Federal Register / Vol. 75, No. 165 / Thursday, August 26, 2010 / Rules and Regulations 52435 

on the mortgage recovery advance note; 

however, borrowers may voluntarily 

submit partial payments without 

incurring any prepayment penalty. 

(iii) The due date for the mortgage 

recovery advance note shall be the due 

date of the guaranteed note held by the 

Lender, as modified by the special loan 

servicing. Prior to the due date on the 

mortgage recovery advance note, 

payment in full under the note is due at 

the earlier of the following: 

(A) When the first lien mortgage and 

the guaranteed note are paid off; or 

(B) When the borrower transfers title 

to the property by voluntary or 

involuntary means. 

(iv) Repayment of all or part of the 

mortgage recovery advance must be 

remitted directly to RHS by the 

borrower. 

(v) RHS will collect this Federal debt 

from the borrower by any available 

means if the mortgage recovery advance 

is not repaid based on the terms 

outlined in the promissory note and 

mortgage or deed-of-trust. 

(4) The following provisions apply 

when a Lender files a claim with RHS 

for reimbursement of a mortgage 

recovery advance: 

(i) A claim for reimbursement in a 

form acceptable to RHS must be 

submitted to RHS within 60 days of the 

advance being executed by the borrower 

through his or her signature on the 

promissory note. 

(ii) When filing the claim for 

reimbursement with RHS, the Lender 

must: 

(A) Submit the original promissory 

note and a copy of the filed mortgage or 

deed-of-trust; 

(B) Include a summary of the amount 

of the funds advanced, including the 

monthly PITI and principal deferment 

(if applicable), and other account 

information indicating the borrower’s 

arrearage before the advance, as well as 

the present status of the account as of 

the date of the advance; 

(C) Provide the name, address, and tax 

ID number for the Lender; and 

(D) Provide the name, address, and 

phone number of a contact person for 

the Lender who can answer questions 

about the reimbursement request. 

(5) If a borrower defaults on his or her 

loan after receiving a mortgage recovery 

advance and a loss claim is filed by the 

Lender due to the default, any Agency 

reimbursement issued for the mortgage 

recovery advance to the Lender on 

behalf of the borrower will be credited 

toward the maximum loan guarantee 

amount payable by the Agency under 

the guarantee. 

Dated: August 18, 2010. 

Tammye Trevin ̃ o, 

Administrator Rural Housing Service. 

[FR Doc. 2010–21261 Filed 8–25–10; 8:45 am] 

BILLING CODE 3410–XV–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2010–0860; Directorate 

Identifier 2010–NE–28–AD; Amendment 39– 

16422; AD 2010–18–09] 

RIN 2120–AA64 

Airworthiness Directives; Pratt & 

Whitney Canada (P&WC) PW530A, 

PW545A, and PW545B Turbofan 

Engines 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; request for 

comments. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for the 

products listed above. This AD results 

from mandatory continuing 

airworthiness information (MCAI) 

issued 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: 

There have been reports of engine surge, 

lack of response to Power Lever input and 

crew commanded engine shutdown on 

PW530A/PW545A/PW545B engines powered 

aeroplanes. Investigation revealed engine 

intercompressor bleed valve/servo valve 

malfunction as the cause of the above 

problems, and that this problem is limited to 

engines fitted with low time (new or 

overhauled) bleed valve servo valves with 

either SB 30343 or 30404 incorporated. 

We are issuing this AD to prevent 

inflight loss of power of one or both of 

the engines and possible loss of control 

of the airplane. 

DATES: This AD becomes effective 

September 10, 2010. 

We must receive comments on this 

AD by September 27, 2010. The Director 

of the Federal Register approved the 

incorporation by reference of P&WC 

Alert Service Bulletin PW500–72– 

A30421, dated June 29, 2010, listed in 

the AD as of September 10, 2010. 

ADDRESSES: You may send comments by 

any of the following methods: 

• Federal eRulemaking Portal: Go to 

http://www.regulations.gov and follow 

the instructions for sending your 

comments electronically. 

• Mail: U.S. Department of 

Transportation, 1200 New Jersey 

Avenue, SE., West Building Ground 

Floor, Room W12–140, Washington, DC 

20590–0001. 

• Hand Delivery: Deliver to Mail 

address above between 9 a.m. and 5 

p.m., Monday through Friday, except 

Federal holidays. 

• Fax: (202) 493–2251. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http:// 

www.regulations.gov; or in person at the 

Docket Operations office 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 street address for 

the Docket Operations office (telephone 

(800) 647–5527) is the same as the Mail 

address provided in the ADDRESSES

section. Comments will be available in 

the AD docket shortly after receipt. 

FOR FURTHER INFORMATION CONTACT: 

James Lawrence, Aerospace Engineer, 

Engine Certification Office, FAA, Engine 

and Propeller Directorate, 12 New 

England Executive Park, Burlington, MA 

01803; e-mail: james.lawrence@faa.gov; 

telephone (781) 238–7176; fax (781) 

238–7199. 

SUPPLEMENTARY INFORMATION: 

Discussion 

Transport Canada, which is the 

aviation authority for Canada, has 

issued Canada Airworthiness Directive 

CF–2010–19, dated July 7, 2010 

(referred to after this as ‘‘the MCAI’’), to 

correct an unsafe condition for the 

specified products. The MCAI states: 

There have been reports of engine surge, 

lack of response to Power Lever input and 

crew commanded engine shutdown on 

PW530A/PW545A/PW545B engines powered 

aeroplanes. Investigation revealed engine 

intercompressor bleed valve/servo valve 

malfunction as the cause of the above 

problems, and that this problem is limited to 

engines fitted with low time (new or 

overhauled) bleed valve servo valves with 

either SB 30343 or 30404 incorporated. 

You may obtain further information by 

examining the MCAI in the AD docket. 

Relevant Service Information 

P&WC has issued Alert Service 

Bulletin (ASB) PW500–72–A30421, 

dated June 29, 2010. 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 AD 

This product has been approved by 

the aviation authority of Canada, and is 

approved for operation in the United 

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52436 Federal Register / Vol. 75, No. 165 / Thursday, August 26, 2010 / Rules and Regulations 

States. Pursuant to our bilateral 

agreement with Canada, they have 

notified us of the unsafe condition 

described in the MCAI and service 

information referenced above. We are 

issuing this AD because we evaluated 

all information provided by Canada and 

determined the unsafe condition exists 

and is likely to exist or develop on other 

products of the same type design. 

Differences Between the AD and the 

MCAI or Service Information 

The MCAI compliance requires action 

on at least one engine of the airplane. 

The FAA AD will require action on both 

engines within the defined compliance 

time and will not state ‘‘on at least one 

engine per airplane.’’ 

FAA’s Determination of the Effective 

Date 

An unsafe condition exists that 

requires the immediate adoption of this 

AD. The FAA has found that the risk to 

the flying public justifies waiving notice 

and comment prior to adoption of this 

rule because the unsafe condition is 

such that a possible twin engine, 

nonrecoverable surge could occur. 

There is insufficient time to issue an 

NPRM for public comment. Therefore, 

we determined that notice and 

opportunity for public comment before 

issuing this AD are impracticable and 

that good cause exists for making this 

amendment effective in fewer than 30 

days. 

Comments Invited 

This AD is a final rule that involves 

requirements affecting flight safety, and 

we did not precede it by notice and 

opportunity for public comment. We 

invite you to send any written relevant 

data, views, or arguments about this AD. 

Send your comments to an address 

listed under the ADDRESSES section. 

Include ‘‘Docket No. FAA–2010–0860; 

Directorate Identifier 2010–NE–28–AD’’ 

at the beginning of your comments. We 

specifically invite comments on the 

overall regulatory, economic, 

environmental, and energy aspects of 

this AD. We will consider all comments 

received by the closing date and may 

amend this 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 with FAA 

personnel concerning this AD. Using the 

search function of the Web site, anyone 

can find and read the comments in any 

of our dockets, including, if provided, 

the name of the individual who sent the 

comment (or signed the comment on 

behalf of an association, business, labor 

union, etc.). You may review the DOT’s 

complete Privacy Act Statement in the 

Federal Register published on April 11, 

2000 (65 FR 19477–78). 

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 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 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); and 

3. 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. 

We prepared a regulatory evaluation 

of the estimated costs to comply with 

this AD and placed it in the AD docket. 

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 adding 

the following new AD: 

2010–18–09 Pratt & Whitney Canada: 

Amendment 39–16422; Docket No. 

FAA–2010–0860; Directorate Identifier 

2010–NE–28–AD. 

Effective Date 

(a) This airworthiness directive (AD) 

becomes effective September 10, 2010. 

Affected ADs 

(b) None. 

Applicability 

(c) This AD applies to Pratt & Whitney 

Canada (P&WC) PW530A, PW545A, and 

PW545B turbofan engines that incorporate 

either P&WC Service Bulletin (SB) PW500– 

72–30343 or PW500–72–30404. These 

engines are installed on, but not limited to, 

Cessna Aircraft Company model 550 

(Citation Bravo) and model 560 (Citation 

Excel and XLS) airplanes. 

Reason 

(d) There have been reports of engine 

surge, lack of response to Power Lever input 

and crew commanded engine shutdown on 

PW530A/PW545A/PW545B engines powered 

aeroplanes. Investigation revealed engine 

intercompressor bleed valve/servo valve 

malfunction as the cause of the above 

problems, and that this problem is limited to 

engines fitted with low time (new or 

overhauled) bleed valve servo valves with 

either SB 30343 or 30404 incorporated. 

We are issuing this AD to prevent inflight 

loss of power of one or both of the engines 

and possible loss of control of the airplane. 

Actions and Compliance 

(e) Unless already done, do the following 

actions. 

(1) For engines that have an 

intercompressor bleed valve (BOV) servo 

valve with 250 or more hours time-in-service 

(TIS) since new or overhaul on the effective 

date of this AD, no further action is required. 

Remove Intercompressor Bleed Valve/Servo 

Valve 

(2) For engines that have a BOV servo valve 

with fewer than 50 hours TIS since new or 

overhaul on the effective date of this AD, 

remove the BOV servo valve from service as 

specified in Table 1 of this AD. 

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Federal Register / Vol. 75, No. 165 / Thursday, August 26, 2010 / Rules and Regulations 52437 

TABLE 1—BOV SERVO VALVE REMOVAL BY ENGINE MODEL AND SERVICE BULLETIN

Engine model Remove from service . . . 

PW530A and PW545A .................................................................................................... Within 15 hours TIS after the effective date of this AD. 

PW545B engines before incorporation of SB PW500–72–30311 ................................... Within 15 hours TIS after the effective date of this AD. 

PW545B engines after incorporation of SB PW500–72–30311 ...................................... Within 35 hours TIS after the effective date of this AD. 

Engine Testing 

(3) For engines that have a BOV servo valve 

with 50 hours or more TIS and fewer than 

250 hours TIS since new or overhaul on the 

effective date of this AD, test the engine as 

specified in P&WC Alert Service Bulletin 

(ASB) PW500–72–A30421, dated June 29, 

2010. Use the compliance times specified in 

Table 2 of this AD. 

TABLE 2—ENGINE TESTING BY ENGINE MODEL AND SERVICE BULLETIN

Engine model Perform test . . . 

PW530A and PW545A .................................................................................................... Within 15 hours TIS after the effective date of this AD. 

PW545B engines before incorporation of SB PW500–72–30311 ................................... Within 15 hours TIS after the effective date of this AD. 

PW545B engines after incorporation of SB PW500–72–30311 ...................................... Within 35 hours TIS after the effective date of this AD. 

(4) Thereafter, test the engine as specified 

in P&WC ASB PW500–72–A30421, dated 

June 29, 2010. Use the compliance times 

specified in Table 3 of this AD. 

TABLE 3—REPETITIVE ENGINE TESTING BY BOV TIS 

Time on BOV servo valve Repeat test 

Fewer than 100 hours TIS since new ............................................................................. Within 25 hours TIS since last inspection. 

100 or more hours TIS since new, but fewer than 250 hours TIS since new ................ Within 50 hours TIS since last inspection. 

250 or more hours TIS since new ................................................................................... No repetitive tests required. 

Optional Terminating Action 

(f) Replacing the BOV servo valve with a 

BOV servo valve that is not subject of this AD 

is terminating action to the testing 

requirements of paragraphs (e)(3) and (e)(4) 

of this AD. 

FAA AD Differences 

(g) This AD differs from the Mandatory 

Continuing Airworthiness Information 

(MCAI) in that while the MCAI requires 

initial mandatory action on only one engine 

per airplane with follow-on action to the 

second engine at a later compliance time, this 

AD requires initial action on both engines of 

the airplane at the same compliance time. 

Other FAA AD Provisions 

(h) Alternative Methods of Compliance 

(AMOCs): The Manager, Engine Certification 

Office, FAA, has the authority to approve 

AMOCs for this AD, if requested using the 

procedures found in 14 CFR 39.19. 

Related Information 

(i) Refer to MCAI Transport Canada 

Airworthiness Directive CF–2010–19, dated 

July 7, 2010. 

(j) Contact James Lawrence, Aerospace 

Engineer, Engine Certification Office, FAA, 

Engine and Propeller Directorate, 12 New 

England Executive Park, Burlington, MA 

01803; e-mail: james.lawrence@faa.gov; 

telephone (781) 238–7176; fax (781) 238– 

7199, for more information about this AD. 

Material Incorporated by Reference 

(k) You must use Pratt & Whitney Canada 

Alert Service Bulletin PW500–72–A30421, 

dated June 29, 2010, to do the actions 

required by this AD, unless the AD specifies 

otherwise. 

(1) The Director of the Federal Register 

approved the incorporation by reference of 

this service information under 5 U.S.C. 

552(a) and 1 CFR part 51. 

(2) For service information identified in 

this AD, contact Pratt & Whitney Canada 

Corp., 1000 Marie-Victorin, Longueuil, 

Quebec, Canada, J4G 1A1; telephone 800– 

268–8000; fax 450–647–2888; Web site: 

http://www.pwc.ca. 

(3) You may review copies at the FAA, 

New England Region, 12 New England 

Executive Park, Burlington, MA; or 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 

August 19, 2010. 

Peter A. White, 

Assistant Manager, Engine and Propeller 

Directorate, Aircraft Certification Service. 

[FR Doc. 2010–21331 Filed 8–25–10; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 95 

[Docket No.30742; Amdt. No. 489] 

IFR Altitudes; Miscellaneous 

Amendments 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: This amendment adopts 

miscellaneous amendments to the 

required IFR (instrument flight rules) 

altitudes and changeover points for 

certain Federal airways, jet routes, or 

direct routes for which a minimum or 

maximum en route authorized IFR 

altitude is prescribed. This regulatory 

action is needed because of changes 

occurring in the National Airspace 

System. These changes are designed to 

provide for the safe and efficient use of 

the navigable airspace under instrument 

conditions in the affected areas. 

DATES: Effective Date: 0901 UTC, 

September 23, 2010. 

FOR FURTHER INFORMATION CONTACT: 

Harry Hodges, Flight Procedure 

Standards Branch (AMCAFS–420), 

Flight Technologies and Programs 

Division, Flight Standards Service, 

Federal Aviation Administration, Mike 

mstockstill on DSKH9S0YB1PROD with RULES