Federal Register / Vol. 79, No. 87 / Tuesday, May 6, 2014 / Proposed Rules 25753 

may be evidence that a creditor 

originated a loan in good faith as a 

qualified mortgage: 

A. A creditor maintains and follows 

policies and procedures designed to 

ensure that points and fees are correctly 

calculated and do not exceed the 

applicable limit under § 1026.43(e)(3)(i); 

or 

B. The pricing for the loan is 

consistent with pricing on qualified 

mortgages originated 

contemporaneously by the same 

creditor. 

ii. In contrast, the following may be 

evidence that a loan was not originated 

in good faith as a qualified mortgage: 

A. A creditor does not maintain, or 

the creditor has, but does not follow, 

policies and procedures designed to 

ensure that points and fees are correctly 

calculated and do not exceed the 

applicable limit under § 1026.43(e)(3)(i); 

or 

B. The pricing for the loan is not 

consistent with pricing on qualified 

mortgages originated 

contemporaneously by the same 

creditor. 

2. Policies and procedures for postconsummation review and refunding. A 

creditor or assignee satisfies 

§ 1026.43(e)(3)(iii)(C) if it maintains and 

follows policies and procedures for 

post-consummation quality control loan 

review and for curing (by providing a 

refund) errors in points and fees 

calculations that occur at or before 

consummation. 

* * * * * 

Dated: April 30, 2014. 

Richard Cordray, 

Director, Bureau of Consumer Financial 

Protection. 

[FR Doc. 2014–10207 Filed 5–5–14; 8:45 am] 

BILLING CODE 4810–AM–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2014–0292; Directorate 

Identifier 2014–CE–011–AD] 

RIN 2120–AA64 

Airworthiness Directives; GROBWERKE GMBH & CO KG and 

BURKHART GROB LUFT- UND 

RAUMFAHRT GmbH & CO KG Gliders 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: We propose to adopt a new 

airworthiness directive (AD) for GROBWERKE GMBH & CO KG Models G102 

STANDARD ASTIR III, G102 CLUB 

ASTIR III, and G102 CLUB ASTIR IIIb 

gliders and BURKHART GROB LUFTUND RAUMFAHRT GmbH & CO KG 

Models G103 TWIN II, G103A TWIN II 

ACRO, G103C TWIN III ACRO, and G 

103 C Twin III SL gliders. This proposed 

AD results from 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 plastic control cable 

pulleys developing cracks due to aging. 

We are issuing this proposed AD to 

require actions to address the unsafe 

condition on these products. 

DATES: We must receive comments on 

this proposed AD by June 20, 2014. 

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 proposed AD, contact FiberglasTechnik Rudolf Lindner GmbH & Co. 

KG, Steige 3, D–88487 Walpertshofen, 

Germany; telephone: +49 (0) 7353/22 

43; fax: +49 (0) 7353/30 96; email: 

info@LTB-Lindner.com; Web site: 

http://www.ltb-lindner.com/ 

home.104.html. You may review this 

referenced 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. 

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–2014– 

0292; 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 proposed 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: Jim 

Rutherford, Aerospace Engineer, FAA, 

Small Airplane Directorate, 901 Locust, 

Room 301, Kansas City, Missouri 64106; 

telephone: (816) 329–4165; fax: (816) 

329–4090; email: 

jim.rutherford@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Comments Invited 

We invite you to send any written 

relevant data, views, or arguments about 

this proposed AD. Send your comments 

to an address listed under the 

ADDRESSES section. Include ‘‘Docket No. 

FAA–2014–0292; Directorate Identifier 

2014–CE–011–AD’’ at the beginning of 

your comments. We specifically invite 

comments on the overall regulatory, 

economic, environmental, and energy 

aspects of this proposed AD. We will 

consider all comments received by the 

closing date and may amend this 

proposed AD because of those 

comments. 

We will post all comments we 

receive, without change, to http:// 

regulations.gov, including any personal 

information you provide. We will also 

post a report summarizing each 

substantive verbal contact we receive 

about this proposed AD. 

Discussion 

The European Aviation Safety Agency 

(EASA), which is the Technical Agent 

for the Member States of the European 

Community, has issued AD No.: 2014– 

0067, dated March 18, 2014 (referred to 

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

unsafe condition for the specified 

products. The MCAI states: 

Control cable pulleys made from plastic 

(white or brown material) in the rudder 

control unit were reported to develop cracks 

due to aging. In one case, jamming of the 

rudder control unit was reported. 

This condition, if not detected and 

corrected, could cause cable pulleys to break, 

potentially jamming the rudder control unit 

and resulting in loss of control of the 

sailplane. 

To address this potential unsafe condition, 

Fiberglas-Technik issued Technische 

Mitteilung/Service Bulletin TM–G05/SB–G05 

and Anweisung/Instructions A/I–G05 (one 

document) to provide instructions for the 

replacement of plastic cable pulleys with 

pulleys made from aluminium. 

For the reason described above, this AD 

requires identification and replacement of 

plastic cable pulleys in the rudder control 

unit. 


sroberts on DSK5SPTVN1PROD with PROPOSALS
25754 Federal Register / Vol. 79, No. 87 / Tuesday, May 6, 2014 / Proposed Rules 

Plastic cable pulleys may also be installed 

in the cable circuits of pedal adjustment and/ 

or tow hook actuation, their replacement is 

not required by this AD. 

You may examine the MCAI on the 

Internet at http://www.regulations.gov 

by searching for and locating Docket No. 

FAA–2014–0292. 

Relevant Service Information 

Fiberglas-Technik Rudolf Lindner 

GmbH & Co. KG has issued Service 

Bulletin SB–G05, dated January 17, 

2014; and Instructions A/I–G05, dated 

January 17, 2014. The actions described 

in this service information are intended 

to correct the unsafe condition 

identified in the MCAI. 

FAA’s Determination and Requirements 

of the Proposed 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 proposing this 

AD because we evaluated all 

information and determined the unsafe 

condition exists and is likely to exist or 

develop on other products of the same 

type design. 

Costs of Compliance 

We estimate that this proposed AD 

will affect 118 products of U.S. registry. 

We also estimate that it would take 

about .5 work-hour per product to 

comply with the basic requirements of 

this proposed AD. The average labor 

rate is $85 per work-hour. 

Based on these figures, we estimate 

the cost of the proposed AD on U.S. 

operators to be $5,015, or $42.50 per 

product. 

In addition, we estimate that any 

necessary follow-on actions would take 

about 2 work-hours and require parts 

costing $244, for a cost of $414 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 proposed AD 

would not have federalism implications 

under Executive Order 13132. This 

proposed AD would not have a 

substantial direct effect on the States, on 

the relationship between the national 

Government and the States, or on the 

distribution of power and 

responsibilities among the various 

levels of government. 

For the reasons discussed above, I 

certify this proposed regulation: 

(1) Is not a ‘‘significant regulatory 

action’’ under Executive Order 12866, 

(2) Is not a ‘‘significant rule’’ under 

the DOT Regulatory Policies and 

Procedures (44 FR 11034, February 26, 

1979), 

(3) Will not affect intrastate aviation 

in Alaska, and 

(4) Will not have a significant 

economic impact, positive or negative, 

on a substantial number of small entities 

under the criteria of the Regulatory 

Flexibility Act. 

List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation 

safety, Incorporation by reference, 

Safety. 

The Proposed Amendment 

Accordingly, under the authority 

delegated to me by the Administrator, 

the FAA proposes to amend 14 CFR part 

39 as follows: 

PART 39—AIRWORTHINESS 

DIRECTIVES 

■ 1. The authority citation for part 39 

continues to read as follows: 

Authority: 49 U.S.C. 106(g), 40113, 44701. 

§ 39.13 [Amended] 

■ 2. The FAA amends § 39.13 by adding 

the following new AD: 

GROB-WERKE GMBH & CO KG and 

BURKHART GROB LUFT-UND 

RAUMFAHRT GmbH & CO KG: Docket 

No. FAA–2014–0292; Directorate 

Identifier 2014–CE–011–AD. 

(a) Comments Due Date 

We must receive comments by June 20, 

2014. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to GROB-WERKE GMBH 

& CO KG Models G102 STANDARD ASTIR 

III, G102 CLUB ASTIR III, and G102 CLUB 

ASTIR IIIb gliders and BURKHART GROB 

LUFT-UND RAUMFAHRT GmbH & CO KG 

Models G103 TWIN II, G103A TWIN II 

ACRO, G103C TWIN III ACRO and Model G 

103 C Twin III SL gliders with the following 

serial numbers (S/N), certificated in any 

category. 

(1) G102 STANDARD ASTIR III, S/N 5501 

through 5652. 

(2) G102 CLUB ASTIR III, S/N 5501 

through 5652. 

(3) G102 CLUB ASTIR IIIb, S/N 5501 

through 5652. 

(4) G103 TWIN II, S/N 3730 through 34078. 

(5) G103A TWIN II ACRO, S/N 3730 

through 34078. 

(6) G103C TWIN III ACRO, S/N 34101 

through 34203. 

(7) G 103 C Twin III SL, S/N 35002 through 

35051. 

(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 plastic 

control cable pulleys developing cracks due 

to aging. We are issuing this proposed AD to 

detect and correct plastic control cable 

pulleys in the rudder control unit, which 

could lead to breaking of the pulley and 

potentially jamming the rudder control unit, 

possibly resulting in loss of control of the 

glider. 

(f) Actions and Compliance 

Comply with this AD within the 

compliance times specified in paragraphs 

(f)(1) through (f)(3) of this AD, unless already 

done. 

(1) For all Models G103C TWIN III ACRO 

and G 103 C Twin III SL gliders: Within 3 

months after the effective date of this AD, 

inspect the rudder control unit for 

installation of plastic cable pulleys. If plastic 

cable pulleys are installed, before further 

flight, replace the plastic cable pulleys with 

aluminum cable pulleys following the 

actions and instructions of Fiberglas-Technik 

Rudolf Lindner GmbH & Co. KG Service 

Bulletin SB–G05 and Fiberglas-Technik 

Rudolf Lindner GmbH & Co. KG Instructions 

A/I–G05, both dated January 17, 2014. 

(2) For all Models G102 STANDARD 

ASTIR III, G102 CLUB ASTIR III, G102 CLUB 

ASTIR IIIb, G103 TWIN II, and G103A TWIN 

II ACRO gliders: Within 1 month after the 

effective date of this AD, inspect the rudder 

control unit for installation of plastic cable 

pulleys. If plastic cable pulleys are installed, 

before further flight, replace the plastic cable 

pulleys with aluminum cable pulleys 

following the actions and instructions of 


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Federal Register / Vol. 79, No. 87 / Tuesday, May 6, 2014 / Proposed Rules 25755 

Fiberglas-Technik Rudolf Lindner GmbH & 

Co. KG Service Bulletin SB–G05 and 

Fiberglas-Technik Rudolf Lindner GmbH & 

Co. KG Instructions A/I–G05, both dated 

January 17, 2014. 

(3) As of the effective date of this AD, do 

not install any plastic control cable pulley in 

the rudder control unit of any glider 

identified in paragraphs (c)(1) through (c)(7) 

of this AD. 

(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: Jim Rutherford, Aerospace Engineer, 

FAA, Small Airplane Directorate, 901 Locust, 

Room 301, Kansas City, Missouri 64106; 

telephone: (816) 329–4165; fax: (816) 329– 

4090; email: jim.rutherford@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. 

(h) Related Information 

Refer to European Aviation Safety Agency 

(EASA) AD No.: 2014–0067, dated March 18, 

2014, for related information. You may 

examine the MCAI on the Internet at 

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

and locating Docket No. FAA–2014–0292. 

For service information related to this AD, 

contact Fiberglas-Technik Rudolf Lindner 

GmbH & Co. KG, Steige 3, D–88487 

Walpertshofen, Germany; telephone: +49 (0) 

7353/22 43; fax: +49 (0) 7353/30 96; email: 

info@LTB-Lindner.com; Web site: http:// 

www.ltb-lindner.com/home.104.html. You 

may review this referenced 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. 

Issued in Kansas City, Missouri, on April 

30, 2014. 

Earl Lawrence, 

Manager, Small Airplane Directorate, Aircraft 

Certification Service. 

[FR Doc. 2014–10308 Filed 5–5–14; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 71 

[Docket No FAA–2014–0198 Airspace 

Docket No. 14–AGL–8] 

Proposed Amendment of Class E 

Airspace; South Dakota 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: This action proposes to 

amend Class E airspace extending 

upward from 1,200 feet above the 

surface within the boundary of the state 

of South Dakota. With the increased use 

of GPS/GNSS navigation systems, pilots 

routinely file and fly flight plans using 

point-to-point routes instead of 

published airways. Often, these pointto-point routes take aircraft through 

uncontrolled airspace (Class G). With 

this proposal, Minneapolis Air Route 

Traffic Control Center (ARTCC) would 

provide more expeditious service and 

increased efficiency within the National 

Airspace System. 

DATES: Comments must be received on 

or before June 20, 2014. 

ADDRESSES: Send comments on this 

proposal to the U.S. Department of 

Transportation, Docket Operations, 1200 

New Jersey Avenue SE., West Building 

Ground Floor, Room W12–140, 

Washington, DC 20590–0001. You must 

identify the docket number FAA–2014– 

0198/Airspace Docket No. 14–AGL–8, at 

the beginning of your comments. You 

may also submit comments through the 

Internet at http://www.regulations.gov. 

You may review the public docket 

containing the proposal, any comments 

received, and any final disposition in 

person in the Dockets Office between 

9:00 a.m. and 5:00 p.m., Monday 

through Friday, except Federal holidays. 

The Docket Office (telephone 1–800– 

647–5527), is on the ground floor of the 

building at the above address. 

FOR FURTHER INFORMATION CONTACT: Raul 

Garza, Jr., Central Service Center, 

Operations Support Group, Federal 

Aviation Administration, Southwest 

Region, 2601 Meacham Blvd., Fort 

Worth, TX 76137; telephone: 817–321– 

7654. 

SUPPLEMENTARY INFORMATION: 

Comments Invited 

Interested parties are invited to 

participate in this proposed rulemaking 

by submitting such written data, views, 

or arguments, as they may desire. 

Comments that provide the factual basis 

supporting the views and suggestions 

presented are particularly helpful in 

developing reasoned regulatory 

decisions on the proposal. Comments 

are specifically invited on the overall 

regulatory, aeronautical, economic, 

environmental, and energy-related 

aspects of the proposal. 

Communications should identify both 

docket numbers and be submitted in 

triplicate to the address listed above. 

Commenters wishing the FAA to 

acknowledge receipt of their comments 

on this notice must submit with those 

comments a self-addressed, stamped 

postcard on which the following 

statement is made: ‘‘Comments to 

Docket No. FAA–2014–0198/Airspace 

Docket No. 14–AGL–8.’’ The postcard 

will be date/time stamped and returned 

to the commenter. 

Availability of NPRMs 

An electronic copy of this document 

may be downloaded through the 

Internet at http://www.regulations.gov. 

Recently published rulemaking 

documents can also be accessed through 

the FAA’s Web page at http:// 

www.faa.gov/airports_airtraffic/ 

air_traffic/publications/ 

airspace_amendments/. 

You may review the public docket 

containing the proposal, any comments 

received and any final disposition in 

person in the Dockets Office (see 

ADDRESSES section for address and 

phone number) between 9:00 a.m. and 

5:00 p.m., Monday through Friday, 

except Federal holidays. An informal 

docket may also be examined during 

normal business hours at the office of 

the Central Service Center, 2601 

Meacham Blvd., Fort Worth, TX 76137. 

Persons interested in being placed on 

a mailing list for future NPRMs should 

contact the FAA’s Office of Rulemaking 

(202) 267–9677, to request a copy of 

Advisory Circular No. 11–2A, Notice of 

Proposed Rulemaking Distribution 

System, which describes the application 

procedure. 

The Proposal 

This action proposes to amend Title 

14, Code of Federal Regulations (14 

CFR), Part 71 by amending Class E 

airspace extending upward from 1,200 

feet above the surface within the state of 

South Dakota. This action would enable 

Minneapolis ARTCC to have greater 

latitude to use radar vectors and/or 

altitude changes that would provide a 

more efficient use of airspace within the 

NAS. 

Class E airspace areas are published 

in Paragraph 6005 of FAA Order 

7400.9X, dated August 7, 2013 and 


sroberts on DSK5SPTVN1PROD with PROPOSALS