This section of the FEDERAL REGISTER

contains regulatory documents having general

applicability and legal effect, most of which

are keyed to and codified in the Code of

Federal Regulations, which is published under

50 titles pursuant to 44 U.S.C. 1510.

The Code of Federal Regulations is sold by

the Superintendent of Documents. Prices of

new books are listed in the first FEDERAL

REGISTER issue of each week.

Rules and Regulations Federal Register

60795 

Vol. 80, No. 195 

Thursday, October 8, 2015 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2015–0934; Directorate 

Identifier 2014–NM–030–AD; Amendment 

39–18287; AD 2015–20–08] 

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 all 

Model FAN JET FALCON, FAN JET 

FALCON SERIES C, D, E, F, and G 

airplanes; Model MYSTERE–FALCON 

200 airplanes; and Model MYSTERE– 

FALCON 20–C5, 20–D5, 20–E5, and 20– 

F5 airplanes. This AD was prompted by 

reports of defective fire extinguisher 

tubes. It was determined the defects 

were caused by corrosion. This AD 

requires repetitive general visual 

inspections of the fire extinguisher 

tubes for cracking and corrosion, and 

replacement of any cracked tube with a 

serviceable tube, if necessary. We are 

issuing this AD to detect and correct 

cracking and corrosion in the fire 

extinguisher tubes, which could impact 

the capability to extinguish an engine 

fire, and possibly result in damage to 

the airplane and injury to the 

passengers. 

DATES: This AD becomes effective 

November 12, 2015. 

ADDRESSES: You may examine the AD 

docket on the Internet at http://

www.regulations.gov/

#!docketDetail;D=FAA-2015-0934; or in 

person at the 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. 

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 by adding an AD that would 

apply to all Dassault Aviation Model 

FAN JET FALCON, FAN JET FALCON 

SERIES C, D, E, F, and G airplanes; 

Model MYSTERE–FALCON 200 

airplanes; and Model MYSTERE– 

FALCON 20–C5, 20–D5, 20–E5, and 20– 

F5 airplanes. The NPRM published in 

the Federal Register on May 4, 2015 (80 

FR 25254). 

The European Aviation Safety Agency 

(EASA), which is the Technical Agent 

for the Member States of the European 

Union, has issued Airworthiness 

Directive 2013–0299, dated December 

19, 2013 (referred to after this as the 

Mandatory Continuing Airworthiness 

Information, or ‘‘the MCAI’’), to correct 

an unsafe condition for all Dassault 

Aviation Model FAN JET FALCON, 

FAN JET FALCON SERIES C, D, E, F, 

and G airplanes; Model MYSTERE– 

FALCON 200 airplanes; and Model 

MYSTERE–FALCON 20–C5, 20–D5, 20– 

E5, and 20–F5 airplanes. The MCAI 

states: 

Several defective extinguisher tubes have 

been reported on certain Dassault Aviation 

Fan Jet Falcon aeroplanes. The results of the 

investigations concluded that these 

occurrences were caused by corrosion. 

This condition, if not detected and 

corrected, could impact the capability to 

extinguish an engine fire, possibly resulting 

in damage to the aeroplane and injury to the 

occupants. 

For the reason described above, this 

[EASA] AD requires repetitive [general 

visual] inspections [for cracking and 

corrosion] of the fire extinguisher tubes and, 

depending on findings, the replacement of an 

affected part with a serviceable part 

(improved fire extinguisher tube). It also 

proposes the replacement of those tubes with 

the ‘‘old Part Number’’ (P/N) with a 

serviceable part with the new P/N as a 

terminating action. In addition, this [EASA] 

AD prohibits installation of an affected tube 

on an aeroplane. 

You may examine the MCAI in the 

AD docket on the Internet at http://

www.regulations.gov/

#!documentDetail;D=FAA-2015-0934- 

0002. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

received no comments on the NPRM (80 

FR 25254, May 4, 2015) 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, except for minor editorial 

changes. We have determined that these 

minor changes: 

• Are consistent with the intent that 

was proposed in the NPRM (80 FR 

25254, May 4, 2015) for correcting the 

unsafe condition; and 

• Do not add any additional burden 

upon the public than was already 

proposed in the NPRM (80 FR 25254, 

May 4, 2015). 

Costs of Compliance 

We estimate that this AD affects 170 

airplanes of U.S. registry. 

We also estimate that it will take 

about 4 work-hours 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 this AD on U.S. 

operators to be $57,800, or $340 per 

product. 

We have received no definitive data 

that will enable us to provide cost 

estimates for the on-condition actions 

specified in this AD. 

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 


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60796 Federal Register / Vol. 80, No. 195 / Thursday, October 8, 2015 / Rules and Regulations 

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. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http://

www.regulations.gov/

#!docketDetail;D=FAA-2015-0934; 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 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 airworthiness 

directive (AD): 

2015–20–08 Dassault Aviation: 

Amendment 39–18287. Docket No. 

FAA–2015–0934; Directorate Identifier 

2014–NM–030–AD. 

(a) Effective Date 

This AD becomes effective November 12, 

2015. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to Dassault Aviation 

Model FAN JET FALCON, FAN JET FALCON 

SERIES C, D, E, F, and G airplanes; Model 

MYSTERE–FALCON 200 airplanes; and 

Model MYSTERE–FALCON 20–C5, 20–D5, 

20–E5, and 20–F5 airplanes, certificated in 

any category, all manufacturer serial 

numbers. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 26, Fire protection. 

(e) Reason 

This AD was prompted by reports of 

defective fire extinguisher tubes. It was 

determined the defects were caused by 

corrosion. We are issuing this AD to detect 

and correct cracking and corrosion in the fire 

extinguisher tubes, which could impact the 

capability to extinguish an engine fire, and 

possibly result in damage to the airplane and 

injury to the passengers. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Inspection 

For airplanes identified in paragraphs 

(g)(1), (g)(2), and (g)(3) of this AD: Within 13 

months or 450 flight hours, whichever occurs 

first after the effective date of this AD, do a 

general visual inspection of the fire 

extinguisher tubes for cracking and 

corrosion, in accordance with a method 

approved by the Manager, International 

Branch, ANM–116, Transport Airplane 

Directorate, FAA; or the European Aviation 

Safety Agency (EASA); or Dassault Aviation’s 

EASA Design Organization Approval (DOA). 

Repeat the inspection thereafter at intervals 

not to exceed 13 months. 

(1) Model FAN JET FALCON airplanes and 

Model FAN JET FALCON SERIES C, D, E, F, 

and G airplanes, equipped with any fire 

extinguisher tubes having part numbers 

MY20791–101, MY20791–101–1, MY20791– 

102, MY20791–102–1, MY20791–117, and 

MY20791–112. 

(2) Model MYSTERE–FALCON 200 

airplanes equipped with any fire extinguisher 

tubes having part numbers 

M20H791000210B1 and M20H791000240B1. 

(3) Model MYSTERE–FALCON 20–C5, 20– 

D5, 20–E5, and 20–F5 airplanes equipped 

with any fire extinguisher tubes having part 

numbers M20R791101, M20R791101A1, and 

M20R791102. 

(h) Corrective Action 

If, during any inspection required by 

paragraph (g) of this AD, any cracking or 

corrosion is found, before further flight, 

replace the tube with a serviceable tube 

having a part number specified in Table 1 to 

paragraph (h) of this AD, as applicable. 

TABLE 1 TO PARAGRAPH (H) OF THIS AD—SERVICEABLE FIRE EXTINGUISHER TUBES

For model— Equipped with affected pin— Replace with serviceable pin— 

FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G airplanes .. MY20791–101 ....................................... MY20791–101–2. 

FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G airplanes .. MY20791–101–1 ................................... MY20791–101–2. 

FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G airplanes .. MY20791–102 ....................................... MY20791–102–2. 

FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G airplanes .. MY20791–102–1 ................................... MY20791–102–2. 

FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G airplanes .. MY20791–117 ....................................... MY20791–117n–1. 

FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G airplanes .. MY20791–112 ....................................... MY20791–112–1. 

MYSTERE–FALCON 200 airplanes ..................................................................... M20H791000210B1 .............................. M20H791000210B2. 

MYSTERE–FALCON 200 airplanes ..................................................................... M20H791000240B1 .............................. M20H791000240B2. 

MYSTERE–FALCON 20–C5, 20–D5, 20–E5, and 20–F5 airplanes ................... M20R791101 ........................................ M20R791101A2. 

MYSTERE–FALCON 20–C5, 20–D5, 20–E5, and 20–F5 airplanes ................... M20R791101A1 .................................... M20R791101A3. 

MYSTERE–FALCON 20–C5, 20–D5, 20–E5, and 20–F5 airplanes ................... M20R791102 ........................................ M20R791102A2. 


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Federal Register / Vol. 80, No. 195 / Thursday, October 8, 2015 / Rules and Regulations 60797 

(i) Terminating Action for the Repetitive 

Inspections 

Replacement of an affected tube with a 

serviceable tube, as required by paragraph (h) 

of this AD, constitutes a terminating action 

for the repetitive inspections required by 

paragraph (g) of this AD. 

(j) Parts Installation Prohibition 

As of the effective date of this AD, no 

person may install a tube having a part 

number identified in paragraphs (g)(1), (g)(2), 

and (g)(3) of this AD, on any airplane. 

(k) Other FAA AD Provisions 

The following provisions also apply to this 

AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, International 

Branch, ANM–116, Transport Airplane 

Directorate, 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) 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 Branch, ANM– 

116, Transport Airplane Directorate, 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. 

(l) Related Information 

Refer to Mandatory Continuing 

Airworthiness Information (MCAI) EASA 

Airworthiness Directive 2013–0299, dated 

December 19, 2013, for related information. 

This MCAI may be found in the AD docket 

on the Internet at http://

www.regulations.gov/

#!documentDetail;D=FAA-2015-0934-0002. 

(m) Material Incorporated by Reference 

None. 

Issued in Renton, Washington, on 

September 29, 2015. 

Jeffrey E. Duven, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2015–25492 Filed 10–7–15; 8:45 am] 

BILLING CODE 4910–13–P 

FEDERAL TRADE COMMISSION 

16 CFR Part 4 

Miscellaneous Rules 

AGENCY: Federal Trade Commission. 

ACTION: Final rules; technical correction. 

SUMMARY: The Federal Trade 

Commission published final rules on 

May 6, 2015, revising certain of its rules 

of practice. This document makes a 

technical correction to those final rules. 

DATES: Effective October 8, 2015. 

FOR FURTHER INFORMATION CONTACT: 

Josephine Liu, Attorney, (202) 326– 

2170, Office of the General Counsel, 

Federal Trade Commission, 600 

Pennsylvania Avenue NW., Washington, 

DC 20580. 

SUPPLEMENTARY INFORMATION: This 

document makes a technical correction 

to two cross-references in Rule 4.4(a)(3). 

List of Subjects in 16 CFR Part 4 

Administrative practice and 

procedure, Freedom of information, 

Public record. 

Accordingly, 16 CFR part 4 is 

corrected by making the following 

correcting amendment: 

PART 4—MISCELLANEOUS RULES 

■ 1. The authority citation for part 4 

continues to read as follows: 

Authority: 15 U.S.C. 46, unless otherwise 

noted. 

§ 4.4 [Amended] 

■ 2. In § 4.4, amend the first sentence of 

paragraph (a)(3) by removing ‘‘section 

20(c)(7) of the FTC Act’’ and adding in 

its place ‘‘section 20(c)(8) of the FTC 

Act’’ and by removing ‘‘section 20(c)(8) 

of the FTC Act’’ and adding in its place 

‘‘section 20(c)(9) of the FTC Act’’. 

By direction of the Commission. 

Donald S. Clark, 

Secretary. 

[FR Doc. 2015–25605 Filed 10–7–15; 8:45 am] 

BILLING CODE 6750–01–P 

DEPARTMENT OF LABOR 

Office of the Secretary 

29 CFR Part 20 

RIN 1290–AA27 

Administrative Wage Garnishment 

Procedures 

AGENCY: Office of the Secretary, Labor. 

ACTION: Interim final rule with request 

for comments. 

SUMMARY: This rule will allow the U.S. 

Department of Labor (Department) to 

garnish the disposable wages of nonfederal workers who are indebted to the 

Department without first obtaining a 

court order. It implements the 

administrative wage garnishment 

provisions contained in the Debt 

Collection Improvement Act of 1996 

(DCIA) in accordance with the 

regulations issued by the Secretary of 

the Treasury. 

DATES: This rule is effective October 8, 

2015. Comments must be received 

within 30 days of publication, which is 

on or before November 9, 2015. 

ADDRESSES: You may submit written 

comments to the docket using any one 

of the following methods: 

(1) Federal eRulemaking Portal: 

http://www.regulations.gov. 

(2) Mail: Address comments 

concerning this interim rule to Shelia 

Alexander, Office of Chief Financial 

Officer, U.S. Department of Labor, 

Frances Perkins Building, Room S4030, 

200 Constitution Avenue NW., 

Washington, DC 20210. 

(3) Email: Comments may also be 

submitted by electronic mail to 

alexander.shelia@dol.gov. 

Additionally, any comments that 

concern information collection may be 

sent to the Office of Information and 

Regulatory Affairs, Attention OMB Desk 

Officer for DOL, Office of Management 

and Budget, Room 10235, New 

Executive Office Building, Washington, 

DC 20503. 

FOR FURTHER INFORMATION CONTACT: 

Shelia Alexander, Office of the Chief 

Financial Officer, (202) 693–4472; or 

Rachel Rikleen, Office of the Solicitor, 

(202) 693–5702. 

SUPPLEMENTARY INFORMATION: 

I. Background 

Section 31001(o) of the Debt 

Collection Improvement Act of 1996 

(DCIA), which is codified at 31 U.S.C. 

3720D, authorizes federal agencies to 

use administrative procedure to garnish 

the disposable pay of an individual to 

collect delinquent non-tax debt owed to 

the United States in accordance with 

regulations promulgated by the 

Secretary of the Treasury. Wage 

garnishment is a process whereby an 

employer withholds amounts from an 

employee’s wages and pays those 

amounts to the employee’s creditor 

pursuant to a withholding order. Under 

the DCIA, agencies may garnish up to 

15% of a delinquent non-tax debtor’s 

disposable wages. Prior to the 

enactment of the DCIA, agencies were 

generally required to obtain a court 


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