41274 Federal Register / Vol. 78, No. 132 / Wednesday, July 10, 2013 / Rules and Regulations 

Where: 

LL,A = value as defined in section 11.2.7 of 

ASHRAE 103–1993, 

LG = value as defined in section 11.3.11.1 of 

ASHRAE 103–1993 at maximum input 

rate, 

LC = value as defined in section 11.3.11.2 of 

ASHRAE 103–1993 at maximum input 

rate, 

LJ = value as defined in section 11.4.8.1.1 of 

ASHRAE 103–1993 at maximum input 

rate, 

tON = value as defined in section 11.4.9.11 of 

ASHRAE 103–1993, 

QP = pilot flame fuel input rate determined 

in accordance with section 9.2 of 

ASHRAE 103–1993 in Btu/h, 

QIN = value as defined in section 11.4.8.1.1 

of ASHRAE 103–1993, 

tOFF = value as defined in section 11.4.9.12 

of ASHRAE 103–1993 at maximum input 

rate, 

LS,ON = value as defined in section 11.4.10.5 

of ASHRAE 103–1993 at maximum input 

rate, 

LS,OFF = value as defined in section 11.4.10.6 

of ASHRAE 103–1993 at maximum input 

rate, 

LI,ON = value as defined in section 11.4.10.7 

of ASHRAE 103–1993 at maximum input 

rate, 

LI,OFF = value as defined in section 11.4.10.8 

of ASHRAE 103–1993 at maximum input 

rate, 

CJ = value as defined in section 10.2 of this 

appendix, 

LS,SS = value as defined in section 11.5.6 of 

ASHRAE 103–1993 at maximum input 

rate, 

CS = value as defined in section 11.5.10.1 of 

ASHRAE 103–1993 at maximum input 

rate. 

* * * * * 

[FR Doc. 2013–16413 Filed 7–9–13; 8:45 am] 

BILLING CODE 6450–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2012–1067; Directorate 

Identifier 2011–NM–231–AD; Amendment 

39–17444; AD 2013–09–03] 

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 

FALCON 2000, FALCON 2000EX, 

MYSTERE–FALCON 900, and FALCON 

900EX airplanes; and all Model 

MYSTERE–FALCON 50 airplanes. This 

AD was prompted by reports that 

collapse of the main landing gear (MLG) 

could cause wing tank structure failure, 

which could result in fuel spillage and 

consequent fire hazard. This AD 

requires modification of the wing fuel 

tanks in the area of the wheel well. We 

are issuing this AD to prevent fuel 

spillage in the event of a MLG collapse, 

and consequent fire hazard. 

DATES: This AD becomes effective 

August 14, 2013. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in this AD 

as of August 14, 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, WA 

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 October 10, 2012 (77 FR 

61539). That NPRM proposed to correct 

an unsafe condition for the specified 

products. The Mandatory Continuing 

Airworthiness Information (MCAI) 

states: 

In service experience has shown that, in 

case of main landing gear collapse due to 

overloads during take off or landing (e.g., 

during high-speed runway excursions), the 

wing tank structure can fail, leading to fuel 

spillage. . . . 

This condition, if not corrected, could 

result, in case of main landing gear collapse, 

in a fuel spillage which may constitute a fire 

hazard. 

To address this unsafe condition, Dassault 

Aviation have developed a structural 

modification of the wing fuel tanks in the 

area of the wheel well which introduces a 

dry bay by adding a sealed boundary in front 

of the rear spar between ribs 4 and 5. 

For the reasons described above, this 

[European Aviation Safety Agency (EASA)] 

AD [2011–0193, dated October 5, 2011] 

requires accomplishment of the abovementioned modification for the Right Hand 

(RH) and Left Hand (LH) wing fuel tanks. 

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 

considered the comments received. 

Request for Updated Service 

Information 

Dassault Aviation requested that we 

revise the NPRM (77 FR 61539, October 

10, 2012) to reference Dassault 

Mandatory Service Bulletin F900–388, 

Revision 3, dated October 19, 2011. (We 

referred to Dassault Mandatory Service 

Bulletin F900–388, Revision 2, dated 

March 10, 2010, as the appropriate 

source of service information for certain 

airplanes for accomplishing the 

modification specified in paragraph (g) 

of the NPRM.) 

We agree. Dassault Mandatory Service 

Bulletin F900–388, Revision 3, dated 

October 19, 2011, clarifies the placard 

instructions for certain airplanes. We 

have updated the reference in paragraph 

(g)(3) of this AD to Dassault Mandatory 

Service Bulletin F900–388, Revision 3, 

dated October 19, 2011. We have also 

added paragraph (h)(3)(iii) to this AD to 

allow credit for actions done before the 

effective date of this AD using Dassault 

Mandatory Service Bulletin F900–388, 

Revision 2, dated March 10, 2010. 

Request for Clarification of Credit 

Service Bulletin 

Tidewater Inc. stated it has already 

complied with Dassault Mandatory 

Service Bulletin F2000EX–171, dated 

July 6, 2009, and requested we take that 

into consideration. The commenter 

noted that Dassault Mandatory Service 

Bulletin F2000EX–171, Revision 3, 

dated March 10, 2010, states that 

Dassault Mandatory Service Bulletin 

F2000EX–171, Revision 1, dated 

October 22, 2009; Revision 2, dated 

February 15, 2010; and Revision 3, 

dated March 10, 2010; are not 

applicable to aircraft already modified 

as specified in the original service 

bulletin. 

We agree to clarify. Dassault 

Mandatory Service Bulletin F2000EX– 

171, Revision 3, dated March 10, 2010, 

does specifically state that Revision 3 is 

‘‘not applicable to aircraft already 

changed per the original issue or 

revision 1 or revision 2.’’ Also, as 

proposed in the NPRM (77 FR 61539, 

October 10, 2012), paragraph (h) of this 

AD states that credit is allowed for 

actions done before the effective date of 

this AD using certain service 

information, including Dassault 

Mandatory Service Bulletin F2000EX– 

171, dated July 6, 2009; Revision 1, 

dated October 22, 2009; and Revision 2, 

dated February 15, 2010; as specified in 


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Federal Register / Vol. 78, No. 132 / Wednesday, July 10, 2013 / Rules and Regulations 41275 

paragraph (h)(5) of this AD. No change 

has been made to the AD in this regard. 

Conclusion 

We reviewed the available data, 

including the comments received, and 

determined that air safety and the 

public interest require adopting the AD 

with the changes described previously 

and minor editorial changes. We have 

determined that these changes: 

• Are consistent with the intent that 

was proposed in the NPRM (77 FR 

61539, October 10, 2012) for correcting 

the unsafe condition; and 

• Do not add any additional burden 

upon the public than was already 

proposed in the NPRM (77 FR 61539, 

October 10, 2012). 

Costs of Compliance 

We estimate that this AD will affect 

753 products of U.S. registry. We also 

estimate that it will take about 640 

work-hours per product to comply with 

the basic requirements of this AD. The 

average labor rate is $85 per work-hour. 

Required parts will cost about $18,500 

per product. Where the service 

information lists required parts costs 

that are covered under warranty, we 

have assumed that there will be no 

charge for these parts. As we do not 

control warranty coverage for affected 

parties, some parties may incur costs 

higher than estimated here. Based on 

these figures, we estimate the cost of 

this AD to the U.S. operators to be 

$54,893,700, or $72,900 per product. 

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. 

We prepared a regulatory evaluation 

of the estimated costs to comply with 

this AD and placed it in the AD docket. 

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 the NPRM (77 FR 61539, 

October 10, 2012), the regulatory 

evaluation, any comments received, and 

other information. The street address for 

the Docket Operations office (telephone 

(800) 647–5527) is in the ADDRESSES

section. 

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: 

2013–09–03 Dassault Aviation: 

Amendment 39–17444. Docket No. 

FAA–2012–1067; Directorate Identifier 

2011–NM–231–AD. 

(a) Effective Date 

This airworthiness directive (AD) becomes 

effective August 14, 2013. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to the airplanes specified 

in paragraphs (c)(1), (c)(2), and (c)(3) of this 

AD, certificated in any category. 

(1) Dassault Aviation Model FALCON 2000 

and FALCON 2000EX airplanes, all serial 

numbers, except those on which 

modification M3072 has been installed. 

(2) DASSAULT AVIATION Model 

MYSTERE–FALCON 50 airplanes, all serial 

numbers. 

(3) DASSAULT AVIATION Model 

MYSTERE–FALCON 900 and FALCON 

900EX airplanes, all serial numbers, except 

those on which modification M5413 has been 

installed. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 57, Wings. 

(e) Reason 

This AD was prompted by reports that 

collapse of the main landing gear (MLG) 

could cause wing tank structure failure, 

which could result in fuel spillage and a 

consequent fire hazard. We are issuing this 

AD to prevent fuel spillage in the event of a 

MLG collapse, and consequent fire hazard. 

(f) Compliance 

You are responsible for having the actions 

required by this AD performed within the 

compliance times specified, unless the 

actions have already been done. 

(g) Modification 

Within 150 months after the effective date 

of this AD, do the modification of the righthand and left-hand wing fuel tanks, in 

accordance with the Accomplishment 

Instructions of the applicable service 

information specified in paragraph (g)(1), 

(g)(2), (g)(3), (g)(4), or (g)(5) of this AD, as 

applicable. The service information specified 

in paragraphs (g)(1) through (g)(5) of this AD 

contains a paragraph which states that each 

person applying the service bulletins must 

have successfully completed a training 

program. This training is recommended, but 

is not required by this AD. 

(1) For Model MYSTERE–FALCON 50 

airplanes: Dassault Mandatory Service 

Bulletin F50–496, Revision 2, dated March 

10, 2010, which includes the following 

appendices: 

(i) Appendix 1, Revision 2, dated February 

15, 2010; 

(ii) Appendix 2, Revision 3, dated February 

15, 2009; 

(iii) Appendix 3, Revision 2, dated October 

21, 2009; 

(iv) Appendix 4, Revision 1, dated October 

20, 2009; and 

(v) Appendix 5, Revision 3, dated February 

15, 2010. 

(2) For Model FALCON 900EX airplanes: 

Dassault Mandatory Service Bulletin 

F900EX–329, Revision 3, dated March 10, 

2010, which includes the following 

appendices: 

(i) Appendix 1, Revision 2, dated February 

15, 2010; 

(ii) Appendix 2, Revision 3, dated February 

15, 2009; 

(iii) Appendix 3, Revision 2, dated October 

21, 2009; 


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(iv) Appendix 4, Revision 1, dated October 

20, 2009; and 

(v) Appendix 5, Revision 3, dated February 

15, 2010. 

(3) For Model MYSTERE–FALCON 900 

airplanes: Dassault Mandatory Service 

Bulletin F900–388, Revision 3, dated October 

19, 2011, which includes the following 

appendices: 

(i) Appendix 1, Revision 2, dated February 

15, 2010; 

(ii) Appendix 2, Revision 3, dated February 

15, 2009; 

(iii) Appendix 3, Revision 2, dated October 

21, 2009; 

(iv) Appendix 4, Revision 1, dated October 

20, 2009; and 

(v) Appendix 5, Revision 4, dated October 

19, 2011. 

(4) For Model FALCON 2000 airplanes: 

Dassault Mandatory Service Bulletin F2000– 

358, Revision 3, dated March 10, 2010, which 

includes the following appendices: 

(i) Appendix 1, Revision 2, dated February 

15, 2010; 

(ii) Appendix 2, Revision 3, dated February 

15, 2009; 

(iii) Appendix 3, Revision 2, dated October 

21, 2009; 

(iv) Appendix 4, Revision 1, dated October 

20, 2009; and 

(v) Appendix 5, Revision 3, dated February 

15, 2010. 

(5) For Model FALCON 2000EX airplanes: 

Dassault Mandatory Service Bulletin 

F2000EX–171, Revision 3, dated March 10, 

2010, which includes the following 

appendices: 

(i) Appendix 1, Revision 2, dated February 

15, 2010; 

(ii) Appendix 2, Revision 3, dated February 

15, 2009; 

(iii) Appendix 3, Revision 2, dated October 

21, 2009; 

(iv) Appendix 4, Revision 1, dated October 

20, 2009; and 

(v) Appendix 5, Revision 3, dated February 

15, 2010. 

(h) Credit for Previous Actions 

This paragraph provides credit for the 

modifications required by paragraph (g) of 

this AD, if those actions were performed 

before the effective date of this AD using the 

service information (which is not 

incorporated by reference in this AD) 

specified in paragraphs (h)(1) through (h)(5) 

of this AD, as applicable. 

(1) For Model MYSTERE–FALCON 50 

airplanes: 

(i) Dassault Mandatory Service Bulletin 

F50–496, dated October 30, 2009, which 

includes the following appendices: 

(A) Appendix 1, Revision 1, dated October 

21, 2009; 

(B) Appendix 2, Revision 2, dated October 

21, 2009; 

(C) Appendix 3, Revision 2, dated October 

21, 2009; 

(D) Appendix 4, Revision 1, dated October 

20, 2009; and 

(E) Appendix 5, Revision 2, dated October 

22, 2009. 

(ii) Dassault Mandatory Service Bulletin 

F50–496, Revision 1, dated February 15, 

2010, which includes the following 

appendices: 

(A) Appendix 1, Revision 2, dated 

February 15, 2010; 

(B) Appendix 2, Revision 3, dated February 

15, 2009; 

(C) Appendix 3, Revision 2, dated October 

21, 2009; 

(D) Appendix 4, Revision 1, dated October 

20, 2009; and 

(E) Appendix 5, Revision 3, dated February 

15, 2010. 

(2) For Model FALCON 900EX airplanes: 

(i) Dassault Mandatory Service Bulletin 

F900EX–329, dated September 25, 2009, 

which includes the following appendices: 

(A) Appendix 1, dated July 6, 2009; 

(B) Appendix 2, dated July 6, 2009; 

(C) Appendix 3, Revision 1, dated 

September 25, 2009; 

(D) Appendix 4, dated July 6, 2009; and 

(E) Appendix 5, Revision 1, dated 

September 24, 2009. 

(ii) Dassault Mandatory Service Bulletin 

F900EX–329, Revision 1, dated October 30, 

2009, which includes the following 

appendices: 

(A) Appendix 1, Revision 1, dated October 

21, 2009; 

(B) Appendix 2, Revision 2, dated October 

21, 2009; 

(C) Appendix 3, Revision 2, dated October 

21, 2009; 

(D) Appendix 4, Revision 1, dated October 

20, 2009; and 

(E) Appendix 5, Revision 2, dated October 

22, 2009. 

(iii) Dassault Mandatory Service Bulletin 

F900EX–329, Revision 2, dated February 15, 

2010, which includes the following 

appendices: 

(A) Appendix 1, Revision 2, dated 

February 15, 201; 

(B) Appendix 2, Revision 3, dated February 

15, 2009; 

(C) Appendix 3, Revision 2, dated October 

21, 2009; 

(D) Appendix 4, Revision 1, dated October 

20, 2009; and 

(E) Appendix 5, Revision 3, dated February 

15, 2010. 

(3) For Model MYSTERE–FALCON 900 

airplanes: 

(i) Dassault Mandatory Service Bulletin 

F900–388, dated October 30, 2009, which 

includes the following appendices: 

(A) Appendix 1, Revision 1, dated October 

21, 2009; 

(B) Appendix 2, Revision 2, dated October 

21, 2009; 

(C) Appendix 3, Revision 2, dated October 

21, 2009; 

(D) Appendix 4, Revision 1, dated October 

20, 2009; and 

(E) Appendix 5, Revision 2, dated October 

22, 2009. 

(ii) Dassault Mandatory Service Bulletin 

F900–388, Revision 1, dated February 15, 

2010, which includes the following 

appendices: 

(A) Appendix 1, Revision 2, dated 

February 15, 2010; 

(B) Appendix 2, Revision 3, dated February 

15, 2009; 

(C) Appendix 3, Revision 2, dated October 

21, 2009; 

(D) Appendix 4, Revision 1, dated October 

20, 2009; and 

(E) Appendix 5, Revision 3, dated February 

15, 2010. 

(iii) Dassault Mandatory Service Bulletin 

F900–388, Revision 2, dated March 10, 2010, 

which includes the following appendices: 

(A) Appendix 1, Revision 2, dated 

February 15, 2010; 

(B) Appendix 2, Revision 3, dated February 

15, 2009; 

(C) Appendix 3, Revision 2, dated October 

21, 2009; 

(D) Appendix 4, Revision 1, dated October 

20, 2009; and 

(E) Appendix 5, Revision 3, dated February 

15, 2010. 

(4) For Model FALCON 2000 airplanes: 

(i) Dassault Mandatory Service Bulletin 

F2000–358, dated September 25, 2009, which 

includes the following appendices: 

(A) Appendix 1, dated July 6, 2009; 

(B) Appendix 2, dated July 6, 2009; 

(C) Appendix 3, Revision 1, dated 

September 25, 2009; 

(D) Appendix 4, dated July 6, 2009; and 

(E) Appendix 5, Revision 1, dated 

September 24, 2009. 

(ii) Dassault Mandatory Service Bulletin 

F2000–358, Revision 1, dated October 30, 

2009, which includes the following 

appendices: 

(A) Appendix 1, Revision 1, dated October 

21, 2009; 

(B) Appendix 2, Revision 2, dated October 

21, 2009; 

(C) Appendix 3, Revision 2, dated October 

21, 2009; 

(D) Appendix 4, Revision 1, dated October 

20, 2009; and 

(E) Appendix 5, Revision 2, dated October 

22, 2009. 

(iii) Dassault Mandatory Service Bulletin 

F2000–358, Revision 2, dated February 15, 

2010, which includes the following 

appendices: 

(A) Appendix 1, Revision 2, dated 

February 15, 2010; 

(B) Appendix 2, Revision 3, dated February 

15, 2009; 

(C) Appendix 3, Revision 2, dated October 

21, 2009; 

(D) Appendix 4, Revision 1, dated October 

20, 2009; and 

(E) Appendix 5, Revision 3, dated February 

15, 2010. 

(5) For Model FALCON 2000EX airplanes: 

(i) Dassault Mandatory Service Bulletin 

F2000EX–171, dated July 6, 2009, which 

includes the following appendices: 

(A) Appendix 1, dated July 6, 2009; 

(B) Appendix 2, dated July 6, 2009; 

(C) Appendix 3, dated July 6, 2009; 

(D) Appendix 4, dated July 6, 2009; and 

(E) Appendix 5, dated July 6, 2009. 

(ii) Dassault Mandatory Service Bulletin 

F2000EX–171, Revision 1, dated October 22, 

2009, which includes the following 

appendices: 

(A) Appendix 1, Revision 1, dated October 

21, 2009; 

(B) Appendix 2, Revision 2, dated October 

21, 2009; 

(C) Appendix 3, Revision 2, dated October 

21, 2009; 

(D) Appendix 4, Revision 1, dated October 

20, 2009; and 

(E) Appendix 5, Revision 2, dated October 

22, 2009. 


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(iii) Dassault Mandatory Service Bulletin 

F2000EX–171, Revision 2, dated February 15, 

2010, which includes the following 

appendices: 

(A) Appendix 1, Revision 2, dated 

February 15, 2010; 

(B) Appendix 2, Revision 3, dated February 

15, 2009; 

(C) Appendix 3, Revision 2, dated October 

21, 2009; 

(D) Appendix 4, Revision 1, dated October 

20, 2009; and 

(E) Appendix 5, Revision 3, dated February 

15, 2010. 

(i) Other FAA AD Provisions 

The following provisions also apply to this 

AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, International 

Branch, ANM–116, FAA, has the authority to 

approve AMOCs for this AD, if requested 

using the procedures found in 14 CFR 39.19. 

In accordance with 14 CFR 39.19, send your 

request to your principal inspector or local 

Flight Standards District Office, as 

appropriate. If sending information directly 

to the International Branch, send it to ATTN: 

Tom Rodriguez, Aerospace Engineer, 

International Branch, ANM–116, Transport 

Airplane Directorate, FAA, 1601 Lind 

Avenue SW., Renton, WA 98057–3356; 

telephone (425) 227–1137; fax (425) 227– 

1149. Information may be emailed to: 9- 

ANM-116-AMOC-REQUESTS@faa.gov. 

Before using any approved AMOC, notify 

your appropriate principal inspector, or 

lacking a principal inspector, the manager of 

the local flight standards district office/ 

certificate holding district office. The AMOC 

approval letter must specifically reference 

this AD. 

(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. 

(j) Related Information 

(1) Refer to Mandatory Continuing 

Airworthiness Information (MCAI) European 

Aviation Safety Agency Airworthiness 

Directive 2011–0193, dated October 5, 2011, 

for related information. This MCAI may be 

viewed on the Internet at http:// 

ad.easa.europa.eu/blob/ 

easa_ad_2011_0193.pdf. 

(2) Service information identified in this 

AD that is not incorporated by referenced 

may be obtained at the addresses specified in 

paragraphs (k)(3) and (k)(4) of this AD. 

(k) 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) Dassault Mandatory Service Bulletin 

F50–496, Revision 2, dated March 10, 2010, 

which includes the following appendices: 

(A) Appendix 1, Revision 2, dated 

February 15, 2010; 

(B) Appendix 2, Revision 3, dated February 

15, 2009; 

(C) Appendix 3, Revision 2, dated October 

21, 2009; 

(D) Appendix 4, Revision 1, dated October 

20, 2009; and 

(E) Appendix 5, Revision 3, dated February 

15, 2010. 

(ii) Dassault Mandatory Service Bulletin 

F900EX–329, Revision 3, dated March 10, 

2010, which includes the following 

appendices: 

(A) Appendix 1, Revision 2, dated 

February 15, 2010; 

(B) Appendix 2, Revision 3, dated February 

15, 2009; 

(C) Appendix 3, Revision 2, dated October 

21, 2009; 

(D) Appendix 4, Revision 1, dated October 

20, 2009; and 

(E) Appendix 5, Revision 3, dated February 

15, 2010. 

(iii) Dassault Mandatory Service Bulletin 

F900–388, Revision 3, dated October 19, 

2011, which includes the following 

appendices: 

(A) Appendix 1, Revision 2, dated 

February 15, 2010; 

(B) Appendix 2, Revision 3, dated February 

15, 2009; 

(C) Appendix 3, Revision 2, dated October 

21, 2009; 

(D) Appendix 4, Revision 1, dated October 

20, 2009; and 

(E) Appendix 5, Revision 4, dated October 

19, 2011. 

(iv) Dassault Mandatory Service Bulletin 

F2000–358, Revision 3, dated March 10, 

2010, which includes the following 

appendices: 

(A) Appendix 1, Revision 2, dated 

February 15, 2010; 

(B) Appendix 2, Revision 3, dated February 

15, 2009; 

(C) Appendix 3, Revision 2, dated October 

21, 2009; 

(D) Appendix 4, Revision 1, dated October 

20, 2009; and 

(E) Appendix 5, Revision 3, dated February 

15, 2010. 

(v) Dassault Mandatory Service Bulletin 

F2000EX–171, Revision 3, dated March 10, 

2010, which includes the following 

appendices: 

(A) Appendix 1, Revision 2, dated 

February 15, 2010; 

(B) Appendix 2, Revision 3, dated February 

15, 2009; 

(C) Appendix 3, Revision 2, dated October 

21, 2009; 

(D) Appendix 4, Revision 1, dated October 

20, 2009; and 

(E) Appendix 5, Revision 3, dated February 

15, 2010. 

(3) For service information identified in 

this AD, contact Dassault Falcon Jet, P.O. Box 

2000, South Hackensack, New Jersey 07606; 

telephone 201–440–6700; Internet http:// 

www.dassaultfalcon.com. 

(4) You may review copies of the 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 April 23, 

2013. 

Jeffrey E. Duven, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2013–15141 Filed 7–9–13; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2013–0535; Directorate 

Identifier 2013–CE–018–AD; Amendment 

39–17489; AD 2013–13–01] 

RIN 2120–AA64 

Airworthiness Directives; Piper 

Aircraft, Inc. Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; request for 

comments. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 

Piper Aircraft, Inc. Models PA–46–310P, 

PA–46–350P, PA–46R–350T, and PA– 

46–500TP airplanes. This AD requires 

inspecting the fuel vent valves to 

identify if the nitrile parts are installed 

and modifying and eventually replacing 

the fuel vent valves if the nitrile parts 

are installed. This AD was prompted by 

nitrile fuel vent valves not providing the 

correct ventilation. If not corrected, this 

unsafe condition may lead to structural 

damage of the wings, which could result 

in loss of control. We are issuing this 

AD to correct the unsafe condition on 

these products. 

DATES: This AD is effective July 10, 

2013. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in the AD 

as of July 10, 2013. 

We must receive comments on this 

AD by August 26, 2013. 

ADDRESSES: You may send comments, 

using the procedures found in 14 CFR 

11.43 and 11.45, by any of the following 

methods: 

• Federal eRulemaking Portal: Go to 

http://www.regulations.gov. Follow the 

instructions for submitting comments. 


TKELLEY on DSK3SPTVN1PROD with RULES