49662 Federal Register / Vol. 78, No. 158 / Thursday, August 15, 2013 / Rules and Regulations 

(MI). We are issuing this AD to prevent 

corrosion that could result in propeller 

failure and loss of airplane control. 

(e) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(f) MI for Blades and Hubs That Have an 

Updated Airworthiness Limitations Section 

(ALS) 

For Hamilton Sundstrand Corporation 

propeller models 14RF–9, 14RF–21, 14SF–5, 

14SF–7, 14SF–11E, and 568F–1, that have an 

approved update to the ALS, within 45 days 

after the effective date of this AD, perform an 

MI on the blades and hubs no later than 

seven years after the date since installation 

(DSI). The DSI will begin at initial 

installation after the most recent MI or initial 

installation after production. Guidance on 

the inspections can be found in the 

applicable Hamilton Sundstrand Corporation 

models/manuals 14RF–9/P5186, revision 12, 

January 20, 2012; 14RF–21/P5189, revision 8, 

February 20, 2013; 14SF–5/P5188, revision 

10, dated January 14, 2013; 14SF–7/P5185, 

revision 13, dated December 13, 2011; 14SF– 

11E/P5207, revision 2, dated June 28, 2012; 

and 568F–1/P5206, revision 9, dated 

February 22, 2013. 

(g) MI for Blades and Hubs That Do Not 

Have an Updated ALS 

For Hamilton Standard Division propeller 

models 6/5500/F and 24PF and Hamilton 

Sundstrand Corporation propeller models 

14RF–19, 14RF–37, 14SF–11, 14SF–15, 

14SF–23, 14SF–17, 14SF–19, 247F–1, 247F– 

1E, 247F–3, 568F–1, 568F–5, and 568F–7, 

that do not have an approved update to the 

ALS, within one year after the effective date 

of this AD, perform an MI on the blades and 

hubs no later than seven years after the DSI. 

The DSI will begin at initial installation after 

the most recent MI or initial installation after 

production. Guidance on the inspections can 

be found in the applicable Hamilton 

Standard Division models/manuals 6/5500/ 

F/P5190 and 24PF/61–12–01, and Hamilton 

Sundstrand Corporation models/manuals 

14RF–19/P5199, 14RF–37/P5209, 14SF–11/ 

P5196, 14SF–15/P5197, 14SF–23/P5197, 

14SF–17/P5198, 14SF–19/P5198, 247F–1/ 

P4202, 247F–1E/P5204, 247F–3/P5205, 

568F–1/P5214, 568F–5/P5203, and 568F–7/ 

P5211. 

(h) Alternative Methods of Compliance 

(AMOCs) 

The Manager, Boston Aircraft Certification 

Office, FAA, may approve AMOCs for this 

AD. Use the procedures found in 14 CFR 

39.19 to make your request. 

(i) Related Information 

(1) For more information about this AD, 

contact Michael Schwetz, Aerospace 

Engineer, Boston Aircraft Certification Office, 

FAA, 12 New England Executive Park, 

Burlington, MA 01803; phone: 781–238– 

7761; fax: 781–238–7170; email: 

michael.schwetz@faa.gov. 

(2) Hamilton Sundstrand Corporation 

models/manuals 14RF–9/P5186, revision 12, 

January 20, 2012; 14RF–21/P5189, revision 8, 

February 20, 2013; 14SF–5/P5188, revision 

10, dated January 14, 2013; 14SF–7/P5185, 

revision 13, dated December 13, 2011; 14SF– 

11E/P5207, revision 2, dated June 28, 2012; 

and 568F–1/P5206, revision 9, dated 

February 22, 2013, which are not 

incorporated by reference in this AD, can be 

obtained from Hamilton Sundstrand 

Corporation, using the contact information in 

paragraph (i)(3) of this AD. 

(3) For service information identified in the 

AD, contact Hamilton Sundstrand 

Corporation, One Hamilton Road, Mail Stop 

1A–3–C63, Windsor Locks, CT 06096–1010; 

or Hamilton Standard Division, United 

Technologies Corporation, One Hamilton 

Road, Mail Stop 1A–3–C63, Windsor Locks, 

CT 06096–1010; phone: 877–808–7575; fax: 

860–660–0372; email: 

tech.solutions@hs.utc.com; Internet: http:// 

myhs.hamiltonsundstrand.com. You may 

view this service information at the FAA, 

Engine & Propeller Directorate, 12 New 

England Executive Park, Burlington, MA 

01803. For information on the availability of 

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

(j) Material Incorporated by Reference 

None. 

Issued in Burlington, Massachusetts, on 

August 2, 2013. 

Carlos A. Pestana, 

Acting Assistant Directorate Manager, Engine 

& Propeller Directorate, Aircraft Certification 

Service. 

[FR Doc. 2013–19649 Filed 8–9–13; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2013–0472; Directorate 

Identifier 98–CE–097–AD; Amendment 39– 

17538; AD 99–07–10 R1] 

RIN 2120–AA64 

Airworthiness Directives; PIAGGIO 

AERO INDUSTRIES S.p.A Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule; rescission. 

SUMMARY: We are rescinding an 

airworthiness directive (AD) for 

PIAGGIO AERO INDUSTRIES S.p.A. 

Model P–180 airplanes. The rescinded 

AD resulted from mandatory continuing 

airworthiness information (MCAI) 

originated 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 partial detachment of the 

inner protective film of the composite 

nacelles. Since issuance of the 

rescinded AD, we have determined that 

the unsafe condition does not exist or is 

not likely to develop on affected type 

design airplanes. 

DATES: This AD is effective September 

19, 2013. 

ADDRESSES: 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 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. 

FOR FURTHER INFORMATION CONTACT: 

Mike Kiesov, Aerospace Engineer, FAA, 

Small Airplane Directorate, 901 Locust, 

Room 301, Kansas City, Missouri 64106; 

telephone: (816) 329–4144; fax: (816) 

329–4090; email: mike.kiesov@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 by rescinding AD 99–07–10 (64 

FR 14824, March 29, 1999) that applied 

to the specified products. The NPRM 

was published in the Federal Register 

on May 30, 2013 (78 FR 32363). 

On March 18, 1999, we issued AD 99– 

07–10, Amendment 39–11095 (64 FR 

14824, March 29, 1999), with an 

effective date of May 10, 1999. The AD 

required actions intended to address an 

unsafe condition on the products listed 

above. 

Since we issued AD 99–07–10, 

Amendment 39–11095 (64 FR 14824, 

March 29, 1999), the European Aviation 

Safety Agency (EASA), which is the 

Technical Agent for the Member States 

of the European Community, has issued 

AD Cancellation Notice No.: 2013– 

0085–CN, dated April 8, 2013, which 

cancelled Ente Nazionale per 

l’Aviazione Civile (ENAC) (the 

airworthiness authority for Italy) AD No. 

98–208, dated June 9, 1998. Italian AD 

No. 98–208 required the inspections and 

corrective actions of Piaggio Service 

Bulletin (Mandatory) No.: SB–80–0101, 

Original Issue: May 6, 1998. AD 99–07– 

10, Amendment 39–11095 (64 FR 

14824, March 29, 1999), is the result of 

mandatory continuing airworthiness 

information (MCAI) issued by ENAC. 

We have been notified that since 

2000, all nacelles for PIAGGIO AERO 

INDUSTRIES S.p.A Model P–180 

airplanes have been manufactured by a 

different supplier, and no new 

occurrences of film detachment have 

been reported on earlier manufactured 

airplanes. Therefore, nacelle inner panel 


tkelley on DSK3SPTVN1PROD with RULES
Federal Register / Vol. 78, No. 158 / Thursday, August 15, 2013 / Rules and Regulations 49663 

protective film detachment is no longer 

considered probable. Consequently, 

PIAGGIO AERO INDUSTRIES S.p.A. 

issued Mandatory Service Bulletin No. 

SB 80–0101, Rev. N. ZZ, dated February 

19, 2013, to cancel the previous revision 

of this service bulletin. 

Refer to MCAI European Aviation 

Safety Agency (EASA) AD No.: AD 

Cancellation Notice No.: 2013–0085– 

CN, dated April 8, 2013, and Ente 

Nazionale per l’Aviazione Civile 

(ENAC) AD No. 98–208, dated June 9, 

1998, for related information; both may 

be found in the AD docket on the 

Internet at http://www.regulations.gov. 

You may also refer to Piaggio Service 

Bulletin (Mandatory) No.: SB 80 0101, 

Original Issue: May 6, 1998, for related 

information. For service information 

related to this AD, contact Piaggio Aero 

Industries S.p.A Airworthiness Office; 

Via Luigi Cibrario, 4–16154 Genova– 

Italy; telephone: +39 010 6481353; fax: 

+39 010 6481881; email: 

airworthiness@piaggioaero.it; Internet: 

www.piaggioaero.com/#/en/after-sales/ 

service-support. You may review copies 

of the referenced service information at 

the FAA, Small Airplane Directorate, 

901 Locust, Kansas City, Missouri 

64106. For information on the 

availability of this material at the FAA, 

call (816) 329–4148. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

received no comments on the NPRM (78 

FR 32363, May 30, 2013). 

Conclusion 

We reviewed the relevant data and 

determined that rescinding the AD will 

not affect air safety and will reduce the 

burden on the public. We will rescind 

the AD as proposed except for minor 

editorial changes. We have determined 

that these minor changes: 

• Are consistent with the intent that 

was proposed in the NPRM (78 FR 

32363, May 30, 2013) for correcting the 

unsafe condition; and 

• Do not add any additional burden 

upon the public than was already 

proposed in the NPRM (78 FR 32363, 

May 30, 2013). 

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 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. 

Adoption of the 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 

removing AD 99–07–10, Amendment 

39–11095 (64 FR 14824, March 29, 

1999), and adding the following new 

AD: 

AD 99–07–10 R1 PIAGGIO AERO 

INDUSTRIES S.p.A: Amendment 39– 

17538; Docket No. FAA–2013–0472; 

Directorate Identifier 98–CE–097–AD. 

(a) Effective Date 

This airworthiness directive (AD) becomes 

effective September 19, 2013. 

(b) Affected ADs 

This AD rescinds AD 99–07–10, 

Amendment 39–11095 (64 FR 14824, March 

29, 1999). 

(c) Applicability 

This AD applies to PIAGGIO AERO 

INDUSTRIES S.p.A Model P–180 airplanes, 

all serial numbers, certificated in any 

category. 

(d) Subject 

Joint Aircraft System Component (JASC)/ 

Air Transport Association (ATA) of America 

Code 54; Nacelles/Pylons. 

Issued in Kansas City, Missouri, on July 25, 

2013. 

Earl Lawrence, 

Manager, Small Airplane Directorate, Aircraft 

Certification Service. 

[FR Doc. 2013–19816 Filed 8–14–13; 8:45 am] 

BILLING CODE 4910–13–P 

COMMODITY FUTURES TRADING 

COMMISSION 

17 CFR Part 39 

RIN 3038–AC98 

Enhanced Risk Management 

Standards for Systemically Important 

Derivatives Clearing Organizations 

AGENCY: Commodity Futures Trading 

Commission. 

ACTION: Final rule. 

SUMMARY: The Commodity Futures 

Trading Commission (‘‘Commission’’ or 

‘‘CFTC’’) is adopting final regulations to 

implement enhanced risk management 

standards for systemically important 

derivatives clearing organizations that 

include increased financial resources 

requirements for systemically important 

derivatives clearing organizations that 

are involved in activities with a more 

complex risk profile or that are 

systemically important in multiple 

jurisdictions, the prohibited use of 

assessments by systemically important 

derivatives clearing organizations in 

calculating their available default 

resources, and enhanced system 

safeguards for systemically important 

derivatives clearing organizations for 

business continuity and disaster 

recovery (‘‘BC–DR’’). This final rule also 

implements special enforcement 

authority over systemically important 

derivatives clearing organizations 

granted to the Commission under 

section 807(c) of the Dodd-Frank Wall 

Street Reform and Consumer Protection 

Act (‘‘Dodd-Frank Act’’). 


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