This section of the FEDERAL REGISTER

contains notices to the public of the proposed

issuance of rules and regulations. The

purpose of these notices is to give interested

persons an opportunity to participate in the

rule making prior to the adoption of the final

rules.

Proposed Rules Federal Register

30370 

Vol. 83, No. 125 

Thursday, June 28, 2018 

DEPARTMENT OF ENERGY 

10 CFR Parts 429 and 430 

[EERE–2018–BT–TP–0004] 

Energy Conservation Program: Test 

Procedures for Cooking Products, 

Notice of Petition for Rulemaking 

AGENCY: Office of Energy Efficiency and 

Renewable Energy, Department of 

Energy (DOE). 

ACTION: Notification of petition for 

rulemaking; reopening of the public 

comment period. 

SUMMARY: This document reopens the 

public comment period for submitting 

comments, data and information on the 

Association of Home Appliance 

Manufacturers (AHAM) petition to 

withdraw the conventional cooking top 

test procedure published on April 25, 

2018. The public comment period 

closed on June 25, 2018 and is reopened 

for 21 days until July 19, 2018. 

DATES: DOE is reopening the comment 

period for AHAM’s petition to withdraw 

the cooking top test procedure 

published on April 25, 2018 (83 FR 

17944). Submit comments July 19, 2018. 

ADDRESSES: Interested persons are 

encouraged to submit comments, 

identified by ‘‘Test Procedure Cooking 

Products Petition,’’ by any of the 

following methods: 

Federal eRulemaking Portal: http://

www.regulations.gov. Follow the 

instructions for submitting comments. 

Email: CookProducts2018TP0004@

ee.doe.gov. Include the docket number 

EERE–2018–BT–TP–0004 in the subject 

line of the message. 

Mail: Appliance and Equipment 

Standards Program, U.S. Department of 

Energy, Building Technologies Office, 

Mailstop EE–5B, 1000 Independence 

Avenue SW, Washington, DC, 20585– 

0121, identified by docket number 

EERE–2018–BT–TP–0004. If possible, 

please submit all items on a compact 

disc (CD), in which case it is not 

necessary to include printed copies. 

Hand Delivery/Courier: Appliance 

and Equipment Standards Program, U.S. 

Department of Energy, Building 

Technologies Office, 950 L’Enfant Plaza 

SW, Suite 600, Washington, DC 20024. 

Telephone: (202) 586–6636. If possible, 

please submit all items on a CD, in 

which case it is not necessary to include 

printed copies. 

Docket: For access to the docket to 

read background documents, or 

comments received, go to the Federal 

eRulemaking Portal at http://

www.regulations.gov. 

FOR FURTHER INFORMATION CONTACT: 

Celia Sher, U.S. Department of Energy, 

Office of the General Counsel, 1000 

Independence Avenue SW, Washington, 

DC 20585. Email: Celia.Sher@

hq.doe.gov; (202) 287–6122. 

SUPPLEMENTARY INFORMATION: On April 

25, 2018, the U.S. Department of Energy 

(DOE) published a petition from AHAM 

requesting that DOE reconsider its final 

rule on Test Procedures for Cooking 

Products, Docket No. EERE–2012–BT– 

TP–0013, RIN 1904–AC71, 81 FR 91418 

(Dec. 16, 2016) (Final Rule). In the 

petition, AHAM requested that DOE 

undertake rulemaking to withdraw the 

cooking top test procedure, while 

maintaining the repeal of the oven test 

procedure that was part of the Final 

Rule. 83 FR 17944. The notice of 

petition provided for the written 

submission of comments by June 25, 

2018. AHAM requested an extension of 

the public comment period to allow 

additional time for AHAM and its 

members to provide data responsive to 

DOE’s detailed inquiries regarding the 

petition. For the same reason, GE 

Appliances also requested an extension 

of the comment period. 

DOE has determined that an extension 

of the public comment period is 

appropriate to allow interested parties 

additional time to submit comments for 

DOE’s consideration. Thus, DOE is 

reopening the comment period by 21 

days, until July 19, 2018. DOE will 

consider any comments received by 

midnight of July 19, 2018 to be timely 

submitted. 

Signed in Washington, DC, on June 22, 

2018. 

Kathleen B. Hogan, 

Deputy Assistant Secretary for Energy 

Efficiency, Energy Efficiency and Renewable 

Energy. 

[FR Doc. 2018–13927 Filed 6–27–18; 8:45 am] 

BILLING CODE 6450–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2018–0431; Product 

Identifier 2018–NE–16–AD] 

RIN 2120–AA64 

Airworthiness Directives; International 

Aero Engines (IAE) Turbofan Engines 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: We propose to adopt a new 

airworthiness directive (AD) for certain 

International Aero Engines (IAE) 

PW1133G–JM, PW1133GA–JM, 

PW1130G–JM, PW1127G–JM, 

PW1127GA–JM, PW1127G1–JM, 

PW1124G–JM, PW1124G1–JM, and 

PW1122G–JM turbofan engines with a 

certain high-pressure compressor (HPC) 

front hub installed. This proposed AD 

was prompted by corrosion found on 

the HPC front hub. This proposed AD 

would require replacing the HPC front 

hub with a part eligible for installation. 

We are proposing this AD to address the 

unsafe condition on these products. 

DATES: We must receive comments on 

this proposed AD by August 13, 2018. 

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. 


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For service information identified in 

this NPRM, contact International Aero 

Engines (IAE), 400 Main Street, East 

Hartford, CT 06118; phone: 800–565– 

0140; email: help24@pw.utc.com; 

internet: http://fleetcare.pw.utc.com. 

You may view this service information 

at the FAA, Engine and Propeller 

Standards Branch, 1200 District 

Avenue, Burlington, MA 01803. For 

information on the availability of this 

material at the FAA, call 781–238–7759. 

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–2018– 

0431; or in person at Docket Operations 

between 9 a.m. and 5 p.m., Monday 

through Friday, except Federal holidays. 

The AD docket contains this NPRM, the 

regulatory evaluation, any comments 

received, and other information. The 

street address for Docket Operations 

(phone: 800–647–5527) is listed above. 

Comments will be available in the AD 

docket shortly after receipt. 

FOR FURTHER INFORMATION CONTACT: 

Kevin M. Clark, Aerospace Engineer, 

ECO Branch, FAA, 1200 District 

Avenue, Burlington, MA 01803; phone: 

781–238–7088; fax: 781–238–7199; 

email: kevin.m.clark@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Comments Invited 

We invite you to send any written 

relevant data, views, or arguments about 

this proposal. Send your comments to 

an address listed under the ADDRESSES

section. Include ‘‘Docket No. FAA– 

2018–0431; Product Identifier 2018– 

NE–16–AD’’ at the beginning of your 

comments. We specifically invite 

comments on the overall regulatory, 

economic, environmental, and energy 

aspects of this NPRM. We will consider 

all comments received by the closing 

date and may amend this NPRM 

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 NPRM. 

Discussion 

We received a report that corrosion 

was found on HPC front hub, part 

number (P/N) 30G2401. The HPC front 

hub exhibited deposits that could not be 

removed using standard procedures and 

worsened over time. After further 

investigation, pitting corrosion was 

found below the painted surface. This 

condition, if not addressed, could result 

in uncontained HPC front hub release, 

damage to the engine, and damage to the 

airplane. 

Related Service Information 

We reviewed Section PW1000G–C– 

05–10–00–02A–288A–D of the 

PW1100G–JM Series Airworthiness 

Limitations Manual, P/N 5316993, dated 

September 30, 2015. Section PW1000G– 

C–05–10–00–02A–288A–D provides 

guidance for an approved FAA method 

of mixed model cycles since new 

calculation. 

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 require 

removing from service the HPC front 

hub, P/N 30G2401, and replacing it with 

a part eligible for installation. 

Costs of Compliance 

We estimate that this proposed AD 

affects 16 engines installed on airplanes 

of U.S. registry. 

We estimate the following costs to 

comply with this proposed AD: 

ESTIMATED COSTS

Action Labor cost Parts cost Cost per 

product 

Cost on U.S. 

operators 

Replace HPC front hub ................................... 0 work-hours × $85 per hour = $0 ................. $11,600 $11,600 $185,600 

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. 

This AD is issued in accordance with 

authority delegated by the Executive 

Director, Aircraft Certification Service, 

as authorized by FAA Order 8000.51C. 

In accordance with that order, issuance 

of ADs is normally a function of the 

Compliance and Airworthiness 

Division, but during this transition 

period, the Executive Director has 

delegated the authority to issue ADs 

applicable to engines, propellers, and 

associated appliances to the Manager, 

Engine and Propeller Standards Branch, 

Policy and Innovation Division. 

Regulatory Findings 

We 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 this 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, 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. 


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30372 Federal Register / Vol. 83, No. 125 / Thursday, June 28, 2018 / Proposed Rules 

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 adding 

the following new airworthiness 

directive (AD): 

International Aero Engines: Docket No. 

FAA–2018–0431; Product Identifier 

2018–NE–16–AD. 

(a) Comments Due Date 

We must receive comments by August 13, 

2018. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to International Aero 

Engines (IAE) PW1133G–JM, PW1133GA–JM, 

PW1130G–JM, PW1127G–JM, PW1127GA– 

JM, PW1127G1–JM, PW1124G–JM, 

PW1124G1–JM, and PW1122G–JM turbofan 

engines with high-pressure compressor (HPC) 

front hub, part number (P/N) 30G2401, 

installed. 

(d) Subject 

Joint Aircraft System Component (JASC) 

Code 7230, Turbine Engine Compressor 

Section. 

(e) Unsafe Condition 

This AD was prompted by corrosion found 

on the HPC front hub. We are issuing this AD 

to prevent cracking and failure of the HPC 

front hub. The unsafe condition, if not 

addressed, could result in uncontained HPC 

front hub release, damage to the engine, and 

damage to the airplane. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Required Actions 

Remove from service the HPC front hub, P/ 

N 30G2401, within 120 days after the 

effective date of this AD, or as follows, 

whichever occurs later, and replace with a 

part eligible for installation: 

(1) For PW1122G–JM, PW1124G1–JM, 

PW1124G–JM, PW1127G1–JM, PW1127GA– 

JM, and PW1127G–JM engines, remove the 

HPC front hub before exceeding 6,180 cycles 

since new (CSN) or within five years since 

the ship date listed in Table 1 to paragraph 

(g) of this AD, whichever occurs first. 

(2) For PW1130G–JM, PW1133GA–JM, and 

PW1133G–JM engines, remove the HPC front 

hub before exceeding 4,440 CSN or within 

four years since the ship date listed in Table 

1 to paragraph (g) of this AD, whichever 

occurs first. 

(3) For engines operating as a mix of 

models listed in paragraphs (g)(1) and (2) of 

this AD, remove the HPC front hub using a 

CSN calculated by an approved FAA method 

or within four years since the ship date listed 

in Table 1 to paragraph (g) of this AD, 

whichever occurs first. You may find 

guidance for an approved FAA method of 

mixed model CSN calculation in Section 

PW1000G–C–05–10–00–02A–288A–D of the 

PW1100G–JM Series Airworthiness 

Limitations Manual, P/N 5316993, dated 

September 30, 2015. 

(4) For any HPC front hub, P/N 30G2401, 

whose serial number is not listed in Table 1 

to paragraph (g) of this AD, use October 21, 

2015, as the ship date. 

BILLING CODE 4910–13–P 


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Table 1 to Paragraph (g) - Steel Front Hub Ship Date 

Originally Installed in 

Steel Front Hub Serial Number Ship Date Engine Serial Number 

LENCAJ3513 10/23/2015 P770121 

LENCAJ4524 11/6/2015 P770125 

LENCAJ2782 11/25/2015 P770126 

LENCAJ2794 11/9/2015 P770127 

LENCAJ4527 11/17/2015 P770128 

LENCAJ3500 11/16/2015 P770129 

LENCAJ4508 11/23/2015 P770130 

LENCAJ3505 6/20/2016 P770131 

LENCAJ4518 12/2/2015 P770132 

LENCAJ3507 12/31/2015 P770133 

LENCAJ2789 12/22/2015 P770134 

LENCAJ4516 12/12/2015 P770135 

LENCAJ3509 12/31/2015 P770136 

LENCAJ3511 12/28/2015 P770137 

LENCAJ4538 1/6/2016 P770138 

LENCAJ4535 1/8/2016 P770139 

LENCAJ2788 1/17/2016 P770140 

LENCAJ4512 1/17/2016 P770141 

LENCAJ3502 1/31/2016 P770142 

LENCAJ3503 2/7/2016 P770143 

LENCAJ4540 1/31/2016 P770144 

LENCAJ3510 2/17/2016 P770145 

LENCAJ4539 2/14/2016 P770146 

LENCAJ4525 2/25/2016 P770147 

LENCAJ4531 2/20/2016 P770148 

LENCAJ4510 3/14/2016 P770149 

LENCAJ4522 2/27/2016 P770150 

LENCAJ3506 2/27/2016 P770151 

LENCAJ4532 3/11/2016 P770153 

LENCAJ3506 3/17/2016 P770154 

LENCAJ4534 3/31/2016 P770155 

LENCAJ4548 6/13/2016 P770160 

LENCAJ4552 5/6/2016 P770161 

LENCAJ4521 4/30/2016 P770163 

LENCAJ4529 4/30/2016 P770164 

LENCAJ4520 4/28/2016 P770165 

LENCAJ4544 4/30/2016 P770166 

LENCAJ4511 8/25/2016 P770167 

LENCAJ4549 8/26/2016 P770168 
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LENCAJ4553 5/19/2016 P770169 

LENCAJ4551 5/19/2016 P770170 

LENCAJ4517 5/21/2016 P770171 

LENCAJ4543 5/19/2016 P770172 

LENCAJ4513 5/31/2016 P770173 

LENCAJ4550 5/20/2016 P770174 

LENCAJ4530 6/8/2016 P770175 

LENCAJ4533 5/26/2016 P770176 

LENCAJ4515 6/8/2016 P770177 

LENCAJ4563 6/26/2016 P770178 

LENCAJ4545 6/10/2016 P770179 

LENCAJ4542 6/10/2016 P770180 

LENCAJ4546 6/22/2016 P770181 

LENCAJ4566 6/22/2016 P770182 

LENCAJ4558 6/23/2016 P770183 

LENCAJ4507 8/31/2016 P770184 

LENCAK4516 8/29/2016 P770185 

LENCAJ3508 7/8/2016 P770186 

LENCAJ4572 6/30/2016 P770187 

LENCAJ4573 6/28/2016 P770188 

LENCAJ4555 6/29/2016 P770189 

LENCAJ4565 6/30/2016 P770190 

LENCAJ4559 7/5/2016 P770191 

LENCAJ4570 7/16/2016 P770192 

LENCAJ4560 7/23/2016 P770193 

LENCAJ4571 7/23/2016 P770194 

LENCAJ4562 7/25/2016 P770195 

LENCAJ4526 8/12/2016 P770196 

LENCAJ4561 8/9/2016 P770197 

LENCAJ4504 7/29/2016 P770198 

LENCAJ4579 8/7/2016 P770199 

LENCAJ4519 8/3/2016 P770200 

LENCAK4517 8/9/2016 P770201 

LENCAJ4595 8/17/2016 P770202 

LENCAK4523 8/30/2016 P770203 

LENCAK4505 8/15/2016 P770204 

LENCAJ4541 8/31/2016 P770205 

LENCAJ4592 8/22/2016 P770206 

LENCAJ4569 9/30/2016 P770207 

LENCAK4512 8/29/2016 P770208 

LENCAK4518 10/7/2016 P770210 

LENCAK4541 8/31/2016 P770211 

LENCAK4535 9/17/2016 P770212 
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LENCAJ4584 9/20/2016 P770213 

LENCAK4538 9/3/2016 P770214 

LENCAK4533 11/30/2016 P770215 

LENCAJ4594 9/23/2016 P770216 

LENCAJ4509 10/25/2016 P770217 

LENCAK4526 9/16/2016 P770218 

LENCAK4532 9/19/2016 P770219 

LENCAJ4602 9/22/2016 P770220 

LENCAK4513 9/27/2016 P770221 

LENCAK5147 10/19/2016 P770222 

LENCAK4536 10/19/2016 P770223 

LENCAK4522 9/30/2016 P770224 

LENCAJ4578 12/29/2016 P770225 

LENCAJ4596 9/30/2016 P770226 

LENCAJ4575 10/4/2017 P770227 

LENCAJ4577 12/5/2016 P770228 

LENCAJ4597 10/12/2016 P770229 

LENCAJ4588 10/19/2016 P770230 

LENCAK4552 10/14/2016 P770231 

LENCAJ4537 10/29/2016 P770232 

LENCAJ4586 10/21/2016 P770233 

LENCAJ4528 11/18/2016 P770234 

LENCAJ4554 12/29/2016 P770235 

LENCAK4553 11/1/2016 P770236 

LENCAJ4598 11/18/2016 P770237 

LENCAK4550 12/5/2016 P770238 

LENCAJ4603 12/5/2016 P770239 

LENCAJ4585 12/5/2016 P770240 

LENCAK4537 12/2/2016 P770241 

LENCAK4520 11/8/2016 P770242 

LENCAK4528 12/2/2016 P770243 

LENCAK5171 11/30/2016 P770244 

LENCAK4549 12/5/2016 P770245 

LENCAJ4557 12/5/2016 P770246 

LENCAK4515 12/7/2016 P770247 

LENCAJ4601 1/8/2017 P770248 

LENCAK4511 12/7/2016 P770249 

LENCAJ4581 2/21/2017 P770250 

LENCAK5182 11/30/2016 P770251 

LENCAK5153 11/30/2016 P770252 

LENCAJ4576 12/12/2016 P770253 

LENCAK4539 2/26/2017 P770254 

LENCAJ4591 8/23/2017 P770255 
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LENCAK5166 12/15/2016 P770256 

LENCAK5193 12/17/2016 P770258 

LENCAK5149 12/21/2016 P770259 

LENCAK5157 3/28/2017 P770260 

LENCAK5191 12/20/2016 P770261 

LENCAK5176 12/20/2016 P770262 

LENCAK4545 12/21/2016 P770263 

LENCAK5192 12/22/2016 P770264 

LENCAK4548 12/23/2016 P770265 

LENCAK5154 12/27/2016 P770266 

LENCAK5163 12/28/2016 P770267 

LENCAK5184 12/23/2016 P770268 

LENCAK4507 12/31/2016 P770269 

LENCAK5165 2/2/2017 P770270 

LENCAK5173 12/29/2016 P770271 

LENCAJ4589 12/29/2016 P770272 

LENCAK5179 12/31/2016 P770273 

LENCAK4543 1/10/2017 P770275 

LENCAK4510 3/31/2017 P770276 

LENCAK5156 1/17/2017 P770277 

LENCAK5169 1/16/2017 P770278 

LENCAK4524 1/19/2017 P770279 

LENCAK5187 1/24/2017 P770280 

LENCAK5175 1/24/2017 P770281 

LENCAK4546 1/25/2017 P770282 

LENCAK5185 1/24/2017 P770283 

LENCAK5162 2/8/2017 P770284 

LENCAK5150 8/25/2017 P770285 

LENCAK5144 3/31/2017 P770286 

LENCAJ2787 1/31/2017 P770287 

LENCAK4554 1/25/2017 P770288 

LENCAK5186 1/31/2017 P770289 

LENCAK5172 1/31/2017 P770290 

LENCAK5170 1/31/2017 P770291 

LENCAK5155 2/6/2017 P770292 

LENCAK5164 2/7/2017 P770293 

LENCAK5168 2/13/2017 P770294 

LENCAK4514 2/14/2017 P770295 

LENCAK5189 6/22/2017 P770296 

LENCAK7184 2/16/2017 P770297 

LENCAK5146 2/28/2017 P770298 

LENCAK5151 2/27/2017 P770299 

LENCAK5152 8/14/2017 P770300 
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BILLING CODE 4910–13–C 

(h) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, ECO 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)(1) of this AD. You 

may email your request to: ANE-AD-AMOC@

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. 

(i) Related Information 

(1) For more information about this AD, 

contact Kevin M. Clark, Aerospace Engineer, 

ECO Branch, FAA, 1200 District Avenue, 

Burlington, MA 01803; phone: 781–238– 

7088; fax: 781–238–7199; email: 

kevin.m.clark@faa.gov. 

(2) For service information identified in 

this AD, contact International Aero Engines 

(IAE), 400 Main Street, East Hartford, CT 

06118; phone: 800–565–0140; email: help24@

pw.utc.com; internet: http://

fleetcare.pw.utc.com. You may view this 

referenced service information at the FAA, 

Engine and Propeller Standards Branch, 1200 

District Avenue, Burlington, MA 01803. For 

information on the availability of this 

material at the FAA, call 781–238–7759. 

Issued in Burlington, MA, on June 22, 

2018. 

Robert J. Ganley, 

Manager, Engine and Propeller Standards 

Branch, Aircraft Certification Service. 

[FR Doc. 2018–13795 Filed 6–27–18; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2018–0555; Product 

Identifier 2017–NM–152–AD] 

RIN 2120–AA64 

Airworthiness Directives; BAE 

Systems (Operations) Limited 

Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: We propose to adopt a new 

airworthiness directive (AD) for all BAE 

Systems (Operations) Limited Model 

4101 airplanes. This proposed AD was 

prompted by a report of an improperly 

installed spacer around the electrical 

pins in the cartridge connector for the 

fire bottle extinguisher cartridge. This 

proposed AD would require repetitive 

inspections for excessive or missing 

spacers, and applicable corrective 


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