19546 Federal Register / Vol. 79, No. 68 / Wednesday, April 9, 2014 / Proposed Rules 

the small businesses that receive 

services from them. 

List of Subjects in 13 CFR Part 102 

Freedom of information, Privacy, 

Grants. 

For the reasons set forth in the 

preamble, SBA proposes to amend 13 

CFR part 102 as follows: 

PART 102—RECORD DISCLOSURE 

AND PRIVACY 

■ 1. The authority citation for part 102 

is revised to read as follows: 

Authority: 5 U.S.C. 301, 552, 552a, 15 

U.S.C. 648(a)(7) and 656(n); 31 U.S.C. 9701; 

44 U.S.C. 3501, E.O. 12600, 52 FR 23781, 3 

CFR, 1987 Comp., p. 235. 

■ 2. Add subpart C to read as follows: 

Subpart C—Standards for Collection 

and Use of Program Activity Data and 

Surveys 

Sec. 

102.50 Purpose and scope. 

102.51 Definitions. 

102.52 Standards for disclosure and use of 

information. 

102.53 Data collection methodologies. 

102.54 Use of program activity or survey 

and poll data. 

102.55 Use of financial examination and 

programmatic review data. 

§ 102.50 Purpose and scope. 

The purpose of these regulations is to 

establish standards for the disclosure of 

information collected from any 

individual or small business concern 

receiving assistance from SBA through 

its resource partners. The scope of these 

regulations is limited to SBA conducted 

financial examinations or programmatic 

reviews of a resource partner, or a 

survey or poll conducted of an SBA 

resource partner’s clients. 

§ 102.51 Definitions 

Audit means a financial examination 

or programmatic review conducted by 

the Office of Entrepreneurial 

Development. This provision does not 

apply to audits, investigations or other 

activities conducted by the SBA’s Office 

of Inspector General (OIG) or a financial 

statement audit. 

Client means a person or small 

business that receives management or 

technical assistance from SBA, an SBA 

resource partner, an approved SBA 

lender, or any other provider 

participating in any of SBA’s programs. 

The assistance is direct or indirect and 

may also include loans, or investments 

or other such activities as enumerated in 

agreements or funding documents 

between the resource partner and SBA. 

Customer Satisfaction means the 

degree to which clients would 

recommend the service received to other 

small business individuals and/or that 

they were generally pleased with the 

service provided to them and would use 

the service again. 

Examination means a financial 

examination or programmatic review. 

This provision does not apply to audits 

conducted by the SBA’s Office of 

Inspector General (OIG) or a financial 

statement audit. 

Poll means an informal, voluntary 

data collection that contains broad 

based questions that place little to no 

burden on the respondent. A Poll is 

anecdotal and not statistical in nature, 

and is used to gain a quick view of a 

particular issue. A Poll does not collect 

information protected under the Privacy 

Act of 1974. 

Program Activity Data means data 

collected through any methods 

established by or on behalf of SBA 

concerning a resource partner’s client 

activity, including but not limited to, 

counseling, training, and other technical 

assistance activities. 

Resource Partner means any grantee, 

subrecipient, or system of grantees and 

subrecipients that enters into a formal 

agreement with SBA to deliver small 

business management and technical 

assistance to the general public, small 

business concerns and/or any 

specialized assistance related thereto. 

Submitter means any person or entity 

that provides information to SBA 

through a data collection system, 

survey, poll, financial examination, 

programmatic review or other data 

collection activity. 

Survey means a collection of data 

whose purposes include the description, 

estimation, or analysis of the 

characteristics of groups, organizations, 

segments, activities, or geographic areas. 

§ 102.52 Standards for disclosure and use 

of information. 

The standards in subparts A and B of 

13 CFR part 102 relating to privacy and 

disclosure of information collected and 

maintained by the SBA apply to the 

disclosure and use of information 

collected from resource partners and 

their clients. 

§ 102.53 Data collection methodologies. 

All data collection methodologies 

utilized will be consistent with relevant 

Federal rules and regulations, including 

the Paperwork Reduction Act, and SBA 

standard operating procedures. 

§ 102.54 Use of program activity or survey 

and poll data. 

Program activity and client survey or 

poll data are collected for the purposes 

of: 

(a) Measuring the effect and economic 

or other impact of Agency programs; 

(b) Assessing public and resource 

partner needs; 

(c) Measuring customer satisfaction; 

(c) Guiding program policy 

development; 

(d) Improving grant-making processes; 

(e) Improving relationship 

management with these entities; and 

(f) Other areas SBA determines would 

be valuable to strengthen programs and/ 

or enhance support for clients. 

§ 102.55 Use of financial examination or 

programmatic review data. 

Financial examination or 

programmatic review data regarding 

client information is collected, to the 

extent necessary, for the purposes of: 

(a) Assessing the quality, quantity and 

scope of client service provided; 

(b) Ensuring compliance with the 

governing rules and program 

requirements; 

(c) Determining the appropriateness of 

activities conducted under the program 

and/or cost incurred by submitters such 

as grantees, resource partners, 

contractors, lenders and other program 

stakeholders; and 

(d) Other areas relevant to SBA 

oversight of its programs. 

This data is separate from ongoing 

program activity data and does not 

interfere with the collection of that 

information. 

Dated: March 31, 2014. 

Marianne O’Brien Markowitz, 

Acting Administrator. 

[FR Doc. 2014–07850 Filed 4–8–14; 8:45 am] 

BILLING CODE 8025–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2014–0191; Directorate 

Identifier 2013–NM–256–AD] 

RIN 2120–AA64 

Airworthiness Directives; Bombardier, 

Inc. 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 

Bombardier, Inc. Model DHC–8–400 

series airplanes. This proposed AD was 

prompted by reports of swing arm 

assemblies of engine fuel feed ejector 

pumps detaching from the outlet port of 

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Federal Register / Vol. 79, No. 68 / Wednesday, April 9, 2014 / Proposed Rules 19547 

the engine fuel feed ejector pump and 

partially blocking the engine fuel feed 

line. This proposed AD would require 

installing a restrictor into the engine 

fuel feed line. We are proposing this AD 

to prevent blocked engine fuel flow and 

possible engine flameout. 

DATES: We must receive comments on 

this proposed AD by May 27, 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, between 9 a.m. and 5 

p.m., Monday through Friday, except 

Federal holidays. 

• For service information identified 

in this proposed AD, contact 

Bombardier, Inc., Q-Series Technical 

Help Desk, 123 Garratt Boulevard, 

Toronto, Ontario M3K 1Y5, Canada; 

telephone 416–375–4000; fax 416–375– 

4539; email thd.qseries@

aero.bombardier.com; Internet http:// 

www.bombardier.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– 

0191; 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: 

Morton Lee, Propulsion Engineer, 

Propulsion & Services Branch, ANE– 

173, FAA, New York Aircraft 

Certification Office, 1600 Stewart 

Avenue, Suite 410, Westbury, NY 

11590; telephone 516–228–7355; fax 

516–794–5531. 

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–2014–0191; Directorate Identifier 

2013–NM–256–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 

Transport Canada Civil Aviation 

(TCCA), which is the aviation authority 

for Canada, has issued Canadian 

Airworthiness Directive CF–2013–35, 

dated November 15, 2013 (referred to 

after this as the Mandatory Continuing 

Airworthiness Information, or ‘‘the 

MCAI’’), to correct an unsafe condition 

for the specified products. The MCAI 

states: 

There have been incidents of the ‘‘ENG 

FUEL PRESS’’ caution light illuminating inflight. An investigation revealed the engine 

fuel feed ejector pump swing arm assembly 

became detached from the outlet port of the 

engine fuel feed ejector pump and partially 

blocked the engine fuel feed line. If the failed 

swing arm assembly migrates along the fuel 

line downstream of the Fuel Tank AUX 

Pump junction, it could block the engine fuel 

flow and the affected engine may experience 

a flameout condition. 

Bombardier issued Service Bulletin (SB) 

84–28–16 to introduce a restrictor into the 

engine fuel feed line that is designed to 

contain a detached ejector pump swing arm 

assembly. 

This [Canadian] AD mandates the 

installation of a restrictor into the engine fuel 

feed line to prevent possible engine flameout. 

You may examine the MCAI in the 

AD docket on the Internet at http:// 

www.regulations.gov by searching for 

and locating it in Docket No. FAA– 

2014–0191. 

Relevant Service Information 

Bombardier has issued Service 

Bulletin 84–28–16, Revision B, dated 

June 17, 2013. The actions described in 

this service information are intended to 

correct the unsafe condition identified 

in the MCAI. 

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 the same 

type design. 

Costs of Compliance 

We estimate that this proposed AD 

affects 81 airplanes of U.S. registry. 

We also estimate that it would take 

about 12 work-hours per product to 

comply with the basic requirements of 

this proposed AD. The average labor 

rate is $85 per work-hour. Required 

parts would cost about $0 per product. 

Based on these figures, we estimate the 

cost of this proposed AD on U.S. 

operators to be $82,620, or $1,020 per 

product. 

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: 

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19548 Federal Register / Vol. 79, No. 68 / Wednesday, April 9, 2014 / Proposed Rules 

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 airworthiness directive 

(AD): 

Bombardier, Inc.: Docket No. FAA–2014– 

0191; Directorate Identifier 2013–NM– 

256–AD. 

(a) Comments Due Date 

We must receive comments by May 27, 

2014. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to Bombardier, Inc. Model 

DHC–8–400, –401, and –402 airplanes; 

certificated in any category; serial numbers 

4001, and 4003 through 4417 inclusive, with 

installed engine fuel feed ejector pump 

having part number (P/N) 2960008–102. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 28, Fuel. 

(e) Reason 

This AD was prompted by reports of swing 

arm assemblies of engine fuel feed ejector 

pumps detaching from the outlet port of the 

engine fuel feed ejector pump and partially 

blocking the engine fuel feed line. We are 

issuing this AD to prevent blocked engine 

fuel flow and possible engine flameout. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Installation 

Within 6,000 flight hours or 36 months, 

whichever occurs first, after the effective date 

of this AD, install a restrictor into the engine 

fuel feed line, in accordance with the 

Accomplishment Instructions of Bombardier 

Service Bulletin 84–28–16, Revision B, dated 

June 17, 2013. 

(h) Credit for Previous Actions 

This paragraph provides credit for actions 

required by paragraph (g) of this AD, if those 

actions were performed before the effective 

date of this AD using Bombardier Service 

Bulletin 84–28–16, dated July 16, 2012; or 

Revision A, dated May 23, 2013. This service 

information is not incorporated by reference 

in this AD. 

(i) Other FAA AD Provisions 

The following provisions also apply to this 

AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, New York Aircraft 

Certification Office (ACO), ANE–170, 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 ACO, send it to ATTN: 

Program Manager, Continuing Operational 

Safety, FAA, New York ACO, 1600 Stewart 

Avenue, Suite 410, Westbury, NY 11590; 

telephone 516–228–7300; fax 516–794–5531. 

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) Airworthy Product: For any requirement 

in this AD to obtain corrective actions from 

a manufacturer, use these actions if they are 

FAA-approved. Corrective actions are 

considered FAA-approved if they were 

approved by the State of Design Authority (or 

its delegated agent, or the DAH with a State 

of Design Authority’s design organization 

approval). For a repair method to be 

approved, the repair approval must 

specifically refer to this AD. You are required 

to ensure the product is airworthy before it 

is returned to service. 

(j) Related Information 

(1) Refer to Mandatory Continuing 

Airworthiness Information (MCAI) Canadian 

Airworthiness Directive CF–2013–35, dated 

November 15, 2013, 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 it in Docket No. 

FAA–2014–0191. 

(2) For service information identified in 

this AD, contact Bombardier, Inc., Q-Series 

Technical Help Desk, 123 Garratt Boulevard, 

Toronto, Ontario M3K 1Y5, Canada; 

telephone 416–375–4000; fax 416–375–4539; 

email thd.qseries@aero.bombardier.com; 

Internet http://www.bombardier.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 April 2, 

2014. 

Jeffrey E. Duven, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2014–07934 Filed 4–8–14; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2014–0192; Directorate 

Identifier 2013–NM–221–AD] 

RIN 2120–AA64 

Airworthiness Directives; Airbus 

Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: We propose to supersede 

Airworthiness Directive (AD) 2013–10– 

06, for all Airbus Model A330–200 

Freighter, A330–200, A330–300, A340– 

200, A340–300, A340–500, and A340– 

600 series airplanes. AD 2013–10–06 

currently requires an inspection to 

identify the installed windshields, and 

replacement of any affected windshield. 

Since we issued AD 2013–10–06, the 

manufacturer has identified a new batch 

of affected windshield parts on the 

airplane. This proposed AD would 

expand the inspection area to 15 

additional windshields’ serial numbers. 

We are proposing this AD to prevent 

significantly increased workload for the 

flightcrew, which could, under some 

flight phases and/or circumstances, 

constitute an unsafe condition. 

DATES: We must receive comments on 

this proposed AD by May 27, 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, between 9 a.m. and 5 

p.m., Monday through Friday, except 

Federal holidays. 

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