Federal Register / Vol. 83, No. 160 / Friday, August 17, 2018 / Rules and Regulations 40959 

§ 1016.8 requires you to provide a 

revised privacy notice, you must 

provide an annual privacy notice in 

accordance with the timing 

requirements in paragraph (a) of this 

section, treating the revised privacy 

notice as an initial privacy notice. 

(ii) Changes not preceded by a revised 

privacy notice. If you no longer meet the 

requirements of paragraph (e)(1) of this 

section because you change your 

policies or practices in such a way that 

§ 1016.8 does not require you to provide 

a revised privacy notice, you must 

provide an annual privacy notice within 

100 days of the change in your policies 

or practices that causes you to no longer 

meet the requirements of paragraph 

(e)(1) of this section. 

(iii) Examples. (A) You change your 

policies and practices in such a way that 

you no longer meet the requirements of 

paragraph (e)(1) of this section effective 

April 1 of year 1. Assuming you define 

the 12-consecutive-month period 

pursuant to paragraph (a) of this section 

as a calendar year, if you were required 

to provide a revised privacy notice 

under § 1016.8 and you provided that 

notice on March 1 of year 1, you must 

provide an annual privacy notice by 

December 31 of year 2. If you were not 

required to provide a revised privacy 

notice under § 1016.8, you must provide 

an annual privacy notice by July 9 of 

year 1. 

(B) You change your policies and 

practices in such a way that you no 

longer meet the requirements of 

paragraph (e)(1) of this section, and so 

provide an annual notice to your 

customers. After providing the annual 

notice to your customers, you once 

again meet the requirements of 

paragraph (e)(1) of this section for an 

exception to the annual notice 

requirement. You do not need to 

provide additional annual notices to 

your customers until such time as you 

no longer meet the requirements of 

paragraph (e)(1) of this section. 

■ 4. Section 1016.9 is amended by 

revising paragraph (c) to read as follows: 

§ 1016.9 Delivering privacy and opt out 

notices. 

* * * * * 

(c) Annual notices only. You may 

reasonably expect that a customer will 

receive actual notice of your annual 

privacy notice if: 

(1) The customer uses your website to 

access financial products and services 

electronically and agrees to receive 

notices at the website, and you post 

your current privacy notice 

continuously in a clear and conspicuous 

manner on the website; or 

(2) The customer has requested that 

you refrain from sending any 

information regarding the customer 

relationship, and your current privacy 

notice remains available to the customer 

upon request. 

* * * * * 

Dated: August 9, 2018. 

Mick Mulvaney, 

Acting Director, Bureau of Consumer 

Financial Protection. 

[FR Doc. 2018–17572 Filed 8–16–18; 8:45 am] 

BILLING CODE 4810–AM–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2018–0303; Product 

Identifier 2018–NM–006–AD; Amendment 

39–19360; AD 2018–17–06] 

RIN 2120–AA64 

Airworthiness Directives; Fokker 

Services B.V. Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 

Fokker Services B.V. Model F28 Mark 

0070 and 0100 airplanes. This AD was 

prompted by a report that the retraction 

actuator eye-end of a Goodrich main 

landing gear (MLG) failed. This AD 

requires a one-time general visual 

inspection of the left-hand (LH) and 

right-hand (RH) MLG retraction 

actuators and replacement if necessary. 

We are issuing this AD to address the 

unsafe condition on these products. 

DATES: This AD is effective September 

21, 2018. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of September 21, 2018. 

ADDRESSES: For service information 

identified in this final rule, contact 

Fokker Services B.V., Technical 

Services Dept., P.O. Box 1357, 2130 EL 

Hoofddorp, the Netherlands; telephone 

+31 (0)88–6280–350; fax +31 (0)88– 

6280–111; email technicalservices@

fokker.com; internet http://

www.myfokkerfleet.com. You may view 

this service information at the FAA, 

Transport Standards Branch, 2200 

South 216th St., Des Moines, WA. For 

information on the availability of this 

material at the FAA, call 206–231–3195. 

It is also available on the internet at 

http://www.regulations.gov by searching 

for and locating Docket No. FAA–2018– 

0303. 

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– 

0303; 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 final rule, 

the regulatory evaluation, any 

comments received, and other 

information. The address for Docket 

Operations (phone: 800–647–5527) is in 

the ADDRESSES section. Comments will 

be available in the AD docket shortly 

after receipt. 

FOR FURTHER INFORMATION CONTACT: 

Tom Rodriguez, Aerospace Engineer, 

International Section, Transport 

Standards Branch, FAA, 2200 South 

216th St., Des Moines, WA 98198; 

telephone and fax 206–231–3226. 

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 certain Fokker Services B.V. 

Model F28 Mark 0070 and 0100 

airplanes. The NPRM published in the 

Federal Register on April 27, 2018 (83 

FR 18488). The NPRM was prompted by 

a report that the retraction actuator eyeend of a Goodrich MLG failed. The 

NPRM proposed to require a one-time 

general visual inspection of the LH and 

RH MLG retraction actuators and 

replacement if necessary. 

We are issuing this AD to address 

failure of the retraction actuator eye-end 

of a Goodrich MLG, which could 

prevent retraction of the MLG and/or its 

complete extension, possibly resulting 

in damage to the airplane during 

landing, and consequent injury to 

occupants. 

The European Aviation Safety Agency 

(EASA), which is the Technical Agent 

for the Member States of the European 

Union, has issued EASA AD 2018–0001, 

dated January 4, 2018 (referred to after 

this as the Mandatory Continuing 

Airworthiness Information, or ‘‘the 

MCAI’’), to correct an unsafe condition 

for certain Fokker Services B.V. Model 

F28 Mark 0070 and 0100 airplanes. The 

MCAI states: 

An occurrence was reported where, 

following take-off after gear up selection, the 

retraction actuator eye-end (P/N [part 

number] 41518–3) of a Goodrich MLG failed. 

After the LG UNSAFE indication, the flight 

crew successfully selected gear down and 

locked by applying the alternate extension 


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40960 Federal Register / Vol. 83, No. 160 / Friday, August 17, 2018 / Rules and Regulations 

procedure, and an uneventful landing was 

made. Investigation results showed that the 

final overload fracture of the eye-end was 

preceded by fatigue cracks, believed to have 

been caused by interference between the 

MLG retraction actuator eye-end and the 

actuator bracket. It was also highlighted that 

the affected eye-end had been installed 

incorrectly, i.e. with the grease nipple 

located on the lower side, thus causing 

damage to the eye-end due to interference 

with the bracket. Further investigations 

revealed other occurrences of interference 

between retraction actuator eye-end and 

bracket with resulting damage. 

This condition, if not detected and 

corrected, could prevent retraction of the 

MLG and/or its complete extension, possibly 

resulting in damage to the aeroplane during 

landing, and consequent injury to occupants. 

To address this potential unsafe condition, 

Fokker Services published SBF100–32–168 

to provide inspection and replacement 

instructions. 

For the reasons described above, this AD 

requires a one-time [general visual] 

inspection [for deficiencies] (check the eyeend for presence of interference/damage and 

for orientation of the greasing nipple) of the 

MLG retraction actuators, left-hand (LH) and 

right-hand (RH) sides, and, depending on 

findings, replacement. 

You may examine the MCAI in the 

AD docket on the internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2018– 

0303. 

Comments 

We gave the public the opportunity to 

participate in developing this final rule. 

We received no comments on the NPRM 

or on the determination of the cost to 

the public. 

Conclusion 

We reviewed the relevant data and 

determined that air safety and the 

public interest require adopting this 

final rule 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 

addressing the unsafe condition; and 

• Do not add any additional burden 

upon the public than was already 

proposed in the NPRM. 

Related Service Information Under 1 

CFR Part 51 

Fokker Services B.V. has issued 

Fokker Service Bulletin SBF100–32– 

168, dated May 22, 2017. This service 

information describes procedures for a 

one-time general visual inspection for 

deficiencies of the Goodrich MLG 

retraction actuators and replacement of 

the actuator if necessary (e.g., if the 

retraction actuator greasing nipple is not 

located on the upper side MLG 

retraction actuator eye-end or if 

interference damage or evidence of 

removed damage is present on the eyeend of the MLG retraction actuator). 

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 5 

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 ...... 1 work-hour × $85 per hour = $85 per inspection cycle.$0 $85 per inspection cycle ........... $425 per inspection cycle. 

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 .................................... 1 work-hour × $85 per hour = $85 ............................................................ $0 $85 

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 transport category 

airplanes and associated appliances to 

the Director of the System Oversight 

Division. 

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 

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 


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Federal Register / Vol. 83, No. 160 / Friday, August 17, 2018 / Rules and Regulations 40961 

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): 

2018–17–06 Fokker Services B.V.: 

Amendment 39–19360; Docket No. 

FAA–2018–0303; Product Identifier 

2018–NM–006–AD. 

(a) Effective Date 

This AD is effective September 21, 2018. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to Fokker Services B.V. 

Model F28 Mark 0070 and 0100 airplanes, 

certificated in any category, all serial 

numbers, if equipped with Goodrich main 

landing gear (MLG), part number (P/N) 

41050-x (all dashes) or P/N 41060-x (all 

dashes). 

(d) Subject 

Air Transport Association (ATA) of 

America Code 32, Landing gear. 

(e) Reason 

This AD was prompted by a report that the 

retraction actuator eye-end of a Goodrich 

MLG failed. We are issuing this AD to 

address failure of the retraction actuator eyeend of a Goodrich MLG, which could prevent 

retraction of the MLG and/or its complete 

extension, possibly resulting in damage to 

the airplane during landing, and consequent 

injury to occupants. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Definition 

For the purposes of this AD, a ‘‘serviceable 

part’’ is a serviceable retraction actuator with 

an eye-end that does not have any indication 

of interference or damage, as specified in the 

Accomplishment Instructions of Fokker 

Service Bulletin SBF100–32–168, dated May 

22, 2017. 

(h) Inspection and Corrective Action 

Within 12 months after the effective date 

of this AD, perform a general visual 

inspection of the left-hand (LH) and righthand (RH) MLG retraction actuators for 

deficiencies (i.e., check for the presence of 

interference damage, including evidence of 

removed damage, and for the orientation of 

the greasing nipple), in accordance with the 

Accomplishment Instructions of Fokker 

Service Bulletin SBF100–32–168, dated May 

22, 2017. If any deficiency is found, before 

further flight, replace the affected MLG 

retraction actuator with a serviceable part, in 

accordance with the Accomplishment 

Instructions of Fokker Service Bulletin 

SBF100–32–168, dated May 22, 2017. 

(i) Other FAA AD Provisions 

The following provisions also apply to this 

AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, International 

Section, Transport Standards 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 International Section, send it 

to the attention of the person identified in 

paragraph (j)(2) of this AD. Information may 

be emailed to: 9-ANM-116-AMOCREQUESTS@faa.gov. 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. 

(2) Contacting the Manufacturer: For any 

requirement in this AD to obtain corrective 

actions from a manufacturer, the action must 

be accomplished using a method approved 

by the Manager, International Section, 

Transport Standards Branch, FAA; or the 

European Aviation Safety Agency (EASA); or 

Fokker Services B.V.’s EASA Design 

Organization Approval (DOA). If approved by 

the DOA, the approval must include the 

DOA-authorized signature. 

(j) Related Information 

(1) Refer to Mandatory Continuing 

Airworthiness Information (MCAI) EASA AD 

2018–0001, dated January 4, 2018, for related 

information. This MCAI may be found in the 

AD docket on the internet at http://

www.regulations.gov by searching for and 

locating Docket No. FAA–2018–0303. 

(2) For more information about this AD, 

contact Tom Rodriguez, Aerospace Engineer, 

International Section, Transport Standards 

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

Moines, WA 98198; telephone and fax 206– 

231–3226. 

(k) 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 this AD specifies otherwise. 

(i) Fokker Service Bulletin SBF100–32– 

168, dated May 22, 2017. 

(ii) Reserved. 

(3) For service information identified in 

this AD, contact Fokker Services B.V., 

Technical Services Dept., P.O. Box 1357, 

2130 EL Hoofddorp, the Netherlands; 

telephone +31 (0)88–6280–350; fax +31 

(0)88–6280–111; email technicalservices@

fokker.com; internet http://www.myfokker

fleet.com. 

(4) You may view this service information 

at the FAA, Transport Standards Branch, 

2200 South 216th St., Des Moines, WA. For 

information on the availability of this 

material at the FAA, call 206–231–3195. 

(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 Des Moines, Washington, on 

August 7, 2018. 

Michael Kaszycki, 

Acting Director, System Oversight Division, 

Aircraft Certification Service. 

[FR Doc. 2018–17624 Filed 8–16–18; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2018–0259; Product 

Identifier 2018–NE–09–AD; Amendment 39– 

19358; AD 2018–17–04] 

RIN 2120–AA64 

Airworthiness Directives; Rolls-Royce 

Corporation Engines 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 

Rolls-Royce Corporation (RRC) AE 

2100D2A and AE 2100D3 model 

turboprop engines and AE 3007A2 

model turbofan engines. This AD was 

prompted by the possibility of a lowcycle fatigue failure on certain turbine 

wheels. This AD requires removing the 

affected turbine wheels at the next 

engine shop visit or before reaching the 

new reduced life limit, whichever 

occurs first, and replacing them with 

parts eligible for installation. We are 

issuing this AD to address the unsafe 

condition on these products. 

DATES: This AD is effective September 

21, 2018. 

The Director of the Federal Register 

approved the incorporation by reference 


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