

21 CFR Part 1308 

[Docket No. DEA–421] 

Schedules of Controlled Substances: 

Placement of MAB-CHMINACA in 

Schedule I 

AGENCY: Drug Enforcement 

Administration, Department of Justice. 

ACTION: Final rule. 

SUMMARY: The Drug Enforcement 

Administration places N-(1-amino-3,3- 

dimethyl-1-oxobutan-2-yl)-1- 

(cyclohexylmethyl)-1H-indazole-3- 

carboxamide (MAB-CHMINACA; ADBCHMINACA), including its salts, 

isomers, and salts of isomers whenever 

the existence of such salts, isomers, and 

salts of isomers is possible, in schedule 

I of the Controlled Substances Act. This 

action continues the imposition of the 

regulatory controls and administrative, 

civil, and criminal sanctions applicable 

to schedule I controlled substances on 


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