Federal Register / Vol. 78, No. 107 / Tuesday, June 4, 2013 / Rules and Regulations 33197 

(i) Boeing Special Attention Service 

Bulletin 747–25–3381, Revision 1, dated May 

17, 2012. 

(ii) Boeing Special Attention Service 

Bulletin 767–25–0381, Revision 1, dated 

September 17, 2012. 

(iii) Boeing Special Attention Service 

Bulletin 777–25–0362, dated August 19, 

2010. 

(3) For service information identified in 

this AD, contact Boeing Commercial 

Airplanes, Attention: Data & Services 

Management, P.O. Box 3707, MC 2H–65, 

Seattle, WA 98124–2207; telephone 206– 

544–5000, extension 1; fax 206–766–5680; 

Internet https://www.myboeingfleet.com. 

(4) You may review copies of the 

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. 

(5) You may view this service information 

that is incorporated by reference 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 Renton, Washington, on May 16, 

2013. 

Jeffrey E. Duven, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2013–12717 Filed 6–3–13; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2013–0455; Directorate 

Identifier 2013–CE–013–AD; Amendment 

39–17461; AD 2013–11–01] 

RIN 2120–AA64 

Airworthiness Directives; Iniziative 

Industriali Italiane S.p.A. Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; request for comments 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for 

Iniziative Industriali Italiane S.p.A. 

Models Sky Arrow 650 TC, Sky Arrow 

650 TCN, Sky Arrow 650TCS, and Sky 

Arrow 650TCNS airplanes. This AD 

results from mandatory continuing 

airworthiness information (MCAI) 

issued by the aviation authority of 

another country to identify and correct 

an unsafe condition on an aviation 

product. The MCAI describes the unsafe 

condition as improper installation of the 

spherical bearing on the central hinge 

lever and a crack on the weld length of 

the horizontal tail/elevator plane hinge 

assembly. We are issuing this AD to 

require actions to address the unsafe 

condition on these products. 

DATES: This AD is effective June 19, 

2013. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in the AD 

as of June 19, 2013. 

We must receive comments on this 

AD by July 19, 2013. 

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 20590, 

between 9 a.m. and 5 p.m., Monday 

through Friday, except Federal holidays. 

For service information identified in 

this AD, contact Magnaghi Aeronautica 

S.p.A., Via G. Ferraris, 76, 80142 

Napoli, Italy; telephone: + 39 081 5977 

225; fax: + 39 081 5977 226; email: 

dtedesco@magnaghiaeronautica.it; 

Internet: www.magnaghiaeronautica.it. 

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. 

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 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: 

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 

The European Aviation Safety Agency 

(EASA), which is the Technical Agent 

for the Member States of the European 

Community, has issued AD No. 2013– 

0073–E, dated March 21, 2013 (referred 

to after this as ‘‘the MCAI’’), to correct 

an unsafe condition for the specified 

products. The MCAI states: 

During an inspection on elevator/stabilizer 

hinges, improper installation of the spherical 

bearing part number (P/N) SKF GE–10 on the 

central hinge lever and a crack on the weld 

length of the horizontal tail/elevator plane 

hinge assembly have been reported. 

This condition, if not detected and 

corrected, could lead to the loss of the main 

elevator control. 

To address this potential unsafe condition, 

Magnaghi Aeronautica issued Service 

Bulletin (SB–C) n. SB–005–2013–SKY 

ARROW to inspect the affected areas of the 

pitch flight control system. 

For the reasons described above, this AD 

requires inspection of the spherical bearing 

and the horizontal tail/elevator plane hinge 

assembly to detect any crack, signs of 

corrosion or improper installation, and 

accomplishment of the applicable corrective 

actions. 

The MCAI also requires sending a 

detailed report of any crack, signs of 

corrosion, or improper installation 

found during the required inspections to 

Magnaghi Aeronautica S.p.A.; 

requesting an FAA-approved repair 

scheme; and incorporating the repair . 

You may obtain further information by 

examining the MCAI in the AD docket. 

Relevant Service Information 

Magnaghi Aeronautica SpA has 

issued Service Bulletin SB–C n. SB– 

005–2013–SKY ARROW, Issue 1, dated 

March 13, 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 the 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 this State of 

Design Authority, 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 the State of 

Design Authority and determined the 

unsafe condition exists and is likely to 

exist or develop on other products of the 

same type design. 


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33198 Federal Register / Vol. 78, No. 107 / Tuesday, June 4, 2013 / Rules and Regulations 

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 This condition, which, if 

not corrected, could lead to the loss of 

the main elevator control and result in 

loss of control. 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–2013–0455; 

Directorate Identifier 2013–CE–013– 

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 we receive 

about this AD. 

Costs of Compliance 

We estimate that this AD will affect 9 

products of U.S. registry. We also 

estimate that it will take about 2 workhours per product to comply with the 

basic requirements of this AD. The 

average labor rate is $85 per work-hour. 

Based on these figures, we estimate 

the cost of the AD on U.S. operators to 

be $1,530, or $170 per product. 

We are unable to estimate the costs to 

accomplish any necessary repair that 

will be required based on the results of 

any required inspection. Magnaghi 

Aeronautica S.p.A. will evaluate the 

damage of each affected airplane and 

develop an appropriate repair scheme. 

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 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, 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 adding 

the following new AD: 

2013–11–01 Iniziative Industriali Italiane 

S.p.A.: Amendment 39–17461; Docket 

No. FAA–2013–0455; Directorate 

Identifier 2013–CE–013–AD. 

(a) Effective Date 

This airworthiness directive (AD) becomes 

effective June 19, 2013. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to Iniziative Industriali 

Italiane S.p.A. Models Sky Arrow 650 TC, 

Sky Arrow 650 TCN, Sky Arrow 650TCS, and 

Sky Arrow 650TCNS airplanes, all serial 

numbers, certificated in any category. 

(d) Subject 

Air Transport Association of America 

(ATA) Code 27: Flight Controls. 

(e) Reason 

This AD was prompted by mandatory 

continuing airworthiness information (MCAI) 

issued by the aviation authority of another 

country to identify and correct an unsafe 

condition on an aviation product. The MCAI 

describes the unsafe condition as improper 

installation of the spherical bearing on the 

central hinge lever and a crack on the weld 

length of the horizontal tail/elevator plane 

hinge assembly. We are issuing this AD to 

correct this condition, which, if not 

corrected, could lead to the loss of the main 

elevator control and could result in loss of 

control. 

(f) Actions and Compliance 

Unless already done, do the following 

actions. 

(1) Before further flight after June 19, 2013 

(the effective date of this AD), and thereafter 

at intervals not to exceed 25 hours time-inservice (TIS), perform detailed visual 

inspections of the horizontal tail/elevator 

plane hinge assembly part number (P/N) 

R26208/00 following paragraph 4. 

INSTRUCTIONS of Magnaghi Aeronautica 

SpA Service Bulletin SB–C n. SB–005–2013– 

SKY ARROW, Issue 1, dated March 13, 2013. 

(2) If during any inspection required by 

paragraph (f)(1) of this AD, the spherical 

bearing is found partially or completely out 

of its seat and/or signs of cracks or corrosion 

of the hinges, hinge levers or hinge brackets 

are detected, before further flight send a 

detailed report to Magnaghi Aeronautica 

S.p.A. following paragraph 4. 

INSTRUCTIONS of Magnaghi Aeronautica 

SpA Service Bulletin SB–C n. SB–005–2013– 

SKY ARROW, Issue 1, dated March 13, 2013, 

to the address specified in paragraph (i)(3) of 

this AD, requesting an FAA-approved repair 

scheme and incorporating the repair. 

(3) As of June 19, 2013 (the effective date 

of this AD) do not install any spherical 

bearing P/N SKF GE–10 or horizontal tail/ 

elevator plane hinge assembly P/N R26208/ 

00 on any airplane, unless it has passed the 

inspection following paragraph 4. 

INSTRUCTIONS of Magnaghi Aeronautica 

SpA Service Bulletin SB–C n. SB–005–2013– 

SKY ARROW, Issue 1, dated March 13, 2013. 

(g) Other FAA AD Provisions 

The following provisions also apply to this 

AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, Standards Office, 

FAA, has the authority to approve AMOCs 


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Federal Register / Vol. 78, No. 107 / Tuesday, June 4, 2013 / Rules and Regulations 33199 

for this AD, if requested using the procedures 

found in 14 CFR 39.19. Send information to 

ATTN: 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. Before 

using any approved AMOC on any airplane 

to which the AMOC applies, notify your 

appropriate principal inspector (PI) in the 

FAA Flight Standards District Office (FSDO), 

or lacking a PI, your local FSDO. 

(2) Airworthy Product: For any requirement 

in this AD to obtain corrective actions from 

a manufacturer or other source, use these 

actions if they are FAA-approved. Corrective 

actions are considered FAA-approved if they 

are approved by the State of Design Authority 

(or their delegated agent). You are required 

to assure the product is airworthy before it 

is returned to service. 

(3) Reporting Requirements: For any 

reporting requirement in this AD, a federal 

agency may not conduct or sponsor, and a 

person is not required to respond to, nor 

shall a person be subject to a penalty for 

failure to comply with a collection of 

information subject to the requirements of 

the Paperwork Reduction Act unless that 

collection of information displays a current 

valid OMB Control Number. The OMB 

Control Number for this information 

collection is 2120–0056. Public reporting for 

this collection of information is estimated to 

be approximately 5 minutes per response, 

including the time for reviewing instructions, 

completing and reviewing the collection of 

information. All responses to this collection 

of information are mandatory. Comments 

concerning the accuracy of this burden and 

suggestions for reducing the burden should 

be directed to the FAA at: 800 Independence 

Ave. SW., Washington, DC 20591, Attn: 

Information Collection Clearance Officer, 

AES–200. 

(h) Related Information 

Refer to MCAI European Aviation Safety 

Agency (EASA) AD No. 2013–0073–E, dated 

March 21, 2013, for related information. 

(i) 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) Magnaghi Aeronautica SpA Service 

Bulletin SB–C n. SB–005–2013–SKY 

ARROW, Issue 1, dated March 13, 2013. 

(ii) Reserved. 

(3) For Iniziative Industriali Italiane S.p.A. 

service information identified in this AD, 

contact Magnaghi Aeronautica S.p.A., Via G. 

Ferraris, 76, 80142 Napoli, Italy; telephone: 

+ 39 081 5977 225; fax: + 39 081 5977 226; 

email: dtedesco@magnaghiaeronautica.it; 

Internet: www.magnaghiaeronautica.it. 

(4) You may view this service information 

at 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. 

(5) You may view this service information 

that is incorporated by reference 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/ibr-locations.html 

Issued in Kansas City, Missouri, on May 

20, 2013. 

Earl Lawrence, 

Manager, Small Airplane Directorate, Aircraft 

Certification Service. 

[FR Doc. 2013–12516 Filed 6–3–13; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2012–1322; Directorate 

Identifier 2012–NM–155–AD; Amendment 

39–17466; AD 2013–11–06] 

RIN 2120–AA64 

Airworthiness Directives; Dassault 

Aviation Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 

Dassault Aviation Model MystereFalcon 900 and Falcon 900EX airplanes. 

This AD was prompted by reports of 

chafing between the tail strobe power 

supply and a hydraulic line. This AD 

requires modifying the tail strobe power 

supply wire routing. We are issuing this 

AD to prevent chafing between the tail 

strobe power supply and a hydraulic 

line, which could result in hydraulic 

fluid leakage and possible fire due to 

arcing, and consequent loss of control of 

the airplane due to structural failure of 

the tail. 

DATES: This AD becomes effective July 

9, 2013. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in this AD 

as of July 9, 2013. 

ADDRESSES: You may examine the AD 

docket on the Internet at http:// 

www.regulations.gov or in person at the 

U.S. Department of Transportation, 

Docket Operations, M–30, West 

Building Ground Floor, Room W12–140, 

1200 New Jersey Avenue SE., 

Washington, DC. 

FOR FURTHER INFORMATION CONTACT: Tom 

Rodriguez, Aerospace Engineer, 

International Branch, ANM–116, 

Transport Airplane Directorate, FAA, 

1601 Lind Avenue SW., Renton, 

Washington 98057–3356; telephone 

(425) 227–1137; fax (425) 227–1149. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 to include an AD that would 

apply to the specified products. That 

NPRM was published in the Federal 

Register on February 5, 2013 (78 FR 

8052). That NPRM proposed to correct 

an unsafe condition for the specified 

products. The European Aviation Safety 

Agency (EASA), which is the Technical 

Agent for the Member States of the 

European Community, has issued EASA 

Airworthiness Directive 2012–0162, 

dated August 29, 2012 (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: 

Two reports were received concerning 

Falcon 900 aeroplanes, where chafing 

between the tail strobe power supply and a 

hydraulic line was found. In the latest 

reported occurrence, the chafing damaged the 

power line and created an electrical arcing 

which created a pin hole in the hydraulic 

line, leading to hydraulic fluid leakage. 

This condition, if not corrected, could 

jeopardize the aeroplane’s safe flight. 

To address this potential unsafe condition, 

Dassault Aviation developed modification 

(M5741) of the routing of the tail strobe 

power supply wire, which is available for 

accomplishment in service through Dassault 

Service Bulletin (SB) F900–431 or SB 

F900EX–437, as applicable to aeroplane 

model. 

For the reasons described above, this 

[EASA] AD requires modification of the 

routing of the tail strobe power supply wire. 

The unsafe condition is chafing between 

the tail strobe power supply and a 

hydraulic line, which could result in 

hydraulic fluid leakage and possible fire 

due to arcing, and consequent loss of 

control of the airplane due to structural 

failure of the tail. You may obtain 

further information by examining the 

MCAI in the AD docket. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

received no comments on the NPRM (78 

FR 8052, February 5, 2013) or on the 

determination of the cost to the public. 

Conclusion 

We reviewed the available data and 

determined that air safety and the 

public interest require adopting the AD 

as proposed—except for minor editorial 

changes. We have determined that these 

minor changes: 


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