43674 Federal Register / Vol. 82, No. 180 / Tuesday, September 19, 2017 / Rules and Regulations 

(3) The replacement of one or more circuit 

breakers as required by paragraph (g)(2) of 

this AD does not terminate the repetitive 

functional tests required by paragraph (g)(1) 

of this AD. 

(h) New Requirement of This AD: 

Installation of Fuel Pumps Having a New 

Standard 

Within 72 months after the effective date 

of this AD: Install a fuel pump having a new 

standard at each applicable location on the 

airplane, in accordance with the 

Accomplishment Instructions of the 

applicable service information specified in 

paragraph (h)(1), (h)(2), or (h)(3) of this AD. 

Accomplishment of the installation of fuel 

pumps having the new standard terminates 

the requirement for the repetitive functional 

tests required by paragraph (g)(1) of this AD. 

(1) Airbus Service Bulletin A300–28–0093, 

dated December 15, 2015. 

(2) Airbus Service Bulletin A300–28–6111, 

Revision 01, dated February 29, 2016. 

(3) Airbus Service Bulletin A310–28–2176, 

dated December 15, 2015. 

(i) Parts Installation Prohibition 

After the installation of any fuel pump 

having a new standard on an airplane, as 

required by paragraph (h) of this AD, no 

person may install any fuel pump having part 

number 2052Cxx (where ‘‘xx’’ represents any 

numerical combination) on that airplane. 

(j) Credit for Previous Actions 

This paragraph provides credit for the 

installation required by paragraph (h) of this 

AD, if the installation was done before the 

effective date of this AD using Airbus Service 

Bulletin A300–28–6111, dated December 15, 

2015. 

(k) Other FAA AD Provisions 

The following provisions also apply to this 

AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, International 

Section, Transport Standards Branch, 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 Section, send it 

to the attention of the person identified in 

paragraph (l)(2) of this AD. Information may 

be emailed to: 9-ANM-116-AMOCREQUESTS@faa.gov. 

(2) Contacting the Manufacturer: As of the 

effective date of this AD, for any requirement 

in this AD to obtain corrective actions from 

a manufacturer, the action must be 

accomplished using a method approved by 

the Manager, International Section, Transport 

Standards Branch, FAA; or the European 

Aviation Safety Agency (EASA); or Airbus’s 

EASA Design Organization Approval (DOA). 

If approved by the DOA, the approval must 

include the DOA-authorized signature. 

(3) Required for Compliance (RC): If any 

Airbus service information contains 

procedures or tests that are identified as RC, 

those procedures and tests must be done to 

comply with this AD; any procedures or tests 

that are not identified as RC are 

recommended. Those procedures and tests 

that are not identified as RC may be deviated 

from using accepted methods in accordance 

with the operator’s maintenance or 

inspection program without obtaining 

approval of an AMOC, provided the 

procedures and tests identified as RC can be 

done and the airplane can be put back in an 

airworthy condition. Any substitutions or 

changes to procedures or tests identified as 

RC require approval of an AMOC. 

(l) Related Information 

(1) Refer to Mandatory Continuing 

Airworthiness Information (MCAI) EASA AD 

2016–0080, dated April 21, 2016, for related 

information. This MCAI may be found in the 

AD docket on the Internet at http://

www.regulations.gov by searching for and 

locating Docket No. FAA–2017–0339. 

(2) For more information about this AD, 

contact Dan Rodina, Aerospace Engineer, 

International Section, Transport Standards 

Branch, FAA, 1601 Lind Avenue SW., 

Renton, WA 98057–3356; telephone 425– 

227–2125; fax 425–227–1149. 

(3) Service information identified in this 

AD that is not incorporated by reference is 

available at the addresses specified in 

paragraphs (m)(5) and (m)(6) of this AD. 

(m) 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 this AD specifies otherwise. 

(3) The following service information was 

approved for IBR on October 24, 2017. 

(i) Airbus Service Bulletin A300–28–0093, 

dated December 15, 2015. 

(ii) Airbus Service Bulletin A300–28–6111, 

Revision 01, dated February 29, 2016. 

(iii) Airbus Service Bulletin A310–28– 

2176, dated December 15, 2015. 

(4) The following service information was 

approved for IBR on August 19, 2014 (79 FR 

41098, July 15, 2014). 

(i) Airbus Alert Operators Transmission 

A28W002–13, dated July 23, 2013. 

(ii) Reserved. 

(5) For service information identified in 

this AD, contact Airbus SAS, Airworthiness 

Office—EAW, 1 Rond Point Maurice 

Bellonte, 31707 Blagnac Cedex, France; 

telephone +33 5 61 93 36 96; fax +33 5 61 

93 44 51; email account.airworth-eas@

airbus.com; Internet http://www.airbus.com. 

(6) You may view this service information 

at the FAA, Transport Standards Branch, 

1601 Lind Avenue SW., Renton, WA. For 

information on the availability of this 

material at the FAA, call 425–227–1221. 

(7) 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 

September 7, 2017. 

Jeffrey E. Duven, 

Director, System Oversight Division, Aircraft 

Certification Service. 

[FR Doc. 2017–19653 Filed 9–18–17; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2017–0529; Product 

Identifier 2016–NM–123–AD; Amendment 

39–19044; AD 2017–19–14] 

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 

900EX airplanes. This AD was 

prompted by a determination that new 

or more restrictive maintenance 

requirements and/or airworthiness 

limitations are necessary. This AD 

requires revising the maintenance or 

inspection program, as applicable, to 

incorporate new or more restrictive 

maintenance requirements and/or 

airworthiness limitations. We are 

issuing this AD to address the unsafe 

condition on these products. 

DATES: This AD is effective October 24, 

2017. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of October 24, 2017. 

ADDRESSES: For service information 

identified in this final rule, contact 

Dassault Falcon Jet Corporation, 

Teterboro Airport, P.O. Box 2000, South 

Hackensack, NJ 07606; telephone 201– 

440–6700; Internet http://

www.dassaultfalcon.com. You may 

view this referenced service information 

at the FAA, Transport Standards 

Branch, 1601 Lind Avenue SW., Renton, 

WA. For information on the availability 

of this material at the FAA, call 425– 

227–1221. It is also available on the 

Internet at http://www.regulations.gov 

by searching for and locating Docket No. 

FAA–2017–0529. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http:// 


asabaliauskas on DSKBBXCHB2PROD with RULES
Federal Register / Vol. 82, No. 180 / Tuesday, September 19, 2017 / Rules and Regulations 43675 

www.regulations.gov by searching for 

and locating Docket No. FAA–2017– 

0529; 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 Docket 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: Tom 

Rodriguez, Aerospace Engineer, 

International Section, Transport 

Standards Branch, 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 by adding an AD that would 

apply to certain Dassault Aviation 

Model FALCON 900EX airplanes. The 

NPRM published in the Federal 

Register on June 6, 2017 (82 FR 25975) 

(‘‘the NPRM’’). 

The European Aviation Safety Agency 

(EASA), which is the Technical Agent 

for the Member States of the European 

Union, has issued EASA AD 2016–0129, 

dated June 23, 2016 (referred to after 

this as the Mandatory Continuing 

Airworthiness Information, or ‘‘the 

MCAI’’), to correct an unsafe condition 

for certain Dassault Aviation Model 

FALCON 900EX airplanes. The MCAI 

states: 

The airworthiness limitations and 

maintenance requirements for the DA 

[Dassault Aviation] Falcon 900EX type 

design relating to Falcon 900EX Easy, Falcon 

900LX and Falcon 900DX variants are 

included in Aircraft Maintenance Manual 

(AMM) chapter 5–40 and are approved by the 

European Aviation Safety Agency (EASA). 

These instructions have been identified as 

mandatory for continued airworthiness. 

Failure to accomplish these instructions 

could result in an unsafe condition. 

Consequently, EASA issued AD 2013–0052 

[which corresponds to AD 2014–16–27, 

Amendment 39–17951 (79 FR 51071, August 

27, 2014) (‘‘2014–16–27’’)] to require 

accomplishment of the maintenance tasks, 

and implementation of the airworthiness 

limitations, as specified in DA Falcon 900EX 

Easy/900LX/900DX AMM chapter 5–40 (DGT 

113875) at revision 7. 

Since that [EASA] AD was issued, DA 

issued revision 9 of DA Falcon 900EX Easy/ 

900LX/900DX AMM chapter 5–40 (DGT 

113875) (hereafter referred to as ‘‘the ALS’’ 

in this AD), which contains new or more 

restrictive maintenance requirements and/or 

airworthiness limitations. The ALS 

introduces, among others, the following new 

tasks: 

—Task 53–50–00–220–803 ‘‘Detailed 

inspection of the baggage compartment’’; 

—Task 53–50–00–220–807 ‘‘Detailed 

inspection of the upper part of frame 30.’’ 

For the reason described above, this 

[EASA] AD retains the requirements of EASA 

AD 2013–0052, which is superseded, and 

requires accomplishment of the actions 

specified in the ALS. 

You may examine the MCAI in the 

AD docket on the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2017– 

0529. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

received no comments on the NPRM or 

on the determination of the cost to the 

public. 

Conclusion 

We reviewed the relevant data and 

determined that air safety and the 

public interest require adopting this AD 

as proposed. We have determined that 

these minor changes: 

• Are consistent with the intent that 

was proposed in the NPRM for 

correcting the unsafe condition; and 

• Do not add any additional burden 

upon the public than was already 

proposed in the NPRM. 

Related Service Information Under 1 

CFR Part 51 

Dassault Aviation has issued Chapter 

5–40, Airworthiness Limitations, 

Revision 9, dated November 2015, of the 

Dassault Falcon 900EX EASy, Falcon 

900LX, and Falcon 900DX Maintenance 

Manual. The service information 

describes procedures, maintenance 

tasks, and airworthiness limitations 

specified in the Airworthiness 

Limitations section (ALS) of the AMM. 

This service information is reasonably 

available because the interested parties 

have access to it through their normal 

course of business or by the means 

identified in the ADDRESSES section. 

Costs of Compliance 

We estimate that this AD affects 63 

airplanes of U.S. registry. 

We estimate the following costs to 

comply with this AD: 

ESTIMATED COSTS

Action Labor cost Parts cost Cost per 

product 

Cost on U.S. 

operators 

Maintenance or inspection program revision .. 1 work-hour × $85 per hour = $85 ................. $0 $85 $5,355 

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. 

This AD is issued in accordance with 

authority delegated by the Executive 

Director, Aircraft Certification Service, 

as authorized by FAA Order 8000.51C. 

In accordance with that order, issuance 

of ADs is normally a function of the 

Compliance and Airworthiness 

Division, but during this transition 

period, the Executive Director has 

delegated the authority to issue ADs 

applicable to transport category 

airplanes to the Director of the System 

Oversight Division. 

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. 


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43676 Federal Register / Vol. 82, No. 180 / Tuesday, September 19, 2017 / Rules and Regulations 

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 airworthiness 

directive (AD): 

2017–19–14 Dassault Aviation: 

Amendment 39–19044; Docket No. 

FAA–2017–0529; Product Identifier 

2016–NM–123–AD. 

(a) Effective Date 

This AD is effective October 24, 2017. 

(b) Affected ADs 

This AD affects AD 2014–16–27, 

Amendment 39–17951 (79 FR 51071, August 

27, 2014) (‘‘AD 2014–16–27’’). 

(c) Applicability 

This AD applies to Dassault Aviation 

Model FALCON 900EX airplanes, serial 

number (S/N) 97 and S/N 120 and higher, 

certificated in any category, with an original 

certificate of airworthiness or original export 

certificate of airworthiness issued on or 

before November 1, 2015. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 05, Time Limits/Maintenance 

Checks. 

(e) Reason 

This AD was prompted by a determination 

that new or more restrictive maintenance 

requirements and/or airworthiness 

limitations are necessary. We are issuing this 

AD to prevent reduced structural integrity of 

the airplane. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Revision of Maintenance or Inspection 

Program 

Within 90 days after the effective date of 

this AD, revise the maintenance or inspection 

program, as applicable, to incorporate the 

information specified in Chapter 5–40, 

Airworthiness Limitations, Revision 9, dated 

November 2015, of the Dassault Falcon 

900EX EASy, Falcon 900LX, and Falcon 

900DX Maintenance Manual. The initial 

compliance time for accomplishing the 

actions specified in Chapter 5–40, 

Airworthiness Limitations, Revision 9, dated 

November 2015, of the Dassault Falcon 

900EX EASy, Falcon 900LX, and Falcon 

900DX Maintenance Manual, is within the 

applicable times specified in the 

maintenance manual or 90 days after the 

effective date of this AD, whichever occurs 

later, except as provided by paragraphs (g)(1) 

through (g)(4) of this AD. 

(1) The term ‘‘LDG’’ in the ‘‘First 

Inspection’’ column of any table in the 

service information means total airplane 

landings. 

(2) The term ‘‘FH’’ in the ‘‘First Inspection’’ 

column of any table in the service 

information means total flight hours. 

(3) The term ‘‘FC’’ in the ‘‘First Inspection’’ 

column of any table in the service 

information means total flight cycles. 

(4) The term ‘‘M’’ in the ‘‘First Inspection’’ 

column of any table in the service 

information means months. 

(h) No Alternative Actions and Intervals 

After accomplishing the revision required 

by paragraph (g) of this AD, no alternative 

actions (e.g., inspections) or intervals may be 

used unless the actions or intervals are 

approved as an alternative method of 

compliance (AMOC) in accordance with the 

procedures specified in paragraph (j)(1) of 

this AD. 

(i) Terminating Action 

Accomplishing the actions required by 

paragraph (g) of this AD terminates all 

requirements of AD 2014–16–27. 

(j) Other FAA AD Provisions 

The following provisions also apply to this 

AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, International 

Section, Transport Standards Branch, 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 Section, send it 

to the attention of the person identified in 

paragraph (k)(2) of this AD. Information may 

be emailed to: 9-ANM-116-AMOCREQUESTS@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. 

(2) Contacting the Manufacturer: For any 

requirement in this AD to obtain corrective 

actions from a manufacturer, the action must 

be accomplished using a method approved 

by the Manager, International Section, 

Transport Standards Branch, FAA; or the 

European Aviation Safety Agency (EASA); or 

Dassault Aviation’s EASA Design 

Organization Approval (DOA). If approved by 

the DOA, the approval must include the 

DOA-authorized signature. 

(k) Related Information 

(1) Refer to Mandatory Continuing 

Airworthiness Information (MCAI) EASA 

Airworthiness Directive 2016–0129, dated 

June 23, 2016, for related information. This 

MCAI may be found in the AD docket on the 

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

searching for and locating Docket No. FAA– 

2017–0529. 

(2) For more information about this AD, 

contact Tom Rodriguez, Aerospace Engineer, 

International Section, Transport Standards 

Branch, FAA, 1601 Lind Avenue SW., 

Renton, WA 98057–3356; telephone 425– 

227–1137; fax 425–227–1149. 

(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 this AD specifies otherwise. 

(i) Chapter 5–40, Airworthiness 

Limitations, Revision 9, dated November 

2015, of the Dassault Falcon 900EX EASy, 

Falcon 900LX, and Falcon 900DX 

Maintenance Manual. 

(ii) Reserved. 

(3) For service information identified in 

this AD, contact Dassault Falcon Jet 

Corporation, Teterboro Airport, P.O. Box 

2000, South Hackensack, NJ 07606; 

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

www.dassaultfalcon.com. 

(4) You may view this service information 

at the FAA, Transport Standards Branch, 

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 

September 7, 2017. 

Jeffrey E. Duven, 

Director, System Oversight Division, Aircraft 

Certification Service. 

[FR Doc. 2017–19652 Filed 9–18–17; 8:45 am] 

BILLING CODE 4910–13–P 


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