Federal Register / Vol. 76, No. 27 / Wednesday, February 9, 2011 / Rules and Regulations 7101 

liability on its guaranty, is being 

modified because, in addition to the 

grounds stated in this regulation, the 

lender’s failure to comply with its 

policies and procedures governing floor 

plan financing or the terms and 

procedures set forth in this Federal 

Register notice or the DFP Procedural 

Guide may result in denial of SBA’s 

guaranty on the loan, in full or in part. 

In addition, if the proceeds of the DFP 

line of credit are used to replace a same 

institution floor plan line and the 

borrower defaults on the DFP line of 

credit within 90 days of initial 

disbursement, SBA may deny liability 

on its guaranty of the DFP line. The 

regulation at 13 CFR 120.520(a) is also 

being waived to allow lenders to make 

demand on SBA to honor its guaranty in 

the above situations without being 

required to liquidate all business 

personal property securing the line of 

credit first. 

The statutory language creating this 

DFP Pilot overrides the regulatory 

prohibition against floor plan financing 

or other revolving line credit (except 

under 120.390) found in 13 CFR 

120.130(c). 

All other provisions of the Small 

Business Act applicable to the 7(a) loan 

program apply to loans made under the 

DFP Pilot. Unless waived or modified 

by this Notice, all the regulations 

applicable to the 7(a) loan program 

apply to loans made under the DFP 

Pilot. All standard operating procedures 

applicable to the 7(a) loan program that 

are not superseded by any provision of 

this Notice or the DFP Procedural Guide 

apply to loans made under this pilot. 

Lenders must use prudent lending 

practices in the making, servicing and 

liquidating of SBA-guaranteed floor 

plan lines of credit and must comply 

with all SBA Loan Program 

Requirements that are not superseded 

by any provisions of this Notice or the 

DFP Procedural Guide. 

SBA will provide more detailed 

guidance in the form of a procedural 

guide which will be available on SBA’s 

Web site, http://www.sba.gov. SBA may 

also provide additional guidance, if 

needed, through SBA notices, which 

will also be published on SBA’s Web 

site, http://www.sba.gov. 

Questions on the DFP Pilot may be 

directed to the Lender Relations 

Specialist in the local SBA district 

office. The local SBA district office may 

be found at http://www.sba.gov/ 

localresources/index.html. 

Authority: 15 U.S.C. 636(a)(34) and 13 CFR 

120.3. 

Dated: February 3, 2011. 

Karen G. Mills, 

Administrator. 

[FR Doc. 2011–2836 Filed 2–8–11; 8:45 am] 

BILLING CODE 8025–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2009–0113; Directorate 

Identifier 2008–NE–25–AD; Amendment 39– 

16602; AD 2011–04–02] 

RIN 2120–AA64 

Airworthiness Directives; Hamilton 

Sundstrand Propellers Model 247F 

Propellers 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for the 

products listed above. This AD requires 

removing affected propeller blades from 

service. This AD was prompted by 

reports of blades with corrosion pits in 

the tulip area of the blades. We are 

issuing this AD to prevent cracks from 

developing in the tulip area of the blade, 

which could result in separation of the 

blade and possible loss of airplane 

control. 

DATES: This AD is effective March 16, 

2011. 

ADDRESSES: 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http:// 

www.regulations.gov; 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 address for the 

Docket Office (phone: 800–647–5527) is 

Document Management Facility, U.S. 

Department of Transportation, Docket 

Operations, M–30, West Building 

Ground Floor, Room W12–140, 1200 

New Jersey Avenue, SE., Washington, 

DC 20590. 

FOR FURTHER INFORMATION CONTACT: 

Michael Schwetz, Aerospace Engineer, 

Boston Aircraft Certification Office, 

FAA, Engine and Propeller Directorate, 

12 New England Executive Park, 

Burlington, MA 01803; telephone (781) 

238–7761; fax (781) 238–7170; e-mail: 

michael.schwetz@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We issued a supplemental notice of 

proposed rulemaking (SNPRM) to 

amend 14 CFR part 39 to include an AD 

that would apply to the specified 

products. That SNPRM published in the 

Federal Register on October 8, 2010 

(75 FR 62333). That SNPRM proposed to 

require removing affected propeller 

blades from service. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

received no comments on the SNPRM or 

on the determination of the cost to the 

public. 

Conclusion 

We reviewed the relevant data and 

determined that air safety and the 

public interest require adopting the AD 

as proposed except for minor changes to 

the compliance date for certain serial 

number (S/N) propeller blades. The 

SNPRM proposed to require removing 

propeller blades part number (P/N) 

817370–1, S/Ns FR2449 to FR2958 

inclusive, FR20010710 to FR20010722 

inclusive, and FR20010723RT to 

FR20020127RT inclusive, before 

December 31, 2010. We determined that 

those S/N propeller blades should be 

removed within the same compliance 

time as propeller blades P/N 817370–1, 

S/Ns FR2018, FR2103, FR2108, FR2109, 

FR2111, FR2123, FR2183, FR2187, 

FR2262, FR2276 through FR2279 

inclusive, and FR2398. We have 

determined that these minor changes: 

• Are consistent with the intent that 

was proposed in the SNPRM for 

correcting the unsafe condition; and 

• Do not add any additional burden 

upon the public than was already 

proposed in the SNPRM. 

Costs of Compliance 

We estimate that this AD will affect 

10 propellers installed on airplanes of 

U.S. registry. We also estimate that it 

will take about 16 work-hours per 

propeller to perform the required 

actions, and that the average labor rate 

is $85 per work-hour. Required parts 

will cost about $50 per propeller. Based 

on these figures, we estimate the total 

cost of this AD to U.S. operators to be 

$14,100. 

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. 


erowe on DSK5CLS3C1PROD with RULES
7102 Federal Register / Vol. 76, No. 27 / Wednesday, February 9, 2011 / Rules and Regulations 

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 

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, 

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

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, 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 airworthiness 

directive (AD): 

2011–04–02 Hamilton Sundstrand 

Corporation: Amendment 39–16602; 

Docket No. FAA–2009–0113; Directorate 

Identifier 2008–NE–25–AD. 

Effective Date 

(a) This AD is effective March 16, 2011. 

Affected ADs 

(b) None. 

Applicability 

(c) This AD applies to Hamilton 

Sundstrand model 247F series propellers 

with blades part number (P/N) 817370–1, 

serial numbers (S/Ns) FR2018, FR2103, 

FR2108, FR2109, FR2111, FR2123, FR2183, 

FR2187, FR2262, FR2276 through FR2279 

inclusive, FR 2398, FR2449 to FR2958 

inclusive, FR20010710 to FR20010722 

inclusive, and FR20010723RT to 

FR20020127RT inclusive, installed. These 

propellers are installed on, but not limited to, 

ATR–GIE Avions de Transport Regional 

ATR72–210 and ATR72–210E airplanes. 

Unsafe Condition 

(d) This AD results from reports of blades 

with corrosion pits in the tulip area of the 

blades. We are issuing this AD to prevent 

cracks from developing in the tulip area of 

the blade, which could result in separation 

of the blade and possible loss of airplane 

control. 

Compliance 

(e) You are responsible for having the 

actions required by this AD performed within 

the compliance times specified unless the 

actions have already been done. 

Removing Blades P/N 817370–1 

(f) Remove from service, blades P/N 

817370–1, S/Ns FR2018, FR2103, FR2108, 

FR2109, FR2111, FR2123, FR2183, FR2187, 

FR2262, FR2276 through FR2279, FR2398, 

FR2449 to FR2958 inclusive, FR20010710 to 

FR20010722 inclusive, and FR20010723RT to 

FR20020127RT inclusive, within 30 days 

after the effective date of this AD. 

Alternative Methods of Compliance 

(g) The Manager, Boston Aircraft 

Certification Office, has the authority to 

approve alternative methods of compliance 

for this AD if requested using the procedures 

found in 14 CFR 39.19. 

Related Information 

(h) For more information about this AD, 

contact Michael Schwetz, Aerospace 

Engineer, Boston Aircraft Certification Office, 

FAA, Engine and Propeller Directorate, 12 

New England Executive Park, Burlington, 

MA 01803; telephone (781) 238–7761; fax 

(781) 238–7170; e-mail: 

michael.schwetz@faa.gov. 

Issued in Burlington, Massachusetts, on 

January 31, 2011. 

Peter A. White, 

Acting Manager, Engine & Propeller 

Directorate, Aircraft Certification Service. 

[FR Doc. 2011–2758 Filed 2–8–11; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF COMMERCE 

Bureau of Industry and Security 

15 CFR Part 748 

[Docket No. 100826397–1059–02] 

RIN 0694–AE98 

Simplified Network Application 

Processing System, On-line 

Registration and Account Maintenance 

AGENCY: Bureau of Industry and 

Security, Commerce. 

ACTION: Final rule. 

SUMMARY: The Bureau of Industry and 

Security (BIS) amends the Export 

Administration Regulations to 

implement a mandatory on-line 

registration process for obtaining an 

account to submit license applications 

and similar documents electronically 

through SNAP–R. This final rule sets 

forth the information that parties 

registering on-line are required to 

provide to BIS and the duties that 

registered parties have with respect to 

keeping information in their accounts 

current. This rulemaking is consistent 

with the goals and principles of 

Executive Orders 13563 and 12866, 

which are to enhance effectiveness and 

efficiency and to promote transparency 

and openness in government, and the 

Presidential Memorandum on 

Regulatory Flexibility, Small Business, 

and Job Creation (January 18, 2011). 

DATES: Effective date: March 11, 2011. 

Compliance dates: Beginning on April 

11, 2011, all new SNAP–R registrations 

must be made in accordance with this 

rule. 

Beginning on June 10, 2011 accounts 

of filing entities that do not have 

account administrators will not be 

accessible until an existing individual 

user for that entity logs-on to SNAP–R 

and registers as account administrator. 

Beginning on September 8, 2011 the 

accounts of filing entities that do not 

have an account administrator will 

become inactive. In order to reactivate 

the account, filing entities will have to 

complete the entire registration process 

that applies to new entities. 

FOR FURTHER INFORMATION CONTACT: 

Thomas W. Andrukonis, Director, 

Export Management and Compliance 

Division, Office of Exporter Services, 

telephone (202) 482–6393, e-mail 

tandruko@bis.doc.gov. 

SUPPLEMENTARY INFORMATION: 

Immediate Voluntary Implementation 

of On-Line Registration 

Beginning on February 9, 2011, BIS 

will accept on-line SNAP–R 


erowe on DSK5CLS3C1PROD with RULES