Airworthiness Directives; The Boeing Company Airplanes, 443-444 [2019-00297]

Download as PDF Federal Register / Vol. 84, No. 19 / Tuesday, January 29, 2019 / Rules and Regulations (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 1200 New Jersey Avenue SE, Washington, DC 20590. PART 39—AIRWORTHINESS DIRECTIVES 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. 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. SUPPLEMENTARY INFORMATION: 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 Federal Aviation Administration (FAA), DOT. ACTION: Final rule; correction. AGENCY: 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: SUMMARY: Examining the AD Docket You may examine the AD docket on the internet at https:// 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, VerDate Sep<11>2014 16:37 Jan 28, 2019 Jkt 247001 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: PO 00000 Frm 00007 Fmt 4700 Sfmt 4700 443 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 E:\FR\FM\29JAR1.SGM 29JAR1 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) (i) Related Information DEPARTMENT OF JUSTICE (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. VerDate Sep<11>2014 16:37 Jan 28, 2019 Jkt 247001 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 PO 00000 Frm 00008 Fmt 4700 Sfmt 4700 Drug Enforcement Administration 21 CFR Part 1308 [Docket No. DEA–421] Schedules of Controlled Substances: Placement of MAB-CHMINACA in Schedule I Drug Enforcement Administration, Department of Justice. ACTION: Final rule. AGENCY: The Drug Enforcement Administration places N-(1-amino-3,3dimethyl-1-oxobutan-2-yl)-1(cyclohexylmethyl)-1H-indazole-3carboxamide (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 SUMMARY: E:\FR\FM\29JAR1.SGM 29JAR1 ER29JA19.000</GPH> 444

Agencies

[Federal Register Volume 84, Number 19 (Tuesday, January 29, 2019)]
[Rules and Regulations]
[Pages 443-444]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2019-00297]


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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 https://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

0
1. The authority citation for part 39 continues to read as follows:

    Authority: 49 U.S.C. 106(g), 40113, 44701.


Sec.  39.13  [Corrected]

0
2. The FAA amends Sec.  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

[[Page 444]]

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.

[GRAPHIC] [TIFF OMITTED] TR29JA19.000

(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-ANM-Seattle-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

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