Federal Register / Vol. 79, No. 150 / Tuesday, August 5, 2014 / Proposed Rules 45383 

EGRPRA review that is currently under 

way. As part of that review, the FDIC 

invites comments concerning whether 

the proposal would impose any 

outdated or unnecessary regulatory 

requirements on insured depository 

institutions. If you provide such 

comments, please be specific and 

provide alternatives whenever 

appropriate. 

List of Subjects in Part 390 

Banks and banking; Savings 

Associations. 

Authority and Issuance 

For the reasons stated in the preamble 

and under the authority of 12 U.S.C. 

5412, the Board of Directors of the 

Federal Deposit Insurance Corporation 

proposes to amend 12 CFR part 390 as 

follows: 

PART 390—REGULATIONS 

TRANSFERRED FROM THE OFFICE OF 

THRIFT SUPERVISION 

■ 1. The authority citation for part 390 

is revised to read as follows: 

Authority: 12 U.S.C. 1819. 

Subpart A also issued under 12 U.S.C. 

1820. 

Subpart B also issued under 12 U.S.C. 

1818. 

Subpart C also issued under 5 U.S.C. 504; 

554–557; 12 U.S.C. 1464; 1467; 1468; 1817; 

1818; 1820; 1829; 3349, 4717; 15 U.S.C. 78 

l; 78o–5; 78u–2; 28 U.S.C. 2461 note; 31 

U.S.C. 5321; 42 U.S.C. 4012a. 

Subpart D also issued under 12 U.S.C. 

1817; 1818; 1820; 15 U.S.C. 78 l. 

Subpart E also issued under 12 U.S.C. 

1813; 1831m; 15 U.S.C. 78. 

Subpart F also issued under 5 U.S.C. 552; 

559; 12 U.S.C. 2901 et seq. 

Subpart G also issued under 12 U.S.C. 2810 

et seq., 2901 et seq.; 15 U.S.C. 1691; 42 U.S.C. 

1981, 1982, 3601–3619. 

Subpart H also issued under 12 U.S.C. 

1464; 1831y. 

Subpart I also issued under 12 U.S.C. 

1831x. 

Subpart J also issued under 12 U.S.C. 

1831p–1. 

Subpart L also issued under 12 U.S.C. 

1831p–1. 

Subpart M also issued under 12 U.S.C. 

1818. 

Subpart O also issued under 12 U.S.C. 

1828. 

Subpart P also issued under 12 U.S.C. 

1470; 1831e; 1831n; 1831p–1; 3339. 

Subpart Q also issued under 12 U.S.C. 

1462; 1462a; 1463; 1464. 

Subpart R also issued under 12 U.S.C. 

1463; 1464; 1831m; 1831n; 1831p–1. 

Subpart S also issued under 12 U.S.C. 

1462; 1462a; 1463; 1464; 1468a; 1817; 1820; 

1828; 1831e; 1831o; 1831p–1; 1881–1884; 

3207; 3339; 15 U.S.C. 78b; 78 l; 78m; 78n; 

78p; 78q; 78w; 31 U.S.C. 5318; 42 U.S.C. 

4106. 

Subpart T also issued under 12 U.S.C. 

1462a; 1463; 1464; 15 U.S.C. 78c; 78 l; 78m; 

78n; 78w. 

Subpart U also issued under 12 U.S.C. 

1462a; 1463; 1464; 15 U.S.C. 78c; 78 l; 78m; 

78n; 78p; 78w; 78d–1; 7241; 7242; 7243; 

7244; 7261; 7264; 7265. 

Subpart V also issued under 12 U.S.C. 

3201–3208. 

Subpart W also issued under 12 U.S.C. 

1462a; 1463; 1464; 15 U.S.C. 78c; 78 l; 78m; 

78n; 78p; 78w. 

Subpart X also issued under 12 U.S.C. 

1462; 1462a; 1463; 1464; 1828; 3331 et seq. 

Subpart Y also issued under 12 U.S.C. 

1831o. 

Subpart Z also issued under 12 U.S.C. 

1462; 1462a; 1463; 1464; 1828 (note). 

Subpart N—[Removed and Reserved] 

■ 2. Remove and reserve subpart N, 

consisting of §§ 390.240 through 

390.241. 

Dated at Washington, DC, this 15th day of 

July, 2014. 

By order of the Board of Directors. 

Federal Deposit Insurance Corporation. 

Robert E. Feldman, 

Executive Secretary. 

[FR Doc. 2014–18262 Filed 8–4–14; 8:45 am] 

BILLING CODE 6714–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2014–0532; Directorate 

Identifier 2014–CE–016–AD] 

RIN 2120–AA64 

Airworthiness Directives; Pacific 

Aerospace Limited Airplanes 

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 Pacific 

Aerospace Limited Models FU24–954 

and FU24A–954 airplanes. 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 cracking of 

control column at the wiring access 

hole, which could lead to loss of 

control. 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 September 19, 

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 Pacific 

Aerospace Limited, Airport Road, 

Hamilton Private Bag 3027 Hamilton 

3240, New Zealand; telephone: +64 7 

843 6144; fax: +64 7 843 6134; email: 

pacific@aerospace.co.nz; Internet: 

http://www.aerospace.co.nz/. 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– 

0532; 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: Karl 

Schletzbaum, Aerospace Engineer, FAA, 

Small Airplane Directorate, 901 Locust, 

Room 301, Kansas City, Missouri 64106; 

telephone: (816) 329–4123; fax: (816) 

329–4090; email: karl.schletzbaum@

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–2014–0532; Directorate Identifier 

2014–CE–016–AD’’ at the beginning of 

your comments. We specifically invite 


emcdonald on DSK67QTVN1PROD with PROPOSALS
45384 Federal Register / Vol. 79, No. 150 / Tuesday, August 5, 2014 / Proposed Rules 

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 Civil Aviation Authority (CAA), 

which is the airworthiness authority for 

New Zealand, has issued AD DCA/

FU24/183, dated May 29, 2014 (referred 

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

an unsafe condition for Pacific 

Aerospace Limited Models FU24–954 

and FU24A–954 airplanes and was 

based on mandatory continuing 

airworthiness information originated by 

an aviation authority of another country. 

The MCAI states: 

This AD requires an inspection of the 

control column for mechanical damage, 

deformation and cracks per the instructions 

in Pacific Aerospace Limited (PAL) 

Mandatory Service Bulletin (MSB) No. 

PACSB/FU/095 issue 2 dated 28 May 2014. 

For control columns found with mechanical 

damage or deformation the AD requires a 50 

hour repetitive NDT inspection until 

replacement. Control column replacement is 

required at the next maintenance inspection, 

or within the next 150 hours TIS, whichever 

is the later. 

You may examine the MCAI on the 

Internet at http://www.regulations.gov 

by searching for and locating Docket No. 

FAA–2014–0532. 

Relevant Service Information 

Pacific Aerospace Limited has issued 

Mandatory Service Bulletin PACSB/FU/ 

095, Issue 2, dated May 28, 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 1 product 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 $42.50, or $42.50 per 

product. 

In addition, we estimate that any 

necessary follow-on actions would take 

about 8 work-hours and require parts 

costing $1,000, for a cost of $1,680 per 

product. We have no way of 

determining the number of products 

that may need these actions. 

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 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. Amend § 39.13 by adding the 

following new AD: 

Pacific Aerospace Limited: Docket No. FAA– 

2014–0532; Directorate Identifier 2014– 

CE–016–AD. 

(a) Comments Due Date 

We must receive comments by September 

19, 2014. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to Pacific Aerospace 

Limited Models FU24–954 and FU24A–954 

airplanes, all serial numbers, certificated in 

any category. 

(d) Subject 

Air Transport Association of America 

(ATA) Code 27: Flight Controls. 

(e) Reason 

This AD was prompted 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 cracking of 

the control column at the wiring access hole. 

We are issuing this AD to detect and correct 

cracking of the control column at the wiring 

access hole which could cause control 

column failure and subsequent loss of 

control. 

(f) Actions and Compliance 

Unless already done, do the following 

actions in paragraphs (f)(1) through (f)(3) of 


emcdonald on DSK67QTVN1PROD with PROPOSALS
Federal Register / Vol. 79, No. 150 / Tuesday, August 5, 2014 / Proposed Rules 45385 

this AD, following the accomplishment 

instructions in Pacific Aerospace Limited 

Mandatory Service Bulletin PACSB/FU/095, 

Issue 2, dated May 28, 2014. 

(1) Within the next 50 hours time-inservice (TIS) after the effective date of this 

AD, inspect the control column part number 

(P/N) 08–45031/32 for cracks. 

(2) If any mechanical damage, deformation, 

or cracks are found, before further flight, 

replace the control column with an airworthy 

control column P/N 08–45031/32. 

(3) If no mechanical damage, deformation, 

or cracks are found after the inspection 

required in paragraph (f)(1) of this AD, at the 

next scheduled maintenance inspection or 

within the next 150 hours TIS, whichever 

occurs later, replace the control column with 

an airworthy P/N 08–45031/32. 

(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: Karl Schletzbaum, Aerospace 

Engineer, FAA, Small Airplane Directorate, 

901 Locust, Room 301, Kansas City, Missouri 

64106; telephone: (816) 329–4123 ; fax: (816) 

329–4090; email: karl.schletzbaum@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 MCAI Civil Aviation Authority 

(CAA) AD DCA/FU24/183, dated May 29, 

2014, and Pacific Aerospace Limited 

Mandatory Service Bulletin PACSB/FU/095, 

Issue 2, dated May 28, 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– 

2014–0532. For service information related to 

this AD, contact Pacific Aerospace Limited, 

Airport Road, Hamilton Private Bag 3027 

Hamilton 3240, New Zealand; telephone: +64 

7 843 6144; fax: +64 7 843 6134; email: 

pacific@aerospace.co.nz; Internet: http://

www.aerospace.co.nz/. 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 July 29, 

2014. 

James E. Jackson, 

Acting Manager, Small Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2014–18449 Filed 8–4–14; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2014–0522; Directorate 

Identifier 2014–NM–087–AD] 

RIN 2120–AA64 

Airworthiness Directives; The Boeing 

Company Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: We propose to adopt a new 

airworthiness directive (AD) for certain 

The Boeing Company Model 747–100, 

747–100B, 747–100B SUD, 747–200B, 

747–200C, 747–200F, 747–300, 747– 

400, 747–400D, 747–400F, 747SR, and 

747SP series airplanes. This proposed 

AD was prompted by reports of cracks 

at the lower forward corner of the main 

entry door (MED) 1 cutout. This 

proposed AD would require repetitive 

inspections of the MED door 1 for 

cracking, and repair if necessary. This 

proposed AD also provides optional 

terminating modification; and would 

require post-repair or post-modification 

inspections for cracking, and corrective 

actions if necessary. We are proposing 

this AD to detect and correct skin 

cracking, which can become large and 

could adversely affect the structural 

integrity of the airplane. 

DATES: We must receive comments on 

this proposed AD by September 19, 

2014. 

ADDRESSES: You may send comments, 

using the procedures found in 14 CFR 

11.43 and 11.45, 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: Deliver to Mail 

address above between 9 a.m. and 5 

p.m., Monday through Friday, except 

Federal holidays. 

For service information identified in 

this proposed 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. 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. 

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– 

0522; 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 

(phone: 800–647–5527) is in the 

ADDRESSES section. Comments will be 

available in the AD docket shortly after 

receipt. 

FOR FURTHER INFORMATION CONTACT: 

Nathan Weigand, Aerospace Engineer, 

Airframe Branch, ANM–120S, Seattle 

Aircraft Certification Office (ACO), 

FAA, 1601 Lind Avenue SW., Renton, 

WA 98057–3356; phone: 425–917–6428; 

fax: 425–917–6590; email: 

Nathan.P.Weigand@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Comments Invited 

We invite you to send any written 

relevant data, views, or arguments about 

this proposal. Send your comments to 

an address listed under the ADDRESSES

section. Include ‘‘Docket No. FAA– 

2014–0522; Directorate Identifier 2014– 

NM–087–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://

www.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 

We have received reports of cracks at 

the lower forward corner of the MED 1 

cutout on two airplanes. A 1.0-inch 

crack in the skin and bearstrap was 

found on an airplane with 17,605 total 

flight cycles. A 5.0-inch crack was 

found in the skin, skin doubler, and 

bearstrap on an airplane with 21,759 

total flight cycles. In addition, four 

cracks between 0.18- and 1.85-inch were 

found on Boeing’s fatigue test airplane 


emcdonald on DSK67QTVN1PROD with PROPOSALS