27114 Federal Register / Vol. 80, No. 91 / Tuesday, May 12, 2015 / Proposed Rules 

§ 745.2(c)(2) are satisfied. In the event 

those requirements are satisfied, funds 

attributable to each client and principal 

will be insured on a pass-through basis 

in whatever right and capacity the client 

or principal owns the funds. For 

example, an IOLTA or other similar 

escrow account must be titled as such 

and the underlying account records of 

the insured credit union must 

sufficiently indicate the existence of the 

relationship on which a claim for 

insurance is founded. The details of the 

relationship between the attorney or 

escrow agent and their clients and 

principals must be ascertainable from 

the records of the insured credit union 

or from records maintained, in good 

faith and in the regular course of 

business, by the attorney or the escrow 

agent administering the account. NCUA 

will determine, in its sole discretion, the 

sufficiency of these records for an 

IOLTA or other similar escrow account. 

(b) Membership requirements and 

treatment of IOLTAs. For share 

insurance purposes, IOLTAs are treated 

as escrow accounts. IOLTAs and other 

similar escrow accounts are considered 

member accounts and eligible for passthrough share insurance if the attorney 

administering the IOLTA or the escrow 

agent administering the escrow account 

is a member of the insured credit union 

in which the funds are held. In this 

circumstance, the membership status of 

the clients or the principals is 

irrelevant. 

(c) Definitions. (1) For purposes of 

this section: 

Interest on lawyers trust account 

(IOLTA) means a system in which 

lawyers place certain client funds in 

interest-bearing or dividend-bearing 

accounts, with the interest or dividends 

then used to fund programs such as 

legal service organizations who provide 

services to clients in need. 

Other similar escrow account means 

an account where a licensed 

professional or other individual serving 

in a fiduciary capacity holds funds for 

the benefit of a client as part of a 

transaction or business relationship, 

such as realtor accounts and prepaid 

funeral accounts. 

Pass-through share insurance means, 

with respect to IOLTAs and other 

similar escrow accounts, insurance 

coverage based on the interest of each 

person on whose behalf funds are held 

in such accounts by the attorney 

administering the IOLTA or the escrow 

agent administering a similar escrow 

account. 

(2) The terms ‘‘Interest on lawyers 

trust account’’, ‘‘IOLTA’’, and ‘‘Passthrough share insurance’’ are given the 

same meaning in this section as in 12 

U.S.C. 1787(k)(5). 

[FR Doc. 2015–10553 Filed 5–11–15; 8:45 am] 

BILLING CODE 7535–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2015–1280; Directorate 

Identifier 2014–NM–064–AD] 

RIN 2120–AA64 

Airworthiness Directives; ATR–GIE 

Avions de Transport Re ́gional 

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 

ATR–GIE Avions de Transport Re ́gional 

Model ATR42–500 airplanes, and Model 

ATR72–102, –202, –212, and –212A 

airplanes. This proposed AD was 

prompted by a report of chafed wires 

between electrical harnesses. This 

proposed AD would require inspections 

for wiring discrepancies, and corrective 

actions if necessary. We are proposing 

this AD to detect and correct damaged 

wiring and incorrect installation of the 

wiring harness and adjacent air ducts, 

which could lead to wire harness 

chafing and arcing, possibly resulting in 

an on-board fire. 

DATES: We must receive comments on 

this proposed AD by June 26, 2015. 

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: U.S. Department of 

Transportation, Docket Operations, 

M–30, West Building Ground Floor, 

Room W12–140, 1200 New Jersey 

Avenue SE., Washington, DC, between 9 

a.m. and 5 p.m., Monday through 

Friday, except Federal holidays. 

For service information identified in 

this proposed AD, contact ATR–GIE 

Avions de Transport Re ́gional, 1, Alle ́e 

Pierre Nadot, 31712 Blagnac Cedex, 

France; telephone +33 (0) 5 62 21 62 21; 

fax +33 (0) 5 62 21 67 18; email 

continued.airworthiness@atr.fr; Internet 

http://www.aerochain.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–2015– 

1280; 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 Operations 

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: Tom 

Rodriguez, Aerospace Engineer, 

International Branch, ANM–116, 

Transport Airplane Directorate, FAA, 

1601 Lind Avenue SW., Renton, WA 

98057–3356; telephone (425) 227–1137; 

fax (425) 227–1149. 

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–2015–1280; Directorate Identifier 

2014–NM–064–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 based on 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 

The European Aviation Safety Agency 

(EASA), which is the Technical Agent 

for the Member States of the European 

Union, has issued EASA Airworthiness 

Directive 2014–0052R1, dated April 7, 

2014 (referred to after this as the 

Mandatory Continuing Airworthiness 

Information, or ‘‘the MCAI’’), to correct 

an unsafe condition for certain ATR– 

mstockstill on DSK4VPTVN1PROD with PROPOSALS

Federal Register / Vol. 80, No. 91 / Tuesday, May 12, 2015 / Proposed Rules 27115 

GIE Avions de Transport Re ́gional 

Model ATR42–500 airplanes, and Model 

ATR72–102, –202, –212, and –212A 

airplanes. The MCAI states: 

An erroneous cockpit indication has been 

reported on an in-service aircraft. Subsequent 

investigation identified chafed wiring 

between harnesses (2M–2S–6M) and the 

metallic structure of the cargo lining panel 

above the electronic rack 90VU shelf. The 

chafing was most likely the result of incorrect 

harness installation. In some cases, the 

bracket, which supports the harnesses, could 

be incorrectly positioned. Consequently, the 

wiring harnesses, and in certain 

configurations, the adjacent air duct, could 

be incorrectly routed. 

This condition, if not detected and 

corrected, could lead to wiring harness 

chafing and arcing, possibly resulting in an 

on-board fire. 

To address this potential unsafe condition, 

ATR issued Service Bulletin (SB) ATR42–92– 

0024 and SB ATR72–92–1032, as applicable 

to aeroplane model, to provide inspection 

instructions. 

For the reasons described above, EASA 

issued AD 2014–0052 [http://www.casa.gov.

au/wcmswr/_assets/main/lib100154/2014- 

0052.pdf] to require a one-time visual 

inspection of the affected area including a 

systematic bracket position check and, 

depending on findings, accomplishment of 

applicable corrective actions. 

This [EASA] AD is revised to make the 

bracket position check dependent on 

findings, determined during the inspection of 

the electrical bundle and air duct routing. 

Corrective actions include repairing damaged 

wiring, correctly installing the bracket which 

supports bundle 2M–2S–6M, and routing 

bundle 2M–2S–6M and the air conditioning 

flexible hose in the correct positions. 

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–2015– 

1280. 

Related Service Information Under 1 

CFR Part 51 

ATR–GIE Avions de Transport 

Re ́gional has issued Service Bulletin 

ATR42–92–0024, Revision 01, dated 

January 16, 2014. The service 

information describes procedures for 

inspecting the electrical harness routing 

on the top of 90VU electric rack and to 

modify it if necessary. 

ATR–GIE Avions de Transport 

Re ́gional has also issued Service 

Bulletin ATR72–92–1032, Revision 01, 

dated January 16, 2014. The service 

information describes procedures for 

inspecting the electrical harness routing 

on the top of 90VU electric rack and to 

modify it if necessary. 

The actions described in this service 

information are intended to correct the 

unsafe condition identified in the 

MCAI. 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 NPRM. 

FAA’s Determination and Requirements 

of This 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 the State of 

Design Authority, we have been notified 

of the unsafe condition described in the 

MCAI and service information 

referenced above. We are proposing this 

AD because we evaluated all pertinent 

information and determined an unsafe 

condition exists and is likely to exist or 

develop on other products of these same 

type designs. 

Costs of Compliance 

We estimate that this proposed AD 

affects 1 airplane of U.S. registry. 

We also estimate that it would take 

about 1 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 

this proposed AD on U.S. operators to 

be $85, or $85 per product. 

In addition, we estimate that any 

necessary follow-on actions would take 

about 3 work-hours and require parts 

costing $82, for a cost of $337 per 

product. We have no way of 

determining the number of aircraft that 

might 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 airworthiness 

directive (AD): 

ATR–GIE Avions de Transport Re ́gional: 

Docket No. FAA–2015–1280; Directorate 

Identifier 2014–NM–064–AD. 

(a) Comments Due Date 

We must receive comments by June 26, 

2015. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to the ATR–GIE Avions de 

Transport Re ́gional airplanes identified in 

paragraphs (c)(1) and (c)(2) of this AD, 

certificated in any category. 

(1) Model ATR42–500 airplanes, serial 

numbers 443 through 1006 inclusive, except 

serial numbers 811, 1002, and 1005. 

(2) Model ATR72–102, –202, –212, and 

–212A airplanes, serial numbers 475 through 

969 inclusive, 971 through 988 inclusive, 

1025, 1028 through 1069 inclusive, and 1072, 

except serial numbers 956 and 1042. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 92, Electrical Routing. 

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27116 Federal Register / Vol. 80, No. 91 / Tuesday, May 12, 2015 / Proposed Rules 

(e) Reason 

This AD was prompted by a report of 

chafed wires between electrical harnesses. 

We are issuing this AD to detect and correct 

damaged wiring and incorrect installation of 

the wiring harness and adjacent air ducts, 

which could lead to wire harness chafing and 

arcing, possibly resulting in an on-board fire. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Inspections 

Within 500 flight hours after the effective 

date of this AD, do the actions specified in 

paragraphs (g)(1) and (g)(2) of this AD, in 

accordance with the Accomplishment 

Instructions of Avions de Transport Re ́gional 

Service Bulletin ATR42–92–0024, Revision 

01, dated January 16, 2014; or Avions de 

Transport Re ́gional Service Bulletin ATR72– 

92–1032, Revision 01, dated January 16, 

2014; as applicable. 

(1) Do a general visual inspection for 

damage of the electrical wires of bundle 2M– 

2S–6M. 

(2) Do a general visual inspection for 

correct routing of electrical bundle 2M–2S– 

6M, and correct routing of the air duct. 

(h) Corrective Actions 

(1) If, during the inspection required by 

paragraph (g)(1) of this AD, any damage is 

found on the electrical wires: Before further 

flight, repair the wires, in accordance with 

the Accomplishment Instructions of Avions 

de Transport Re ́gional Service Bulletin 

ATR42–92–0024, Revision 01, dated January 

16, 2014; or Avions de Transport Re ́gional 

Service Bulletin ATR72–92–1032, Revision 

01, dated January 16, 2014; as applicable. 

(2) If, during the inspection required by 

paragraph (g)(2) of this AD, electrical bundle 

2M–2S–6M and/or an air duct is found to be 

incorrectly routed: Within 500 flight hours 

after the effective date of this AD, do a 

general visual inspection for correct 

positioning of the bracket, in accordance 

with the Accomplishment Instructions of 

Avions de Transport Re ́gional Service 

Bulletin ATR42–92–0024, Revision 01, dated 

January 16, 2014; or Avions de Transport 

Re ́gional Service Bulletin ATR72–92–1032, 

Revision 01, dated January 16, 2014; as 

applicable. 

(i) If, during the inspection required by 

paragraph (h)(2) of this AD, the bracket is 

found to be correctly positioned: Within 500 

flight hours after the effective date of this AD, 

do all applicable corrective actions, in 

accordance with the Accomplishment 

Instructions of Avions de Transport Re ́gional 

Service Bulletin ATR42–92–0024, Revision 

01, dated January 16, 2014; or Avions de 

Transport Re ́gional Service Bulletin ATR72– 

92–1032, Revision 01, dated January 16, 

2014; as applicable. 

(ii) If, during the inspection required by 

paragraph (h)(2) of this AD, the bracket is 

found to be missing or incorrectly positioned: 

Within 500 flight hours after the inspection 

required by paragraph (h)(2) of this AD, 

repair using a method approved by the 

Manager, International Branch, ANM–116, 

Transport Airplane Directorate, FAA; or the 

European Aviation Safety Agency (EASA); or 

ATR–GIE Avions de Transport Re ́gional’s 

EASA Design Organization Approval (DOA). 

(i) Credit for Previous Actions 

This paragraph provides credit for actions 

required by this AD, if those actions were 

performed before the effective date of this AD 

using Avions de Transport Re ́gional Service 

Bulletin ATR42–92–0024, dated June 6, 2013; 

or Avions de Transport Re ́gional Service 

Bulletin ATR72–92–1032, dated June 6, 2013; 

as applicable; which are not incorporated by 

reference in this AD. 

(j) Other FAA AD Provisions 

The following provisions also apply to this 

AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, International 

Branch, ANM–116, Transport Airplane 

Directorate, 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 Branch, send it to ATTN: 

Tom Rodriguez, Aerospace Engineer, 

International Branch, ANM–116, Transport 

Airplane Directorate, FAA, 1601 Lind 

Avenue SW., Renton, WA 98057–3356; 

telephone (425) 227–1137; fax (425) 227– 

1149. Information may be emailed to: 9- 

ANM-116-AMOC-REQUESTS@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. The AMOC 

approval letter must specifically reference 

this AD. 

(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 Branch, ANM– 

116, Transport Airplane Directorate, FAA; or 

the EASA; or ATR–GIE Avions de Transport 

Re ́gional’s EASA DOA. If approved by the 

DOA, the approval must include the DOAauthorized signature. 

(k) Related Information 

(1) Refer to Mandatory Continuing 

Airworthiness Information (MCAI) EASA 

Airworthiness Directive 2014–0052R1, dated 

April 7, 2014, 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– 

2015–1280. 

(2) For service information identified in 

this AD, contact ATR–GIE Avions de 

Transport Re ́gional, 1, Alle ́e Pierre Nadot, 

31712 Blagnac Cedex, France; telephone +33 

(0) 5 62 21 62 21; fax +33 (0) 5 62 21 67 18; 

email continued.airworthiness@atr.fr; 

Internet http://www.aerochain.com. 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. 

Issued in Renton, Washington, on May 1, 

2015. 

Jeffrey E. Duven, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2015–11350 Filed 5–11–15; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2015–1281; Directorate 

Identifier 2014–NM–241–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 all The 

Boeing Company Model 777 airplanes. 

This proposed AD was prompted by an 

evaluation by the design approval 

holder (DAH) indicating that the lap 

splices of the aft pressure bulkhead 

webs are subject to widespread fatigue 

damage (WFD). This proposed AD 

would require repetitive inspections for 

any crack in the aft webs of the radial 

lap splices of the aft pressure bulkhead, 

and, if necessary, corrective actions. We 

are proposing this AD to detect and 

correct fatigue cracking in the aft webs 

of the radial lap splices of the aft 

pressure bulkhead, which could result 

in reduced structural integrity of the 

airplane and decompression of the 

cabin. 

DATES: We must receive comments on 

this proposed AD by June 26, 2015. 

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 

mstockstill on DSK4VPTVN1PROD with PROPOSALS