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

36433 

Vol. 81, No. 109 

Tuesday, June 7, 2016 

DEPARTMENT OF HOMELAND 

SECURITY 

Office of the Secretary 

6 CFR Part 5 

[Docket No. DHS–2016–0035] 

Privacy Act of 1974: Implementation of 

Exemptions; Department of Homeland 

Security/U.S. Customs and Border 

Protection–014 Regulatory Audit 

Archive System (RAAS) System of 

Records 

AGENCY: Privacy Office, Department of 

Homeland Security. 

ACTION: Final rule. 

SUMMARY: The Department of Homeland 

Security (DHS) is issuing a final rule to 

extend the exemptions from certain 

provisions of the Privacy Act to the 

updated and reissued system of records 

titled, ‘‘DHS/CBP–014 Regulatory Audit 

Archive System (RAAS) System of 

Records.’’ Specifically, the Department 

exempts portions of the ‘‘DHS/CBP–014 

Regulatory Audit Archive System 

(RAAS) System of Records’’ from one or 

more provisions of the Privacy Act 

because of criminal, civil, and 

administrative enforcement 

requirements. 

DATES: This final rule is effective June 

7, 2016. 

FOR FURTHER INFORMATION CONTACT: For 

general questions, please contact: John 

Connors, (202) 344–1610, Privacy 

Officer, U.S. Customs and Border 

Protection, Privacy and Diversity Office, 

1300 Pennsylvania Avenue NW., 

Washington, DC 20229. For privacy 

questions, please contact: Karen L. 

Neuman, (202) 343–1717, Chief Privacy 

Officer, Privacy Office, Department of 

Homeland Security, Washington, DC 

20528. 

SUPPLEMENTARY INFORMATION: 

I. Background 

The Department of Homeland 

Security (DHS) U.S. Customs and 

Border Protection (CBP) published a 

notice of proposed rulemaking in the 

Federal Register, 81 FR 19932, April 6, 

2016, proposing to exempt portions of 

the system of records from one or more 

provisions of the Privacy Act because of 

criminal, civil, and administrative 

enforcement requirements. DHS 

reissued the DHS/CBP–014 Regulatory 

Audit Archive System (RAAS) System 

of Records in the Federal Register on 

April 6, 2016 (81 FR 19985), to provide 

notice to the public that DHS/CBP was 

updating the categories of records to 

include the capture of Employer 

Identification Numbers (EINs) or Social 

Security numbers (SSNs), also known as 

a Federal Taxpayer Identifying Number, 

pursuant to 19 CFR 24.5, 19 CFR 149.3, 

and E.O. 9397, as amended by E.O. 

13748. This final rule exempts portions 

of the new categories of records 

pursuant to 5 U.S.C. 552a(k)(2). 

II. Public Comments 

DHS received no comments on the 

NPRM and will implement the 

rulemaking as proposed. 

List of Subjects in 6 CFR Part 5 

Freedom of information; Privacy. 

For the reasons stated in the 

preamble, DHS amends Chapter I of 

Title 6, Code of Federal Regulations, as 

follows: 

PART 5—DISCLOSURE OF RECORDS 

AND INFORMATION 

■ 1. The authority citation for part 5 

continues to read as follows: 

Authority: Pub. L. 107–296, 116 Stat. 

2135; (6 U.S.C. 101 et seq.); 5 U.S.C. 301. 

Subpart A also issued under 5 U.S.C. 552. 

Subpart B also issued under 5 U.S.C. 552a. 

■ 2. In appendix C to part 5, revise the 

introductory text of paragraph 25, and 

paragraph 25(a), to read as follows: 

Appendix C to Part 5—DHS Systems of 

Records Exempt From the Privacy Act 

* * * * * 

25. The Department of Homeland Security 

(DHS)/U.S. Customs and Border Protection014 Regulatory Audit Archive System 

(RAAS) System of Records consists of 

electronic and paper records and will be used 

by DHS and its Components. The DHS/CBP– 

014 RAAS System of Records is a repository 

of information held by DHS in connection 

with its several and varied missions and 

functions, including, but not limited to: the 

enforcement of civil and criminal laws; 

investigations; inquiries; and proceedings 

there under. The DHS/CBP–014 RAAS 

System of Records contains information that 

is collected by, on behalf of, in support of, 

or in cooperation with DHS and its 

Components and may contain personally 

identifiable information collected by other 

Federal, State, local, tribal, foreign, or 

international government agencies. The 

Secretary of Homeland Security, pursuant to 

5 U.S.C. 552a(k)(2), has exempted this system 

from the following provisions of the Privacy 

Act: 5 U.S.C. 552a(c)(3). Exemptions from 

these particular subsections are justified, on 

a case-by-case basis to be determined at the 

time a request is made, for the following 

reasons: 

(a) From subsection (c)(3) (Accounting for 

Disclosures) because release of the 

accounting of disclosures could alert the 

subject of an investigation of an actual or 

potential criminal, civil, or regulatory 

violation to the existence of that investigation 

and reveal investigative interest on the part 

of DHS as well as the recipient agency. 

Disclosure of the accounting would therefore 

present a serious impediment to law 

enforcement efforts and/or efforts to preserve 

national security. Disclosure of the 

accounting would also permit the individual 

who is the subject of a record to impede the 

investigation, to tamper with witnesses or 

evidence, and to avoid detection or 

apprehension, which would undermine the 

entire investigative process. 

* * * * * 

Dated: May 23, 2016. 

Karen L. Neuman, 

Chief Privacy Officer, Department of 

Homeland Security. 

[FR Doc. 2016–13311 Filed 6–6–16; 8:45 am] 

BILLING CODE 9111–14–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2015–2958; Directorate 

Identifier 2014–NM–248–AD; Amendment 

39–18545; AD 2016–11–18] 

RIN 2120–AA64 

Airworthiness Directives; The Boeing 

Company Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for all The 


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36434 Federal Register / Vol. 81, No. 109 / Tuesday, June 7, 2016 / Rules and Regulations 

Boeing Company Model 787 airplanes. 

This AD was prompted by the 

disclosure that the inner diameters of 

some batches of landing gear pins were 

not shot peened in accordance with 

design specifications, and need to be 

replaced. This AD requires inspection 

for improperly manufactured landing 

gear pins, and replacement if necessary. 

We are issuing this AD to detect and 

correct insufficient shot peening that 

could lead to stress corrosion cracking 

and failure of the landing gear pin, and 

cause landing gear collapse and 

inability to control the airplane at high 

speeds on the ground. 

DATES: This AD is effective July 12, 

2016. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of July 12, 2016. 

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 referenced 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. It is also 

available on the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2015– 

2958. 

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– 

2958; 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 

Document 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: 

Melanie Violette, Senior Aerospace 

Engineer, Airframe Branch, ANM–120S, 

FAA, Seattle Aircraft Certification 

Office (ACO), 1601 Lind Avenue SW., 

Renton, WA 98057–3356; phone: 425– 

917–6422; fax: 425–917–6590; email: 

melanie.violette@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 by adding an AD that would 

apply to all The Boeing Company Model 

787 airplanes. The NPRM published in 

the Federal Register on July 23, 2015 

(80 FR 43642) (‘‘the NPRM’’). The 

NPRM was prompted by a report 

indicating that the inner diameters of 

some batches of landing gear pins were 

not shot peened and need to be 

replaced. The NPRM proposed to 

require inspection for improperly 

manufactured landing gear pins, and 

replacement if necessary. We are issuing 

this AD to detect and correct 

insufficient shot peening that could lead 

to stress corrosion cracking and failure 

of the landing gear pin, and cause 

landing gear collapse and inability to 

control the airplane at high speeds on 

the ground. 

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. 

Request To Use Revised Service 

Information 

One commenter, Junji Miura, found 

several errors in Boeing Alert Service 

Bulletin B787–81205–SB320022–00, 

Issue 001, dated November 14, 2014, 

and requested that we include a 

reference to the upcoming corrections. 

The commenter stated that Boeing will 

correct these errors in the next revision, 

and that referencing this revision in this 

AD will avoid the need for a global 

alternative method of compliance 

(AMOC). 

We agree with the request. Boeing has 

issued Alert Service Bulletin B787– 

81205–SB320022–00, Issue 002, dated 

April 6, 2016. We have reviewed this 

service information, which was issued 

to correct typographical errors and part 

numbers, and to update statements, but 

adds no new actions. The changes in 

Boeing Alert Service Bulletin B787– 

81205–SB320022–00, Issue 002, dated 

April 6, 2016, address the commenter’s 

concerns. We have revised the service 

information references throughout this 

final rule to refer to Boeing Alert Service 

Bulletin B787–81205–SB320022–00, 

Issue 002, dated April 6, 2016, and we 

have added a new paragraph (h) to this 

AD to provide credit for the original 

service information. We have 

redesignated subsequent paragraphs 

accordingly. 

Request for Correction to Paragraphs 

(g) and (h) of This AD 

Boeing requested a correction to 

paragraphs (g) and (h) of the proposed 

AD to replace the word ‘‘or’’ with the 

word ‘‘and’’ in the phrase ‘‘part number 

or serial number.’’ 

We agree to correct the applicable 

paragraphs of this AD because the intent 

was to require replacement of the pin 

only if both the part number and serial 

number are identified in Boeing Alert 

Service Bulletin B787–81205– 

SB320022–00, Issue 002, dated April 6, 

2016. In paragraphs (g) and (i) of this 

AD, we revised the phrase ‘‘part number 

or serial number’’ to ‘‘part number and 

serial number.’’ 

Request for Clarification of Airplanes 

Affected by Inspection Requirements 

One commenter, Raja Rehman, 

requested that we clarify the required 

actions for airplanes that are covered by 

this AD, but not listed in the 

‘‘Effectivity’’ section of Boeing Alert 

Service Bulletin B787–81205– 

SB320022–00, Issue 001, dated 

November 14, 2014. The commenter 

asked if the inspection requirements of 

the proposed AD would apply to all 

delivered and to-be-delivered Model 

787 airplanes, and if Boeing intends to 

issue a revision to the service bulletin 

that will cover the additional airplanes. 

The commenter also asked if an airplane 

that did not have the affected pins 

installed at production/delivery, and 

had never replaced the pins during 

service would comply with the AD. 

We agree that clarification is 

necessary. The landing gear pin is a 

removable structural component 

(rotable part). Through maintenance 

action, the affected (discrepant) pins 

could be installed on airplanes that 

were initially delivered with acceptable 

pins. Therefore, the applicability of this 

AD is all Model 787 airplanes—both 

those that are currently delivered and 

future deliveries—because the affected 

pins could be installed on any Model 

787 airplane. It is not necessary for the 

applicability of the AD to match the 

effectivity of Boeing Alert Service 

Bulletin B787–81205–SB320022–00, 

Issue 001, dated November 14, 2014, or 

Issue 002, dated April 6, 2016. This 

difference has been coordinated with 

Boeing. 

We have modified paragraph (g) to 

require the inspections only for 

airplanes that received their original 

airworthiness certificate or original 

export certificate of airworthiness on or 

before the effective date of this AD. 

These are the airplanes that either had 

the affected (discrepant) pins installed 


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Federal Register / Vol. 81, No. 109 / Tuesday, June 7, 2016 / Rules and Regulations 36435 

in production, or may have had them 

installed through maintenance action. 

Paragraph (i), which remains applicable 

to all Model 787 airplanes, prohibits 

installation of the affected pins in the 

future. 

Conclusion 

We reviewed the relevant data, 

considered the comments received, and 

determined that air safety and the 

public interest require adopting this AD 

with the changes described previously 

and 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. 

We also determined that these 

changes will not increase the economic 

burden on any operator or increase the 

scope of this AD. 

Related Service Information Under 1 

CFR Part 51 

We reviewed Boeing Alert Service 

Bulletin B787–81205–SB320022–00, 

Issue 002, dated April 6, 2016. The 

service information describes 

procedures to inspect and replace 

certain landing gear pins. This service 

information is reasonably available 

because the interested parties have 

access to it through their normal course 

of business or by the means identified 

in the ADDRESSES section. 

Costs of Compliance 

We estimate that this AD affects 13 

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 

Cost on U.S. 

operators 

Inspection ................................ 3 work-hours × $85 per hour = $255 ..................................... $0 $255 $3,315 

We estimate the following costs to do 

any necessary replacements that would 

be required based on the results of the 

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 .................................... Up to 19 work-hours × $85 per hour = $1,615 .......................................... $35,569 Up to 

$37,184 

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 

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. 

§ 39.13 [Amended] 

■ 2. The FAA amends § 39.13 by adding 

the following new airworthiness 

directive (AD): 

2016–11–18 The Boeing Company: 

Amendment 39–18545; Docket No. 

FAA–2015–2958; Directorate Identifier 

2014–NM–248–AD. 

(a) Effective Date 

This AD is effective July 12, 2016. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to all The Boeing 

Company Model 787 airplanes, certificated in 

any category. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 32, Landing Gear. 

(e) Unsafe Condition 

This AD was prompted by the disclosure 

that the inner diameters of some batches of 

landing gear pins were not shot peened in 

accordance with design specifications, and 

need to be replaced. We are issuing this AD 

to detect and correct insufficient shot 

peening that could lead to stress corrosion 

cracking and failure of the landing gear pin, 

and cause landing gear collapse and inability 

to control the airplane at high speeds on the 

ground. 


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36436 Federal Register / Vol. 81, No. 109 / Tuesday, June 7, 2016 / Rules and Regulations 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Inspection and Replacement 

For airplanes on which the original 

airworthiness certificate or the original 

export certificate of airworthiness was issued 

on or before the effective date of this AD: At 

the applicable time specified in paragraph 5, 

‘‘Compliance,’’ of Boeing Alert Service 

Bulletin B787–81205–SB320022–00, Issue 

002, dated April 6, 2016, do a landing gear 

pin part number and serial number 

inspection, in accordance with the 

Accomplishment Instructions of Boeing Alert 

Service Bulletin B787–81205–SB320022–00, 

Issue 002, dated April 6, 2016. A review of 

airplane maintenance or delivery records is 

acceptable in lieu of this inspection if the 

part number and serial number of the 

installed landing gear pins can be 

conclusively determined from that review. 

(1) If the part number and serial number do 

not match the list of affected pin numbers: 

No further action is required by this 

paragraph at that pin location. 

(2) If the part number and serial number 

match the list of affected pin numbers: At the 

applicable time specified in paragraph 5, 

‘‘Compliance,’’ of Boeing Alert Service 

Bulletin B787–81205–SB320022–00, Issue 

002, dated April 6, 2016, replace the affected 

pin with a pin that does not have an affected 

part number and serial number, in 

accordance with the Accomplishment 

Instructions of Boeing Alert Service Bulletin 

B787–81205–SB320022–00, Issue 002, dated 

April 6, 2016. 

(h) Credit for Previous Actions 

This paragraph provides credit for the 

actions specified in paragraph (g) of this AD, 

if those actions were performed before the 

effective date of this AD, using Boeing Alert 

Service Bulletin B787–81205–SB320022–00, 

Issue 001, dated November 14, 2014. This 

service information is not incorporated by 

reference in this AD. 

(i) Parts Installation Prohibition 

As of the effective date of this AD, no 

person may install on any airplane a landing 

gear pin having an affected part number and 

serial number identified in Boeing Alert 

Service Bulletin B787–81205–SB320022–00, 

Issue 002, dated April 6, 2016. 

(j) 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 (k) 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) 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, 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. 

(4) For service information that contains 

steps that are labeled as Required for 

Compliance (RC), the provisions of 

paragraphs (j)(4)(i) and (j)(4)(ii) of this AD 

apply. 

(i) The steps labeled as RC, including 

substeps under an RC step and any figures 

identified in an RC step, must be done to 

comply with the AD. An AMOC is required 

for any deviations to RC steps, including 

substeps and identified figures. 

(ii) Steps not labeled as RC may be 

deviated from using accepted methods in 

accordance with the operator’s maintenance 

or inspection program without obtaining 

approval of an AMOC, provided the RC steps, 

including substeps and identified figures, can 

still be done as specified, and the airplane 

can be put back in an airworthy condition. 

(k) Related Information 

For more information about this AD, 

contact Melanie Violette, Senior Aerospace 

Engineer, Airframe Branch, ANM–120S, 

FAA, Seattle ACO, 1601 Lind Avenue SW., 

Renton, WA 98057–3356; phone: 425–917– 

6422; fax: 425–917–6590; email: 

melanie.violette@faa.gov. 

(l) 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. 

(i) Boeing Alert Service Bulletin B787– 

81205–SB320022–00, Issue 002, dated April 

6, 2016. 

(ii) Reserved. 

(3) For 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. 

(4) 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. 

(5) 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 May 24, 

2016. 

Michael Kaszycki, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2016–12847 Filed 6–6–16; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2016–4232; Directorate 

Identifier 2015–CE–043–AD; Amendment 

39–18538; AD 2016–11–11] 

RIN 2120–AA64 

Airworthiness Directives; EVEKTOR, 

spol. S.r.o. Gliders 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for 

EVEKTOR, spol. s.r.o. Models L 13 SEH 

VIVAT and L 13 SDM VIVAT gliders 

(type certificate previously held by 

AEROTECHNIK s.r.o.). This AD results 

from mandatory continuing 

airworthiness information (MCAI) 

issued by an aviation authority of 

another country to identify and correct 

an unsafe condition on an aviation 

product. The MCAI describes the unsafe 

condition as lack of distinct color 

marking of the elevator drive. We are 

issuing this AD to require actions to 

address the unsafe condition on these 

products. 

DATES: This AD is effective July 12, 

2016. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in the AD 

as of July 12, 2016. 

ADDRESSES: You may examine the AD 

docket on the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2016– 

4232; or in person at Document 

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 service information identified in 

this AD, contact EVEKTOR, spol. s.r.o, 

Letecka 1008, 686 04 Kunovice, Czech 

Republic; phone: +420 572 537 428; 

email: evektor@evektor.cz; Internet: 

http://www.evektor.cz/en/sales-andsupport. You may view this referenced 

service information at the FAA, Small 


jstallworth on DSK7TPTVN1PROD with RULES