Federal Register / Vol. 80, No. 158 / Monday, August 17, 2015 / Rules and Regulations 49127 

PARTS 10003–10049—[RESERVED] 

Dated: August 11, 2015. 

Rebecca Cokley, 

Executive Director. 

[FR Doc. 2015–20140 Filed 8–14–15; 8:45 am] 

BILLING CODE 8421–03–P 

BUREAU OF CONSUMER FINANCIAL 

PROTECTION 

12 CFR Part 1010 

Compliance Bulletin—Amendment to 

the Interstate Land Sales Full 

Disclosure Act 

AGENCY: Bureau of Consumer Financial 

Protection. 

ACTION: Compliance bulletin. 

SUMMARY: The Bureau of Consumer 

Financial Protection is issuing a 

compliance bulletin titled ‘‘Amendment 

to the Interstate Land Sales Full 

Disclosure Act’’ to provide information 

to developers and other interested 

parties relating to a recent Congressional 

amendment to the Interstate Land Sales 

Full Disclosure Act. 

DATES: This bulletin is applicable 

August 17, 2015. 

FOR FURTHER INFORMATION CONTACT: 

Amanda Quester, Senior Counsel, Office 

of Regulations, at (202) 435–7700. 

SUPPLEMENTARY INFORMATION: 

I. Compliance Bulletin 

The Consumer Financial Protection 

Bureau (Bureau) issues this compliance 

bulletin to provide information to 

developers and other interested parties 

relating to Public Law 113–167, 128 

Stat. 1882 (2014), which amended the 

Interstate Land Sales Full Disclosure 

Act (ILSA). This ILSA amendment was 

signed by the President on September 

26, 2014. It became effective on March 

25, 2015, and is codified primarily at 15 

U.S.C. 1702(b)(9) and (d). 

The amendment exempts from ILSA’s 

registration and disclosure requirements 

the sale or lease of a condominium unit 

that is not exempt under 15 U.S.C. 

1702(a). Under 15 U.S.C. 1702(d), a 

‘‘condominium unit’’ is defined for 

purposes of this new exemption as a 

unit of residential or commercial 

property to be designated for separate 

ownership pursuant to a condominium 

plan or declaration provided that upon 

conveyance: (1) The owner of such unit 

will have sole ownership of the unit and 

an undivided interest in the common 

elements appurtenant to the unit; and 

(2) the unit will be an improved lot. 

Pursuant to § 1010.4(d) of the 

Bureau’s ILSA regulations, eligibility for 

an exemption under 15 U.S.C. 1702, 

including the exemption of section 

1702(b)(9), is self-determining, and a 

developer is not required to file notice 

with or obtain the approval of the 

Bureau in order to take advantage of an 

exemption. Section 1010.4(d) also 

provides that a developer is responsible 

for maintaining records to demonstrate 

that the requirements of an exemption 

have been met if a developer elects to 

take advantage of an exemption. The 

Bureau will continue to process filings 

made by developers seeking to fulfill 

their obligations under ILSA and its 

implementing regulations. 

If you have questions about ILSA 

program operations, you may contact 

ILSA program staff via email to CFPB_

ILS_Inquiries@cfpb.gov or at the address 

below: Consumer Financial Protection 

Bureau, Interstate Land Sales Program, 

1700 G St. NW., Attn: 1625 Eye St., 

Room 3093, Washington, DC 20552. 

If you have a question regarding the 

interpretation of ILSA or the Bureau’s 

implementing regulations, please email 

CFPB_reginquiries@cfpb.gov with your 

specific question, including reference to 

the applicable regulation section(s). 

Bureau staff responding to queries 

cannot provide legal advice and are not 

authorized to provide official 

interpretations of ILSA or of the 

Bureau’s implementing regulations. 

II. Regulatory Requirements 

This Compliance Bulletin summarizes 

existing requirements under the law, 

and does not itself establish any binding 

obligations. It is therefore exempt from 

notice and comment rulemaking 

requirements under the Administrative 

Procedure Act pursuant to 5 U.S.C. 

553(b). Because no notice of proposed 

rulemaking is required, the Regulatory 

Flexibility Act does not require an 

initial or final regulatory flexibility 

analysis. 5 U.S.C. 603(a), 604(a). The 

Bureau has determined that this 

Compliance Bulletin does not impose 

any new or revise any existing 

recordkeeping, reporting, or disclosure 

requirements on covered entities or 

members of the public that would be 

collections of information requiring 

OMB approval under the Paperwork 

Reduction Act, 44 U.S.C. 3501 et seq. 

Dated: August 10, 2015. 

Richard Cordray, 

Director, Bureau of Consumer Financial 

Protection. 

[FR Doc. 2015–19998 Filed 8–14–15; 8:45 am] 

BILLING CODE 4810–AM–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2015–3398; Directorate 

Identifier 2015–CE–031–AD; Amendment 

39–18232; AD 2015–16–07] 

RIN 2120–AA64 

Airworthiness Directives; REIMS 

AVIATION S.A. Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; request for 

comments. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for REIMS 

AVIATION S.A. Model F406 airplanes. 

This AD results from mandatory 

continuing airworthiness information 

(MCAI) issued by the aviation authority 

of another country to identify and 

correct an unsafe condition on an 

aviation product. The MCAI describes 

the unsafe condition as detachment of 

the pilot’s rudder control pedal in flight. 

We are issuing this AD to require 

actions to address the unsafe condition 

on these products. 

DATES: This AD is effective August 18, 

2015. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in the AD 

as of August 18, 2015. 

We must receive comments on this 

AD by October 1, 2015. 

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. 

• 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: U.S. Department of 

Transportation, Docket Operations, M– 

30, West Building Ground Floor, Room 

W12–140, 1200 New Jersey Avenue SE., 

Washington, DC 20590, between 9 a.m. 

and 5 p.m., Monday through Friday, 

except Federal holidays. 

For service information identified in 

this AD, contact ASI Aviation, 

Ae ́rodrome de Reims Prunay, 51360 

Prunay, FRANCE; phone: +33 3 26 48 46 

65; fax: +33 3 26 49 18 57; email: none; 

Internet: http://asi-aviation.fr/asiaviation-support/1.html (requires user 

name and password). You may view this 

referenced service information at the 

FAA, Small Airplane Directorate, 901 


tkelley on DSK3SPTVN1PROD with RULES
49128 Federal Register / Vol. 80, No. 158 / Monday, August 17, 2015 / Rules and Regulations 

Locust, Kansas City, Missouri 64106. 

For information on the availability of 

this material at the FAA, call (816) 329– 

4148. It is also available on the Internet 

at http://www.regulations.gov by 

searching for locating Docket No. FAA– 

2015–3398. 

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– 

3398; 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 street address for 

the Docket Office (telephone (800) 647– 

5527) is in the ADDRESSES section. 

Comments will be available in the AD 

docket shortly after receipt. 

FOR FURTHER INFORMATION CONTACT: 

Albert J. Mercado, Aerospace Engineer, 

FAA, Small Airplane Directorate, 901 

Locust, Room 301, Kansas City, 

Missouri 64106; telephone: (816) 329– 

4119; fax: (816) 329–4090; email: 

albert.mercado@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Discussion 

The European Aviation Safety Agency 

(EASA), which is the Technical Agent 

for the Member States of the European 

Community, has issued AD No.: 2015– 

0159–E, dated July 31, 2015 (referred to 

after this as ‘‘the MCAI’’), to correct an 

unsafe condition for the specified 

products. The MCAI states: 

An occurrence was reported where one 

pilot rudder control pedal of an F 406 

aeroplane detached in flight. No change in 

aeroplane attitude occurred. The rudder was 

controlled using the co-pilot rudder pedals, 

and the flight continued uneventfully until a 

safe landing was performed. 

This condition, if not detected and 

corrected, could result in loss of directional 

control of the aeroplane. 

To address this unsafe condition, ASI 

Aviation issued Service Bulletin (SB) F406– 

104 to provide inspection instructions. 

For the reason described above, this AD 

requires inspection of the rudder control 

pedal torque tubes, both left-hand (LH) and 

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

replacement with a serviceable part. 

This AD also requires inspection before 

new installation of rudder control pedal 

torque tubes. 

You may examine the MCAI on the 

Internet at http://www.regulations.gov 

by searching for and locating Docket No. 

FAA–2015–3398. 

Related Service Information Under 1 

CFR Part 51 

ASI AVIATION has issued Service 

Bulletin No.: F406–104, dated July 28, 

2015. The actions described in this 

service information are intended to 

correct the unsafe condition identified 

in the MCAI. The service information 

describes procedures for inspection of 

the left-hand and right-hand rudder 

control pedal torque tubes, and, 

depending on findings, replacement 

with a serviceable part. 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 of this AD. 

FAA’s Determination and Requirements 

of the AD 

This product has been approved by 

the aviation authority of another 

country, and is approved for operation 

in the United States. Pursuant to our 

bilateral agreement with this State of 

Design Authority, they have notified us 

of the unsafe condition described in the 

MCAI and service information 

referenced above. We are issuing this 

AD because we evaluated all 

information provided by the State of 

Design Authority and determined the 

unsafe condition exists and is likely to 

exist or develop on other products of the 

same type design. 

FAA’s Determination of the Effective 

Date 

An unsafe condition exists that 

requires the immediate adoption of this 

AD. The FAA has found that the risk to 

the flying public justifies waiving notice 

and comment prior to adoption of this 

rule because detachment of the pilot 

rudder control pedal in flight could 

result in loss of airplane directional 

control. Therefore, we determined that 

notice and opportunity for public 

comment before issuing this AD are 

impracticable and that good cause exists 

for making this amendment effective in 

fewer than 30 days. 

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–2015–3398; 

Directorate Identifier 2015–CE–031– 

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 we receive 

about this AD. 

Costs of Compliance 

We estimate that this AD will affect 7 

products of U.S. registry. We also 

estimate that it will take about 5 workhours per product to comply with the 

basic requirements of this AD. The 

average labor rate is $85 per work-hour. 

Based on these figures, we estimate 

the cost of the AD on U.S. operators to 

be $2,975, or $425 per product. 

In addition, we estimate that any 

necessary follow-on actions would take 

about 20 work-hours and require parts 

costing $10,000, for a cost of $11,700 

per product. We have no way of 

determining the number of products 

that may need these actions. 

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 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, 


tkelley on DSK3SPTVN1PROD with RULES
Federal Register / Vol. 80, No. 158 / Monday, August 17, 2015 / Rules and Regulations 49129 

(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. 

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 AD: 

2015–16–07 REIMS AVIATION S.A.: 

Amendment 39–18232; Docket No. 

FAA–2015–3398; Directorate Identifier 

2015–CE–031–AD. 

(a) Effective Date 

This airworthiness directive (AD) becomes 

effective August 18, 2015. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to Reims Aviation S.A. 

Model F406 airplanes, serial numbers 0001 

through 0098, certificated in any category. 

(d) Subject 

Air Transport Association of America 

(ATA) Code 27: Flight Controls. 

(e) Reason 

This AD was prompted by mandatory 

continuing airworthiness information (MCAI) 

originated 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 detachment 

of the pilot’s rudder control pedal in flight. 

We are issuing this AD to detect and correct 

cracking of the pilot rudder control pedal 

which, if not corrected, could result in 

detachment of the pedal with possible loss of 

airplane directional control. 

(f) Actions and Compliance 

Unless already done, do the actions in 

paragraphs (f)(1) through (f)(4) of this AD. 

(1) Before further flight after August 18, 

2015 (the effective date of this AD), do a 

visual inspection and a dye or fluorescent 

penetrant inspection of the rudder control 

pedal torque tubes, LH (Part Number (P/N) 

5115260–1) and RH (P/N 5115260–2), 

following the instructions of PART A of ASI 

AVIATION Service Bulletin No.: F406–104, 

dated July 28, 2015. 

(2) If no crack is detected during the 

inspection required by paragraph (f)(1) of this 

AD, within 100 hours time-in-service (TIS) 

after August 18, 2015 (the effective date of 

this AD), do a magnetic particle inspection of 

the rudder control pedal torque tubes, LH (P/ 

N 5115260–1) and RH (P/N 5115260–2), 

following the instructions of PART B of ASI 

AVIATION Service Bulletin No.: F406–104, 

dated July 28, 2015. 

(3) If any crack is detected on a rudder 

control pedal torque tube during the 

inspection required by paragraph (f)(1) or 

(f)(2) of this AD, before further flight, replace 

the affected part with a serviceable part 

following the instructions of ASI AVIATION 

Service Bulletin No.: F406–104, dated July 

28, 2015. 

(4) For the purpose of this AD, a 

serviceable part is a rudder control pedal 

torque tube that has had a magnetic particle 

inspection following the instructions of 

PART B of ASI AVIATION Service Bulletin 

No.: F406–104, dated July 28, 2015, and no 

cracks were found. 

(5) You may install a rudder control pedal 

torque tube P/N 5115260–1 (LH) or P/N 

5115260–2 (RH) on an airplane, provided it 

is a serviceable part. 

(g) Other FAA AD Provisions 

The following provisions also apply to this 

AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, Standards Office, 

FAA, has the authority to approve AMOCs 

for this AD, if requested using the procedures 

found in 14 CFR 39.19. Send information to 

ATTN: Albert J. Mercado, Aerospace 

Engineer, FAA, Small Airplane Directorate, 

901 Locust, Room 301, Kansas City, Missouri 

64106; telephone: (816) 329–4119; fax: (816) 

329–4090; email: albert.mercado@faa.gov. 

Before using any approved AMOC on any 

airplane to which the AMOC applies, notify 

your appropriate principal inspector (PI) in 

the FAA Flight Standards District Office 

(FSDO), or lacking a PI, your local FSDO. 

(2) Airworthy Product: For any requirement 

in this AD to obtain corrective actions from 

a manufacturer or other source, use these 

actions if they are FAA-approved. Corrective 

actions are considered FAA-approved if they 

are approved by the State of Design Authority 

(or their delegated agent). You are required 

to assure the product is airworthy before it 

is returned to service. 

(3) Reporting Requirements: For any 

reporting requirement in this AD, a federal 

agency may not conduct or sponsor, and a 

person is not required to respond to, nor 

shall a person be subject to a penalty for 

failure to comply with a collection of 

information subject to the requirements of 

the Paperwork Reduction Act unless that 

collection of information displays a current 

valid OMB Control Number. The OMB 

Control Number for this information 

collection is 2120–0056. Public reporting for 

this collection of information is estimated to 

be approximately 5 minutes per response, 

including the time for reviewing instructions, 

completing and reviewing the collection of 

information. All responses to this collection 

of information are mandatory. Comments 

concerning the accuracy of this burden and 

suggestions for reducing the burden should 

be directed to the FAA at: 800 Independence 

Ave. SW., Washington, DC 20591, Attn: 

Information Collection Clearance Officer, 

AES–200. 

(h) Related Information 

Refer to MCAI European Aviation Safety 

Agency (EASA) AD No.: 2015–0159–E, dated 

July 31, 2015, for related information. You 

may examine the MCAI on the Internet at 

http://www.regulations.gov by searching for 

and locating Docket No. FAA–2015–3398. 

(i) 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) ASI AVIATION Service Bulletin No.: 

F406–104, dated July 28, 2015. 

(ii) Reserved. 

(3) For service information identified in 

this AD, contact ASI Aviation, Ae ́rodrome de 

Reims Prunay, 51360 Prunay, FRANCE; 

phone: +33 3 26 48 46 65; fax: +33 3 26 49 

18 57; email: none; Internet: http://asiaviation.fr/asi-aviation-support/1.html 

(requires user name and password). 

(4) You may view this service information 

at the FAA, Small Airplane Directorate, 901 

Locust, Kansas City, Missouri 64106. For 

information on the availability of this 

material at the FAA, call (816) 329–4148. It 

is also available on the Internet at http://

www.regulations.gov by searching for 

locating Docket No. FAA–2015–3398. 

(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 Kansas City, Missouri on August 

6, 2015. 

Earl Lawrence, 

Manager, Small Airplane Directorate, Aircraft 

Certification Service. 

[FR Doc. 2015–19901 Filed 8–14–15; 8:45 am] 

BILLING CODE 4910–13–P 


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