This section of the FEDERAL REGISTER

contains regulatory documents having general

applicability and legal effect, most of which

are keyed to and codified in the Code of

Federal Regulations, which is published under

50 titles pursuant to 44 U.S.C. 1510.

The Code of Federal Regulations is sold by

the Superintendent of Documents. Prices of

new books are listed in the first FEDERAL

REGISTER issue of each week.

Rules and Regulations Federal Register

20219 

Vol. 81, No. 67 

Thursday, April 7, 2016 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2015–0075; Directorate 

Identifier 2014–NM–202–AD; Amendment 

39–18461; AD 2016–07–16] 

RIN 2120–AA64 

Airworthiness Directives; The Boeing 

Company Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: We are superseding 

Airworthiness Directive (AD) 2013–26– 

08 for certain The Boeing Company 

Model 737–600, –700, –700C, –800, 

–900, and –900ER series airplanes. AD 

2013–26–08 required inspecting the 

orientation of both sides of the coil cord 

connector keyways of the number 2 

windows on the flight deck; re-clocking 

the connector keyways, if necessary; 

and replacing the coil cord assemblies 

on both number 2 windows on the flight 

deck. This new AD adds airplanes to the 

applicability. AD 2013–26–08 resulted 

from reports of arcing and smoke at the 

left number 2 window in the flight deck. 

This AD was prompted by a 

determination that additional airplanes 

are subject to the same identified unsafe 

condition. We are issuing this AD to 

prevent arcing, smoke, and fire in the 

flight deck, which could lead to injuries 

to or incapacitation of the flightcrew. 

DATES: This AD is effective May 12, 

2016. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of February 10, 2014 (79 FR 545, 

January 6, 2014). 

ADDRESSES: For service information 

identified in this final rule, contact 

Boeing Commercial Airplanes, 

Attention: Data & Services Management, 

P. O. Box 3707, MC 2H–65, Seattle, WA 

98124–2207; telephone 206–544–5000, 

extension 1; fax 206–766–5680; Internet 

https://www.myboeingfleet.com. You 

may view this service information at the 

FAA, Transport Airplane Directorate, 

1601 Lind Avenue SW., Renton, WA. 

For information on the availability of 

this material at the FAA, call 425–227– 

1221. This service information is also 

available on the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2015– 

0075. 

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–2015– 

0075; 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 the 

Docket Office (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: 

Frank Carreras, Aerospace Engineer, 

Systems and Equipment Branch, ANM– 

130S, FAA, Seattle Aircraft Certification 

Office (ACO), 1601 Lind Avenue SW., 

Renton, WA 98057–3356; phone: 425– 

917–6442; fax: 425–917–6590; email: 

frank.carreras@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 to supersede AD 2013–26–08, 

Amendment 39–17717 (79 FR 545, 

January 6, 2014) (‘‘AD 2013–26–08’’). 

AD 2013–26–08 applied to certain The 

Boeing Company Model 737–600, –700, 

–700C, –800, –900, and –900ER series 

airplanes. The NPRM published in the 

Federal Register on January 23, 2015 

(80 FR 3527) (‘‘the NPRM’’). AD 2013– 

26–08 resulted from reports of arcing 

and smoke at the left number 2 window 

in the flight deck. The NPRM was 

prompted by a determination that 

additional airplanes are subject to the 

same identified unsafe condition. The 

NPRM proposed to continue to require 

inspecting the orientation of both sides 

of the coil cord connector keyways of 

the number 2 windows on the flight 

deck; re-clocking the connector 

keyways, if necessary; and replacing the 

coil cord assemblies on both number 2 

windows on the flight deck. The NPRM 

also proposed to add airplanes to the 

applicability. We are issuing this AD to 

prevent arcing, smoke, and fire in the 

flight deck, which could lead to injuries 

to or incapacitation of the flightcrew. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. The 

following presents the comments 

received on the NPRM and the FAA’s 

response to each comment. 

Support for the NPRM 

Boeing stated that it supports the 

NPRM as written. 

Effect of Winglets on Accomplishment 

of the Proposed Actions 

Aviation Partners Boeing stated that 

the installation of winglets per 

Supplemental Type Certificate (STC) 

ST00830SE (http://rgl.faa.gov/

Regulatory_and_Guidance_Library/

rgstc.nsf/0/

184de9a71ec3fa5586257eae00707da6/

$FILE/ST00830SE.pdf) does not affect 

the accomplishment of the 

manufacturer’s service instructions. 

We agree with the commenter that 

STC ST00830SE (http://rgl.faa.gov/

Regulatory_and_Guidance_Library/

rgstc.nsf/0/

184de9a71ec3fa5586257eae00707da6/

$FILE/ST00830SE.pdf) does not affect 

the accomplishment of the 

manufacturer’s service instructions. 

Therefore, the installation of STC 

ST00830SE does not affect the ability to 

accomplish the actions required by this 

AD. We have not changed this AD in 

this regard. 

Comment Regarding Applicability 

United Airlines (UAL) stated that it 

found it curious that the technical 

compliance mandated in AD 2013–26– 

08 was per Boeing Special Attention 

Service Bulletin 737–30–1058, Revision 

5, dated April 24, 2013, whereas the 

airplane applicability in AD 2013–26– 

08 was based on Boeing Special 

Attention Service Bulletin 737–30– 

1058, Revision 4, dated November 3, 


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2011. UAL stated that, consequently, it 

anticipated further regulatory action 

that would include the Group 3 

airplanes specified in Boeing Special 

Attention Service Bulletin 737–30– 

1058, Revision 5, dated April 24, 2013, 

and has acted accordingly. UAL also 

stated that, since it was already 

planning accomplishment on the Group 

3 airplanes, the only impact to it will be 

to change the AD number on the 

compliance documentation. UAL stated 

that it has no further comments at this 

time. 

We acknowledge UAL’s comment. No 

change to this AD is necessary. 

Conclusion 

We reviewed the relevant data, 

considered the comments received, and 

determined that air safety and the 

public interest require adopting this AD 

as proposed except for minor editorial 

changes. We have determined that these 

minor changes: 

• Are consistent with the intent that 

was proposed in the NPRM for 

correcting the unsafe condition; and 

• Do not add any additional burden 

upon the public than was already 

proposed in the NPRM. 

Costs of Compliance 

We estimate that this AD affects 718 

airplanes of U.S. registry. 

We estimate the following costs to 

comply with this AD: 

ESTIMATED COSTS

Action Labor cost Parts cost Cost per product Number of airplanes Cost on U.S. operators 

Keyway inspection and installation (Group 1, Configuration 1 

airplanes) [actions retained 

from AD 2013-26-08].

6 work-hours × $85 

per hour = $510.

$1,608 $2,118 ....................... 712 $1,508,016. 

Adjustment of receptacles 

(Group 1, Configuration 2, 

Group 2, and Group 3 airplanes) [actions retained from 

AD 2013-26-08].

4 work-hours × $85 

per hour = $340.

0 340 ............................ 410 139,400. 

Coil cord inspection (Group 1, 

Configuration 3, and Group 2 

airplanes) [actions retained 

from AD 2013-26-08].

1 work-hour × $85 

per hour = $85 per 

coil cord.

0 85 per coil cord ........ 404 34,340 per coil cord. 

We estimate the following costs to do 

any necessary replacements that would 

be required based on the results of the 

coil cord inspection. We have no way of 

determining the number of aircraft that 

might need these replacements: 

ON-CONDITION COSTS

Action Labor cost Parts cost Cost per product 

Replacement ............... 3 work-hours × $85 per hour = $255 per coil 

cord assembly.

$1,735 per coil cord assembly ..... $1,990 per coil cord assembly. 

According to the manufacturer, some 

of the costs of this AD may be covered 

under warranty, thereby reducing the 

cost impact on affected individuals. We 

do not control warranty coverage for 

affected individuals. As a result, we 

have included all costs in our cost 

estimate. 

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 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, 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. 


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Federal Register / Vol. 81, No. 67 / Thursday, April 7, 2016 / Rules and Regulations 20221 

§ 39.13 [Amended] 

■ 2. The FAA amends § 39.13 by 

removing Airworthiness Directive (AD) 

2013–26–08, Amendment 39–17717 (79 

FR 545, January 6, 2014), and adding the 

following new AD: 

2016–07–16 The Boeing Company: 

Amendment 39–18461; Docket No. 

FAA–2015–0075; Directorate Identifier 

2014–NM–202–AD. 

(a) Effective Date 

This AD is effective May 12, 2016. 

(b) Affected ADs 

This AD replaces AD 2013–26–08, 

Amendment 39–17717 (79 FR 545, January 6, 

2014) (‘‘AD 2013–26–08’’). 

(c) Applicability 

This AD applies to The Boeing Company 

Model 737–600, –700, –700C, –800, –900, 

and –900ER series airplanes, certificated in 

any category, as identified in Boeing Special 

Attention Service Bulletin 737–30–1058, 

Revision 5, dated April 24, 2013. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 30, Ice and Rain Protection. 

(e) Unsafe Condition 

This AD was prompted by reports of arcing 

and smoke at the left number 2 window in 

the flight deck. We are issuing this AD to 

prevent arcing, smoke, and fire in the flight 

deck, which could lead to injuries to or 

incapacitation of the flightcrew. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Retained Inspection and Replacement for 

Group 1, Configuration 1, Airplanes 

This paragraph restates the requirements of 

paragraph (g) of AD 2013–26–08, with no 

changes. For airplanes identified as Group 1, 

Configuration 1, in Boeing Special Attention 

Service Bulletin 737–30–1058, Revision 5, 

dated April 24, 2013: Within 48 months after 

February 10, 2014 (the effective date of AD 

2013–26–08), do the actions specified in 

paragraphs (g)(1) and (g)(2) of this AD. 

(1) Do a general visual inspection of the 

orientation of the coil cord connector 

keyways on the captain’s and first officer’s 

sides of the flight compartment, in 

accordance with the Accomplishment 

Instructions of Boeing Special Attention 

Service Bulletin 737–30–1058, Revision 5, 

dated April 24, 2013, except as specified in 

paragraph (k) of this AD. If the orientation is 

not at the specified position, before further 

flight, turn the receptacle connector to the 

correct position, in accordance with the 

Accomplishment Instructions of Boeing 

Special Attention Service Bulletin 737–30– 

1058, Revision 5, dated April 24, 2013, 

except as specified in paragraph (k) of this 

AD. 

(2) Replace the coil cords with new coil 

cords on both sides of the flight deck, in 

accordance with the Accomplishment 

Instructions of Boeing Special Attention 

Service Bulletin 737–30–1058, Revision 5, 

dated April 24, 2013, except as specified in 

paragraph (k) of this AD. 

(h) Retained Receptacle Replacement for 

Group 1, Configuration 2, and Group 2, 

Configuration 1, Airplanes 

This paragraph restates the requirements of 

paragraph (h) of AD 2013–26–08, with no 

changes. For airplanes identified as Group 1, 

Configuration 2, and Group 2, Configuration 

1, in Boeing Special Attention Service 

Bulletin 737–30–1058, Revision 5, dated 

April 24, 2013: Within 48 months after 

February 10, 2014 (the effective date of AD 

2013–26–08), install the receptacle connector 

with changed keyway position on both sides 

of the flight deck, in accordance with the 

Accomplishment Instructions of Boeing 

Special Attention Service Bulletin 737–30– 

1058, Revision 5, dated April 24, 2013, 

except as specified in paragraph (k) of this 

AD. 

(i) Retained Coil Cord Inspection and 

Corrective Action 

This paragraph restates the requirements of 

paragraph (i) of AD 2013–26–08, with no 

changes. For airplanes identified as Group 1, 

Configuration 3, and Group 2, Configuration 

2, in Boeing Special Attention Service 

Bulletin 737–30–1058, Revision 5, dated 

April 24, 2013: Within 48 months after 

February 10, 2014 (the effective date of AD 

2013–26–08), do a general visual inspection 

for rubbing damage of the coil cord on the 

captain’s and first officer’s sides of the flight 

compartment, in accordance with the 

Accomplishment Instructions of Boeing 

Special Attention Service Bulletin 737–30– 

1058, Revision 5, dated April 24, 2013, 

except as specified in paragraph (k) of this 

AD. If any rubbing damage is found: Before 

further flight, replace the coil cord with a 

new coil cord, in accordance with the 

Accomplishment Instructions of Boeing 

Special Attention Service Bulletin 737–30– 

1058, Revision 5, dated April 24, 2013, 

except as specified in paragraph (k) of this 

AD. 

(j) New Requirements of This AD: Receptacle 

Replacement for Group 3 Airplanes 

For airplanes identified as Group 3 in 

Boeing Special Attention Service Bulletin 

737–30–1058, Revision 5, dated April 24, 

2013: Within 48 months after the effective 

date of this AD, install the receptacle 

connector with changed keyway position on 

both sides of the flight deck, in accordance 

with the Accomplishment Instructions of 

Boeing Special Attention Service Bulletin 

737–30–1058, Revision 5, dated April 24, 

2013, except as specified in paragraph (k) of 

this AD. 

(k) Exceptions to Boeing Special Attention 

Service Bulletin 737–30–1058, Revision 5, 

dated April 24, 2013 

(1) This paragraph restates the provisions 

of paragraph (j)(1) of AD 2013–26–08, with 

no changes. In the circuit breaker tables of 

the Work Instructions of Boeing Special 

Attention Service Bulletin 737–30–1058, 

Revision 5, dated April 24, 2013, the panel 

number for circuit breaker C00393 is 

incorrectly identified as ‘‘P6–12.’’ The correct 

panel number reference for circuit breaker 

C00393, ‘‘WINDOW HEAT POWER RIGHT 

SIDE,’’ is P6–11. 

(2) This paragraph restates the provisions 

of paragraph (j)(2) of AD 2013–26–08, with 

no changes. In paragraph 3.B. of the Work 

Instructions of Boeing Special Attention 

Service Bulletin 737–30–1058, Revision 5, 

dated April 24, 2013, the description for Part 

3 of the Work Instructions is identified as 

‘‘PART 3: RECEPTACLE CONNECTOR 

POSITION CHANGE,’’ which is incorrect. 

The correct description for Part 3 of the Work 

Instructions is ‘‘PART 3: COIL CORD 

INSPECTION AND REPLACEMENT IF 

DAMAGE IS FOUND.’’ 

(3) This paragraph restates the provisions 

of paragraph (j)(3) of AD 2013–26–08, with 

no changes. In Figures 13 and 14, in 

paragraph 3.B. of the Work Instructions of 

Boeing Special Attention Service Bulletin 

737–30–1058, Revision 5, dated April 24, 

2013, the note before the step tables 

misidentifies certain parts and airplane 

groups. The note should read: 

Note: Group 1 and Group 2 airplanes have 

the connector receptacle identified as 

D10572. Group 3 airplanes have the 

connector receptacle identified as D10560. 

Except for Group 1 airplanes, a wire diagram 

change is not necessary and not shown in 

this service bulletin. 

(l) Credit for Previous Actions 

This paragraph restates the provisions of 

paragraph (k) of AD 2013–26–08, with no 

changes. This paragraph provides credit for 

the replacement required by paragraph (g)(2) 

of this AD, if the replacement was performed 

before February 10, 2014 (the effective date 

of AD 2013–26–08), using the service 

information specified in paragraph (l)(1), 

(l)(2), (l)(3), (l)(4), or (l)(5) of this AD, 

provided that the actions required by 

paragraph (h) of this AD were done as 

specified in Boeing Special Attention Service 

Bulletin 737–30–1058, Revision 4, dated 

November 3, 2011; or Boeing Special 

Attention Service Bulletin 737–30–1058, 

Revision 5, dated April 24, 2013; for 

airplanes in Group 1, Configuration 2, and 

Group 2. 

(1) Boeing Service Bulletin 737–30–1058, 

dated July 27, 2006, which is not 

incorporated by reference in this AD. 

(2) Boeing Service Bulletin 737–30–1058, 

Revision 1, dated June 18, 2007, which is not 

incorporated by reference in this AD. 

(3) Boeing Service Bulletin 737–30–1058, 

Revision 2, dated February 13, 2009, which 

is not incorporated by reference in this AD. 

(4) Boeing Special Attention Service 

Bulletin 737–30–1058, Revision 3, dated July 

7, 2010, which is not incorporated by 

reference in this AD. 

(5) Boeing Special Attention Service 

Bulletin 737–30–1058, Revision 4, dated 

November 3, 2011, which was previously 

incorporated by reference on February 10, 

2014 (79 FR 545, January 6, 2014). 

(m) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, Seattle Aircraft 

Certification Office (ACO), FAA, has the 

authority to approve AMOCs for this AD, if 


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20222 Federal Register / Vol. 81, No. 67 / Thursday, April 7, 2016 / Rules and Regulations 

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 (n)(1) 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. 

(3) AMOCs approved for AD 2013–26–08, 

are approved as AMOCs for the 

corresponding provisions of this AD. 

(4) For airplanes identified as Group 3 in 

Boeing Special Attention Service Bulletin 

737–30–1058, Revision 5, dated April 24, 

2013, AMOCs approved for the actions 

required by paragraph (h) of AD 2013–26–08, 

are approved as AMOCs for the 

corresponding provisions of paragraph (j) of 

this AD. 

(n) Related Information 

(1) For more information about this AD, 

contact Frank Carreras, Aerospace Engineer, 

Systems and Equipment Branch, ANM–130S, 

FAA, Seattle Aircraft Certification Office 

(ACO), 1601 Lind Avenue SW., Renton, WA 

98057–3356; phone: 425–917–6442; fax: 425– 

917–6590; email: frank.carreras@faa.gov. 

(2) Service information identified in this 

AD that is not incorporated by reference is 

available at the addresses specified in 

paragraphs (o)(4) and (o)(5) of this AD. 

(o) 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. 

(3) The following service information was 

approved for IBR on February 10, 2014 (79 

FR 545, January 6, 2014). 

(i) Boeing Special Attention Service 

Bulletin 737–30–1058, Revision 5, dated 

April 24, 2013. 

(ii) Reserved. 

(4) For Boeing service information 

identified in this AD, contact Boeing 

Commercial Airplanes, Attention: Data & 

Services Management, P. O. Box 3707, MC 

2H–65, Seattle, WA 98124–2207; telephone 

206–544–5000, extension 1; fax 206–766– 

5680; Internet https://

www.myboeingfleet.com. 

(5) You may view this service information 

at FAA, Transport Airplane Directorate, 1601 

Lind Avenue SW., Renton, WA. For 

information on the availability of this 

material at the FAA, call 425–227–1221. 

(6) 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 Renton, Washington, on March 

24, 2016. 

Michael Kaszycki, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2016–07576 Filed 4–6–16; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2016–3692; Directorate 

Identifier 2016–NE–05–AD; Amendment 39– 

18458; AD 2016–07–13] 

RIN 2120–AA64 

Airworthiness Directives; GE Aviation 

Czech s.r.o. Turboprop Engines 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; request for 

comments. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 

GE Aviation Czech s.r.o. M601E–11 

turboprop engines. This AD requires 

inspection of the engine power turbine 

(PT) disk and, if found damaged, its 

replacement with a part eligible for 

installation. This AD was prompted by 

discovery of damage to certain engine 

PT disks during engine shop visits. We 

are issuing this AD to prevent failure of 

the engine PT disk, which could result 

in release of high-energy debris, damage 

to the engine, and reduced control of the 

airplane. 

DATES: This AD becomes effective April 

22, 2016. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of April 22, 2016. 

We must receive comments on this 

AD by May 23, 2016. 

ADDRESSES: You may send comments by 

any of the following methods: 

• Federal eRulemaking Portal: Go to 

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

instructions for submitting comments. 

• Mail: U.S. Department of 

Transportation, Docket Operations, M– 

30, West Building Ground Floor, Room 

W12–140, 1200 New Jersey Avenue SE., 

Washington, DC 20590–0001. 

• Hand Delivery: Deliver to Mail 

address above between 9 a.m. and 5 

p.m., Monday through Friday, except 

Federal holidays. 

• Fax: 202–493–2251. 

For service information identified in 

this AD, contact GE Aviation Czech 

s.r.o., Beranovy ́ch 65, 199 02 Praha 9— 

Letnˇ any, Czech Republic; phone: +420 

222 538 111; fax: +420 222 538 222. You 

may view this service information at the 

FAA, Engine & Propeller Directorate, 

1200 District Avenue, Burlington, MA 

01803. For information on the 

availability of this material at the FAA, 

call 781–238–7125. It is also available 

on the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2016– 

3692. 

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–2016– 

3692; or in person at the Docket 

Operations office between 9 a.m. and 5 

p.m., Monday through Friday, except 

Federal holidays. The AD docket 

contains this AD, the mandatory 

continuing airworthiness information 

(MCAI), regulatory evaluation, any 

comments received, and other 

information. The 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: 

Kenneth Steeves, Aerospace Engineer, 

Engine Certification Office, FAA, Engine 

& Propeller Directorate, 1200 District 

Avenue, Burlington, MA 01803; phone: 

781–238–7765; fax: 781–238–7199; 

email: kenneth.steeves@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Comments Invited 

This AD is a final rule that involves 

requirements affecting flight safety, and 

we did not precede it by notice and 

opportunity for public comment. We 

invite you to send any written relevant 

data, views, or arguments about this AD. 

Send your comments to an address 

listed under the ADDRESSES section. 

Include ‘‘Docket No. FAA–2016–3692; 

Directorate Identifier 2016–NE–05–AD’’ 

at the beginning of your comments. We 

specifically invite comments on the 

overall regulatory, economic, 

environmental, and energy aspects of 

this AD. We will consider all comments 

received by the closing date and may 

amend this 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 with FAA 

personnel concerning this AD. 


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