Federal Register / Vol. 78, No. 8 / Friday, January 11, 2013 / Rules and Regulations 2331 

For CICA programs other than AHP and 

CIP, a Bank shall price advances to 

members as provided in § 1266.5 of this 

chapter, and may price such advances at 

rates below the price of advances of 

similar amounts, maturities and terms 

made pursuant to section 10(a) of the 

Bank Act. (12 U.S.C. 1430(a)). 

(2) Pricing of CIP advances. The price 

of advances made under CIP shall not 

exceed the Bank’s cost of issuing 

consolidated obligations of comparable 

maturity, taking into account reasonable 

administrative costs. 

(3) Pricing of AHP advances. A Bank 

shall price advances made under AHP 

in accordance with parts 1266 and 1291 

of this chapter. 

(4) Advances to housing associate 

borrowers. (i) A Bank may offer 

advances under CICA programs to 

housing associate borrowers at the 

Bank’s option, except for AHP and CIP, 

which are available only to members. 

(ii) A Bank shall price advances to 

housing associate borrowers as provided 

in § 1266.17 of this chapter, and may 

price such advances at rates below the 

price of advances of similar amounts, 

maturities and terms made pursuant to 

section 10b of the Bank Act. (12 U.S.C. 

1430b). 

(5) Pricing pass-through. A Bank may 

require that borrowers receiving 

advances made under CICA programs 

pass through the benefit of any price 

reduction from regular advance pricing 

to their borrowers. 

(6) Discount Fund. (i) A Bank may 

establish a Discount Fund which the 

Bank may use to reduce the price of CIP 

or other advances made under CICA 

programs below the advance prices 

provided for by this part. 

(ii) Price reductions made through the 

Discount Fund shall be made in 

accordance with a fair distribution 

scheme. 

§ 1292.6 Reporting. 

(a) Each Bank annually shall provide 

to FHFA, on or before January 31, a 

Targeted Community Lending Plan. 

(b) Each Bank shall provide such 

other reports concerning its CICA 

programs as FHHA may request from 

time to time. 

§ 1292.7 Documentation. 

(a) A Bank shall require the borrower 

to certify to the Bank that each project 

funded under a CICA program (other 

than AHP) meets the respective 

targeting requirements of the CICA 

program. Such certification shall 

include a description of how the project 

meets the requirements, and where 

appropriate, a statistical summary or list 

of incomes of the borrowers, rents for 

the project, or salaries of jobs created or 

retained. 

(b) For those CICA-funded projects 

that also receive funds from another 

targeted Federal economic development 

program that has income targeting 

requirements that are the same as, or 

more restrictive than, the targeting 

requirements of the applicable CICA 

program, the Bank shall permit the 

borrower to certify that compliance with 

the criteria of such Federal economic 

development program will meet the 

requirements of the respective CICA 

program. 

(c) Such certifications shall satisfy the 

Bank’s obligations to document 

compliance with the CICA funding 

provisions of this part. 

Dated: December 18, 2012. 

Edward J. DeMarco, 

Acting Director, Federal Housing Finance 

Agency. 

[FR Doc. 2012–31093 Filed 1–10–13; 8:45 am] 

BILLING CODE 8070–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2012–0416; Directorate 

Identifier 2012–NE–13–AD; Amendment 39– 

17303; AD 2012–26–08] 

RIN 2120–AA64 

Airworthiness Directives; Pratt & 

Whitney Canada Corp. Turboprop 

Engines 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: We are superseding an 

existing airworthiness directive (AD) for 

all Pratt & Whitney Canada Corp. 

(P&WC) PW118, PW118A, PW118B, 

PW119B, PW119C, PW120, PW120A, 

PW121, PW121A, PW123, PW123B, 

PW123C, PW123D, PW123E, PW123AF, 

PW124B, PW125B, PW126A, PW127, 

PW127E, PW127F, PW127G, and 

PW127M turboprop engines. That AD 

currently requires initial and repetitive 

inspections of certain serial numbers (S/ 

Ns) of propeller shafts for cracks and 

removal from service if found cracked. 

This new AD requires the same actions, 

but requires removal from service of 

affected propeller shafts as mandatory 

terminating action to the repetitive 

inspections. This AD was prompted by 

reports of two propeller shafts found 

cracked at time of inspection during 

maintenance. We are issuing this AD to 

detect propeller shaft cracks, which 

could cause failure of the shaft, 

propeller release, and loss of control of 

the airplane. 

DATES: This AD is effective February 15, 

2013. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of February 15, 2013. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain other publications listed in 

this AD as of July 20, 2012 (77 FR 

39624, July 5, 2012). 

ADDRESSES: For service information 

identified in this AD, contact Pratt & 

Whitney Canada Corp., 1000 MarieVictorin, Longueuil, Quebec, Canada, 

J4G 1A1; phone: 800–268–8000; fax: 

450–647–2888; Web site: www.pwc.ca. 

You may view this service information 

at the FAA, Engine & Propeller 

Directorate, 12 New England Executive 

Park, Burlington, MA. For information 

on the availability of this material at the 

FAA, call 781–238–7125. 

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: 

James Lawrence, Aerospace Engineer, 

Engine Certification Office, FAA, Engine 

& Propeller Directorate, 12 New England 

Executive Park, Burlington, MA 01803; 

email: james.lawrence@faa.gov; phone: 

781–238–7176; fax: 781–238–7199. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 to supersede AD 2012–11–14, 

Amendment 39–17078 (77 FR 39624, 

July 5, 2012). That AD applies to the 

specified products. The NPRM 

published in the Federal Register on 

September 14, 2012 (77 FR 56794). That 

NPRM proposed initial and repetitive 

inspections of certain S/Ns of propeller 

shafts for cracks and removal from 

service if found cracked. That NPRM 

also proposed to require the removal 

from service of affected propeller shafts 


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2332 Federal Register / Vol. 78, No. 8 / Friday, January 11, 2013 / Rules and Regulations 

as mandatory terminating action to the 

repetitive inspections. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

received no comments on the NPRM (77 

FR 56794, September 14, 2012). 

Conclusion 

We reviewed the relevant data and 

determined that air safety and the 

public interest require adopting the AD 

as proposed (77 FR 56794, September 

14, 2012). 

Costs of Compliance 

We estimate that this AD will affect 

570 P&WC engines installed on 

airplanes of U.S. registry. We estimate 

that it will take 6 hours per engine to 

remove the propeller shaft for 

inspection, 1 hour to perform the 

inspection, 65 hours to remove and 

reinstall the engine if needed, and 35 

hours to replace the propeller shaft. We 

estimate that consumable materials will 

cost $2,200 per engine, and required 

engine testing will cost $5,000. The 

average labor rate is $85 per hour. We 

expect that about 30 engines will be 

found with propeller shafts requiring a 

replacement propeller shaft. Based on 

these figures, we estimate the cost of the 

AD on U.S. operators to be $1,028,850. 

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 have determined that 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 

the DOT Regulatory Policies and 

Procedures (44 FR 11034, February 26, 

1979), 

(3) Will not affect intrastate aviation 

in Alaska to the extent that it justifies 

making a regulatory distinction, 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. 

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 

removing airworthiness directive (AD) 

2012–11–14, Amendment 39–17078 (77 

FR 39624, July 5, 2012), and adding the 

following new AD: 

2012–26–08 Pratt & Whitney Canada Corp: 

Amendment 39–17303 ; Docket No. 

FAA–2012–0416; Directorate Identifier 

2012–NE–13–AD. 

(a) Effective Date 

This airworthiness directive (AD) is 

effective February 15, 2013. 

(b) Affected ADs 

This AD supersedes AD 2012–11–14 (77 

FR 39624, July 5, 2012). 

(c) Applicability 

This AD applies to all Pratt & Whitney 

Canada Corp. (P&WC) PW118, PW118A, 

PW118B, PW119B, PW119C, PW120, 

PW120A, PW121, PW121A, PW123, 

PW123B, PW123C, PW123D, PW123E, 

PW123AF, PW124B, PW125B, PW126A, 

PW127, PW127E, PW127F, PW127G, and 

PW127M turboprop engines, with the serial 

number (S/N) propeller shafts listed in P&WC 

Alert Service Bulletin (ASB) No. PW100–72– 

A21813, Revision 3, dated March 21, 2012, 

ASB No. PW100–72–A21802, Revision 4, 

dated March 16, 2012, and ASB No. PW100– 

72–A21798, Revision 5, dated March 20, 

2012. 

(d) Unsafe Condition 

This AD was prompted by reports of two 

propeller shafts found cracked at time of 

inspection during maintenance. We are 

issuing this AD to detect propeller shaft 

cracks, which could cause failure of the shaft, 

propeller release, and loss of control of the 

airplane. 

(e) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(f) Inspecting Propeller Shafts 

(1) For propeller shafts with an S/N listed 

in Table 1 and Table 2 of P&WC ASB No. 

PW100–72–A21813, Revision 3, dated March 

21, 2012: 

(i) For engines not yet initially inspected 

per AD 2012–11–14 (77 FR 39624, July 5, 

2012), before further flight, perform either an 

initial visual inspection or an initial 

ultrasonic inspection (UI) for cracks, in 

accordance with paragraphs 3.C.(1) through 

3.C.(1)(a), and 3.C.(2) of P&WC ASB No. 

PW100–72–A21813, Revision 3, dated March 

21, 2012, and Section 9 of P&WC Special 

Instruction (SI) P&WC No. 22–2012, R2, 

dated April 4, 2012. 

(ii) If the visual inspection was performed, 

repeat the visual inspection within 50 engine 

flight hours (EFH) after the initial inspection, 

and thereafter within every 10 EFH, until the 

propeller shaft is removed from service. 

(iii) If the UI was performed, repeat the UI 

at intervals not to exceed 1,000 EFH, until 

the propeller shaft is removed from service. 

(2) If a crack is found during any of the 

inspections required by this AD, remove the 

propeller shaft from service before the next 

flight. 

(g) Mandatory Terminating Action 

As mandatory terminating action to the 

repetitive inspections required by this AD: 

(1) For propeller shafts with an S/N listed 

in Table 1 of P&WC ASB No. PW100–72– 

A21802, Revision 4, dated March 16, 2012, 

remove the propeller shafts from service 

before further flight. 

(2) For affected S/N propeller shafts listed 

in Table 1 of P&WC ASB No. PW100–72– 

A21798, Revision 5, dated March 20, 2012, 

remove the propeller shafts from service 

within 6 months after the effective date of 

this AD. 

(3) For affected S/N propeller shafts listed 

in Table 2 of P&WC ASB No. PW100–72– 

A21798, Revision 5, dated March 20, 2012, 

remove the propeller shafts from service 

within 12 months after the effective date of 

this AD. 

(h) Installation Prohibition 

(1) After the effective date of this AD, do 

not install any propeller shaft S/Ns listed in 

Table 1 of P&WC ASB No. PW100–72– 

A21802, Revision 4, dated March 16, 2012, 

into any engine. 

(2) After the effective date of this AD, do 

not install any propeller shaft S/Ns listed in 

Table 1 and Table 2 of P&WC ASB No. 

PW100–72–A21798, Revision 5, dated March 

20, 2012, into any engine. 


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Federal Register / Vol. 78, No. 8 / Friday, January 11, 2013 / Rules and Regulations 2333 

(i) Credit for Actions Accomplished in 

Accordance With Previous Service 

Information 

(1) Initial inspections performed before the 

effective date of this AD using P&WC ASB 

No. PW100–72–A21813, Revision 3, dated 

March 21, 2012 or earlier revisions satisfy the 

initial inspection requirements of paragraph 

(f) of this AD. However, you must perform 

the repetitive inspection intervals specified 

in paragraph (f). 

(2) Ultrasonic inspections performed before 

the effective date of this AD per Special 

Instruction P&WC 22–2012R2, dated April 4, 

2012, or earlier revisions satisfy the 

requirements of paragraph (f) of this AD. 

(j) Alternative Methods of Compliance 

(AMOCs) 

The Manager, Engine Certification Office, 

may approve AMOCs for this AD. Use the 

procedures found in 14 CFR 39.19 to make 

your request. 

(k) Related Information 

(1) For more information about this AD, 

contact James Lawrence, Aerospace Engineer, 

Engine Certification Office, FAA, Engine & 

Propeller Directorate, 12 New England 

Executive Park, Burlington, MA 01803; 

email: james.lawrence@faa.gov; phone: 781– 

238–7176; fax: 781–238–7199. 

(2) Refer to Transport Canada AD CF– 

2012–12, dated March 26, 2012, for related 

information. 

(l) Material Incorporated by Reference 

(1) The Director of the Federal Register 

approved the incorporation by reference 

(IBR) of the service information listed in this 

paragraph under 5 U.S.C. 552(a) and 1 CFR 

part 51. 

(2) You must use this service information 

as applicable to do the actions required by 

this AD, unless the AD specifies otherwise. 

(i) Pratt & Whitney Canada Alert Service 

Bulletin ASB No. PW100–72–A21798, 

Revision 5, dated March 20, 2012. 

(ii) Reserved. 

(3) The following service information was 

approved for IBR on July 20, 2012, (77 FR 

39624, July 5, 2012). 

(i) Pratt & Whitney Canada Alert Service 

Bulletin No. PW100–72–A21813, Revision 3, 

dated March 21, 2012. 

(ii) Pratt & Whitney Canada Alert Service 

Bulletin No. PW100–72–A21802, Revision 4, 

dated March 16, 2012. 

(iii) Pratt & Whitney Canada Special 

Instruction P&WC 22–2012R2, dated April 4, 

2012. 

(4) For Pratt & Whitney Canada service 

information identified in this AD, contact 

Pratt & Whitney Canada Corp., 1000 MarieVictorin, Longueuil, Quebec, Canada, J4G 

1A1; phone: 800–268–8000; fax: 450–647– 

2888; Web site: www.pwc.ca. 

(5) You may view this service information 

at the FAA, Engine & Propeller Directorate, 

12 New England Executive Park, Burlington, 

MA. For information on the availability of 

this material at the FAA, call 781–238–7125. 

(6) You may view this service information 

at the National Archives and Records 

Administration (NARA). For information on 

the availability of this material at NARA, call 

202–741–6030, or go to: http:// 

www.archives.gov/federal-register/cfr/ibrlocations.html. 

Issued in Burlington, Massachusetts, on 

December 21, 2012. 

Colleen M. D’Alessandro, 

Assistant Manager, Engine & Propeller 

Directorate, Aircraft Certification Service. 

[FR Doc. 2012–31361 Filed 1–10–13; 8:45 am] 

BILLING CODE 4910–13–P 

ENVIRONMENTAL PROTECTION 

AGENCY 

40 CFR Parts 61 and 63 

[EPA–R01–OAR–2012–0430; FRL–9697–2] 

Approval of the Clean Air Act, Section 

112(l), Authority for Hazardous Air 

Pollutants: Asbestos Management and 

Control; State of New Hampshire 

Department of Environmental Services 

AGENCY: Environmental Protection 

Agency (‘‘EPA’’). 

ACTION: Direct final rule. 

SUMMARY: Under the Clean Air Act 

(‘‘CAA’’) and Federal regulations 

promulgated there under, the New 

Hampshire Department of 

Environmental Services (‘‘NH DES’’) 

submitted a request for approval to 

implement and enforce the readopted 

and re-codified ‘‘Env-Sw 2100: 

Management and Control of Asbestos 

Disposal Sites Not Operated after July 9, 

1981,’’ and the amended ‘‘Env-A 1801– 

1807.01: Asbestos Management and 

Control,’’ (amended Asbestos 

Management Rules) in place of the 

National Emission Standard for 

Asbestos (‘‘Asbestos NESHAP’’). EPA 

has reviewed this request and has 

determined that the amended Asbestos 

Management Rules satisfy the 

requirements necessary for approval. 

Thus, EPA is hereby granting NH DES 

the authority to implement and enforce 

the amended Asbestos Management 

Rules in place of the Asbestos NESHAP. 

This approval makes NH DES’s 

amended Asbestos Management Rules 

federally enforceable. 

DATES: This direct final rule will be 

effective March 12, 2013, unless EPA 

receives adverse comments by February 

11, 2013. If adverse comments are 

received, EPA will publish a timely 

withdrawal of the direct final rule in the 

Federal Register informing the public 

that the rule will not take effect. The 

incorporation by reference of certain 

publications listed in the rule is 

approved by the Director of the Federal 

Register as of March 12, 2013. 

ADDRESSES: Submit your comments, 

identified by Docket ID Number EPA– 

R01–OAR–2012–0430 by one of the 

following methods: 

1. www.regulations.gov: Follow the 

on-line instructions for submitting 

comments. 

2. Email: mcdonnell.ida@epa.gov. 

3. Fax: (617) 918–0653. 

4. Mail: ‘‘EPA–R01–OAR–2012– 

0430’’, Ida E. McDonnell, U.S. 

Environmental Protection Agency, EPA 

New England Regional Office, 5 Post 

Office Square (mail code OEP05–2), 

Boston, MA 02109–3912. 

5. Hand Delivery or Courier: Deliver 

your comments to: Ida McDonnell, 

Manager, Air Permits, Toxics and 

Indoor Programs Unit, Office of 

Ecosystem Protection, U.S. 

Environmental Protection Agency, EPA 

New England Regional Office, 5 Post 

Office Square, 5th floor, (OEP05–2), 

Boston, MA 02109–3912. Such 

deliveries are only accepted during the 

Regional Office’s normal hours of 

operation. The Regional Office’s official 

hours of business are Monday through 

Friday, 8:30 to 4:30, excluding legal 

holidays. 

Instructions: Direct your comments to 

Docket ID No. EPA–R01–OAR–2012– 

0430. EPA’s policy is that all comments 

received will be included in the public 

docket without change and may be 

made available online at 

www.regulations.gov, including any 

personal information provided, unless 

the comment includes information 

claimed to be Confidential Business 

Information (‘‘CBI’’) or other 

information whose disclosure is 

restricted by statute. Do not submit 

through www.regulations.gov, or email, 

information that you consider to be CBI 

or otherwise protected. The 

www.regulations.gov Web site is an 

‘‘anonymous access’’ system, which 

means EPA will not know your identity 

or contact information unless you 

provide it in the body of your comment. 

If you send an email comment directly 

to EPA without going through 

www.regulations.gov your email address 

will be automatically captured and 

included as part of the comment that is 

placed in the public docket and made 

available on the Internet. If you submit 

an electronic comment, EPA 

recommends that you include your 

name and other contact information in 

the body of your comment and with any 

disk or CD–ROM you submit. If EPA 

cannot read your comment due to 

technical difficulties and cannot contact 

you for clarification, EPA may not be 

able to consider your comment. 

Electronic files should avoid the use of 

special characters, any form of 

encryption, and be free of any defects or 

viruses. EPA will forward copies of all 


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