Federal Register / Vol. 80, No. 78 / Thursday, April 23, 2015 / Rules and Regulations 22635 

(d) Shipping requirements. Sealed 

containers of apples destined for export 

to the continental United States must be 

held in a cold storage facility while 

awaiting export. 

(e) Phytosanitary certificate. Each 

consignment of apples imported from 

China into the continental United States 

must be accompanied by a 

phytosanitary certificate issued by the 

NPPO of China with an additional 

declaration stating that the requirements 

of this section have been met and the 

consignment has been inspected by the 

NPPO and found free of quarantine 

pests. 

(f) Additional conditions for apples 

from areas of China south of the 33rd 

parallel. In addition to the conditions in 

paragraphs (a) through (e) of this 

section, apples from areas of China 

south of the 33rd parallel apples must 

be treated in accordance with 7 CFR 

part 305. (Approved by the Office of 

Management and Budget under control 

number 0579–0423) 

Done in Washington, DC, this 20th day of 

April 2015. 

Kevin Shea, 

Administrator, Animal and Plant Health 

Inspection Service. 

[FR Doc. 2015–09508 Filed 4–22–15; 8:45 am] 

BILLING CODE 3410–34–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2015–0830; Directorate 

Identifier 2015–NM–024–AD; Amendment 

39–18141; AD 2015–08–05] 

RIN 2120–AA64 

Airworthiness Directives; Dassault 

Aviation Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule; request for 

comments. 

SUMMARY: We are superseding 

Airworthiness Directive (AD) 2013–26– 

05 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. AD 2013–26–05 required 

repetitive weighing of fire extinguisher 

bottles having a certain part number, 

and eventual replacement of those 

bottles to terminate the repetitive 

weighing. This new AD continues to 

require repetitive weighing of fire 

extinguisher bottles having a certain 

part number, and eventual replacement 

of those bottles to terminate the 

repetitive weighing. This AD was 

prompted by our determination that 

certain text in the method of compliance 

language specified in AD 2013–26–05 

incorrectly refers to Airbus, instead of 

‘‘Dassault Aviation.’’ We are issuing this 

AD to detect and correct a dormant 

failure in the fire suppression system, 

which could result in the inability to 

put out a fire in an engine, auxiliary 

power unit (APU), or rear compartment. 

DATES: This AD becomes effective May 

8, 2015. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain other publications listed in 

this AD as of October 20, 2014 (79 FR 

54897, dated September 15, 2014). 

We must receive comments on this 

AD by June 8, 2015. 

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, between 9 a.m. and 5 

p.m., Monday through Friday, except 

Federal holidays. 

For service information identified in 

this AD, contact Dassault Falcon Jet, 

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 

Airplane Directorate, 1601 Lind Avenue 

SW., Renton, WA. For information on 

the availability of this material at the 

FAA, call 425–227–1221. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2015– 

0830; 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 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. Comments will be available in 

the AD docket shortly after receipt. 

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 

On August 29, 2014, we issued AD 

2013–26–05, Amendment 39–17714 (79 

FR 54897, September 15, 2014), which 

applied 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. AD 2013–26–05 was 

prompted by reports of a manufacturing 

defect in the charge indicator on fire 

extinguisher bottles. AD 2013–26–05 

required repetitive weighing of fire 

extinguisher bottles having a certain 

part number, and eventual replacement 

of those bottles to terminate the 

repetitive weighing. We issued AD 

2013–26–05 to detect and correct a 

dormant failure in the fire suppression 

system, which could result in the 

inability to put out a fire in an engine, 

APU, or rear compartment. 

AD 2013–26–05, Amendment 39– 

17714 (79 FR 54897, September 15, 

2014), corresponds to Mandatory 

Continuing Airworthiness Information 

(MCAI) European Aviation Safety 

Agency (EASA) AD 2012–0189, dated 

September 24, 2012. You may examine 

the MCAI on the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2015– 

0830. 

Since we issued AD 2013–26–05, 

Amendment 39–17714 (79 FR 54897, 

September 15, 2014), we have 

determined that there is an error in the 

manufacturer’s name in the method of 

compliance language in certain text in 

the ‘‘Explanation of Change Made to 

This AD’’ section and in certain 

paragraphs of the regulatory text of AD 

2013–26–05. AD 2013–26–05 refers to 

Airbus’s EASA Design Organization 

Approval (DOA), instead of Dassault 

Aviation’s EASA DOA. In order to refer 

to the appropriate EASA DOA, this AD 

replaces ‘‘Airbus’s’’ with ‘‘Dassault 

Aviation’s’’ in paragraphs (h)(2), 

(h)(2)(i), (h)(2)(ii), (h)(2)(iii), (h)(2)(iv), 

(i), (i)(1), (i)(2), (i)(3), (i)(4), (j)(1), (j)(2), 

(j)(3), (j)(4), and (l)(2) of this AD. The 

‘‘Explanation of Change Made to This 

AD’’ section of AD 2013–26–05 is not 

restated in this AD. 


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22636 Federal Register / Vol. 80, No. 78 / Thursday, April 23, 2015 / Rules and Regulations 

FAA’s Determination and Requirements 

of This 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 the State of 

Design Authority, we have been notified 

of the unsafe condition described in the 

MCAI and service information 

referenced above. We are issuing this 

AD because we evaluated all pertinent 

information and determined the unsafe 

condition exists and is likely to exist or 

develop on other products of these same 

type designs. 

FAA’s Determination of the Effective 

Date 

We are superseding AD 2013–26–05, 

Amendment 39–17714 (79 FR 54897, 

September 15, 2014), to correct certain 

erroneous manufacturer information in 

the ‘‘Explanation of Changes to This 

AD’’ section and in certain paragraphs 

of the regulatory text. No other changes 

have been made to AD 2013–26–05. 

Therefore, we determined that notice 

and opportunity for prior public 

comment are unnecessary. 

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–2015–0830; 

Directorate Identifier 2015–NM–024– 

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 affects 185 

airplanes of U.S. registry. 

The actions required by AD 2013–26– 

05, Amendment 39–17714 (79 FR 

54897, September 15, 2014), and 

retained in this AD take about 4 workhours per product, at an average labor 

rate of $85 per work-hour. Required 

parts cost about $6,400 per product. 

Based on these figures, the estimated 

cost of the actions that were required by 

AD 2013–26–05 is $1,246,900, or $6,740 

per product. 

The new requirements of this AD add 

no additional economic burden. 

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 

removing airworthiness directive (AD) 

2013–26–05, Amendment 39–17714 (79 

FR 54897, September 15, 2014), and 

adding the following new AD: 

2015–08–05 Dassault Aviation: 

Amendment 39–18141. Docket No. 

FAA–2015–0830; Directorate Identifier 

2015–NM–024–AD. 

(a) Effective Date 

This AD becomes effective May 8, 2015. 

(b) Affected ADs 

This AD replaces AD 2013–26–05, 

Amendment 39–17714 (79 FR 54897, 

September 15, 2014). 

(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 serial numbers. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 26, Fire Protection. 

(e) Reason 

This AD was prompted by reports of a 

manufacturing defect in the charge indicator 

on fire extinguisher bottles and also our 

determination that certain text in the method 

of compliance language specified in AD 

2013–26–05, Amendment 39–17714 (79 FR 

54897, September 15, 2014), incorrectly 

refers to ‘‘Airbus’’ instead of ‘‘Dassault 

Aviation.’’ We are issuing this AD to detect 

and correct a dormant failure in the fire 

suppression system, which could result in 

the inability to put out a fire in an engine, 

auxiliary power unit (APU), or rear 

compartment. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Retained Definitions, With No Changes 

This paragraph restates the requirements of 

paragraph (g) of AD 2013–26–05, 

Amendment 39–17714 (79 FR 54897, 

September 15, 2014), with no changes. For 

the purposes of this AD, the following 

definitions apply. 

(1) An affected fire extinguisher bottle is 

any fire extinguisher bottle having a part 

number included in table 1 to the 

introductory text of paragraph (h) of this AD 

and having a manufacturing batch number 

168 through 200 inclusive on the data plate 

of the charge indicator. 


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Federal Register / Vol. 80, No. 78 / Thursday, April 23, 2015 / Rules and Regulations 22637 

(2) A serviceable fire extinguisher bottle is 

any fire extinguisher bottle having a 

manufacturing batch number lower than 168 

or higher than 200 on the data plate of the 

charge indicator. 

(h) Retained Determining Charge Indicator 

Batch Number, With Revised Method of 

Compliance Language 

This paragraph restates the requirements of 

paragraph (h) of AD 2013–26–05, 

Amendment 39–17714 (79 FR 54897, 

September 15, 2014), with revised method of 

compliance language in paragraphs (h)(2), 

(h)(2)(i), (h)(2)(ii), (h)(2)(iii) and (h)(2)(iv) of 

this AD. Within 30 days or 100 flight hours 

after October 20, 2014 (the effective date of 

AD 2013–26–05), whichever occurs first: 

Determine the manufacturing batch number 

for the charge indicator installed on each 

engine and APU fire extinguisher bottle 

having a part number included in table 1 to 

the introductory text of paragraph (h) of this 

AD, in accordance with the Accomplishment 

Instructions of Dassault Service Bulletin 

F20–785, also referred to as 785, dated June 

11, 2012 (for Model FAN JET FALCON, FAN 

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

airplanes; and Model MYSTERE–FALCON 

20–C5, 20–D5, 20–E5, and 20–F5 airplanes); 

or Dassault Service Bulletin F200–131, also 

referred to as 131, dated June 11, 2012 (for 

Model MYSTERE–FALCON 200 airplanes). 

TABLE 1 TO THE INTRODUCTORY TEXT

OF PARAGRAPH (h) OF THIS AD— 

PART NUMBERS OF AFFECTED FIRE

EXTINGUISHER BOTTLES

Type of bottle— Part No.— 

Engine Fire Extinguisher Bottle.111–1555–324–12A 

Engine Fire Extinguisher Bottle.811456 

Engine Fire Extinguisher Bottle.111–355–32142A 

APU Fire Extinguisher 

Bottle.

111–011–324–12A 

APU Fire Extinguisher 

Bottle.

811475 

(1) For fire extinguisher bottles with part 

numbers that are not included in table 1 to 

the introductory text of paragraph (h) of this 

AD, no further action is required by 

paragraph (h) of this AD. 

(2) For any affected charge indicator, as 

identified in paragraph (g)(1) of this AD: 

Before further flight, weigh each affected fire 

extinguisher bottle, 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). Weigh the fire 

extinguishers thereafter at intervals not to 

exceed 12 months until the replacement 

specified in paragraph (h)(2)(i), (h)(2)(ii), 

(h)(2)(iii), (h)(2)(iv), or (j) of this AD is 

accomplished. If it is determined that the fire 

extinguisher weighs less than the lowest 

weight limit indicated on the fire 

extinguisher’s data plate, before further 

flight, replace any affected fire extinguisher 

bottle and charge indicator cartridge with a 

serviceable part, in accordance with the 

applicable method specified in paragraph 

(h)(2)(i), (h)(2)(ii), (h)(2)(iii), or (h)(2)(iv) of 

this AD. 

Note 1 to paragraph (h)(2) of this AD: The 

instructions specified in Dassault 

Maintenance Procedure, ‘‘Weighing of Engine 

Freon Fire Extinguishers,’’ (page 601, 

‘‘Inspection/Check’’) of Subject 26–20–2, 

‘‘Extinguishing System—Description and 

Operation, of Chapter 26, ‘‘Fire Protection,’’ 

in Book 2 of the Dassault Falcon 20 

Maintenance Manual, Phase 50, dated 

October 2011 (for Model FAN JET FALCON, 

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

airplanes; and Model MYSTERE–FALCON 

20–C5, 20–D5, 20–E5, and 20–F5 airplanes); 

or Procedure 2, ‘‘Engine and Rear 

Compartment Extinguisher (14W1–14W2): 

Weighing’’ of Falcon 200 Maintenance 

Requirement Card 171.0, Revised December 

2011, of Chapter 26, ‘‘Fire Protection,’’ in 

Book 1, ‘‘Work Cards,’’ of the Dassault Falcon 

200 Maintenance Manual, Revision 30, dated 

December 2011 (for Model MYSTERE– 

FALCON 200 airplanes); provide additional 

guidance for weighing affected fire 

extinguisher bottles. This service information 

is not incorporated by reference in this AD. 

(i) For Model FAN JET FALCON, FAN JET 

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

and Model MYSTERE–FALCON 20–C5, 20– 

D5, 20–E5, and 20–F5 airplanes: Replace the 

charge indicator cartridge with a serviceable 

part, in accordance with a method approved 

by the Manager, International Branch, ANM– 

116, Transport Airplane Directorate, FAA; or 

EASA; or Dassault Aviation’s EASA DOA. 

Note 2 to paragraphs (h)(2)(i), (i), (i)(1), 

and (j)(1) of this AD: The instructions 

specified in Dassault Maintenance Procedure, 

‘‘Removal of Pyrotechnical Cartridge for 

Check/Replacement’’ (pages 401–403, 

‘‘Removal/Installation’’), of Subject 26–20–2 

‘‘Extinguishing System—Description and 

Operation,’’ of Chapter 26, ‘‘Fire Protection,’’ 

in Book 2 of the Dassault Falcon 20 

Maintenance Manual, Phase 50, dated 

October 2011, are a source of guidance for the 

actions specified in paragraphs (h)(2)(i), (i), 

(i)(1), and (j)(1) of this AD. This service 

information is not incorporated by reference 

in this AD. 

(ii) For Model FAN JET FALCON, FAN JET 

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

and Model MYSTERE–FALCON 20–C5, 20– 

D5, 20–E5, and 20–F5 airplanes: Replace the 

fire extinguisher bottle with a serviceable 

part, in accordance with a method approved 

by the Manager, International Branch, ANM– 

116, Transport Airplane Directorate, FAA; or 

the EASA; or Dassault Aviation’s EASA 

DOA. 

(iii) For Model MYSTERE–FALCON 200 

airplanes: Replace the charge indicator 

cartridge with a serviceable part, in 

accordance with a method approved by the 

Manager, International Branch, ANM–116, 

Transport Airplane Directorate, FAA; or the 

EASA; or Dassault Aviation’s EASA DOA. 

Note 3 to paragraphs (h)(2)(iii), (i), (i)(3), 

and (j)(3) of this AD: Procedure 3, ‘‘Engine 

and Rear Compartment Extinguisher (14W1– 

14W2): Check/Replacement of Percussion 

Cartridge,’’ of Falcon 200 Maintenance 

Requirement Card 171.0, Revised December 

2011, of Chapter 26, ‘‘Fire Protection’’, in 

Book 1, ‘‘Work Cards,’’ of the Dassault Falcon 

200 Maintenance Manual, Revision 30, dated 

December 2011, is a source of guidance for 

paragraphs (h)(2)(iii), (i), (i)(3), and (j)(3) of 

this AD. This service information is not 

incorporated by reference in this AD. 

(iv) For Model MYSTERE–FALCON 200 

airplanes: Replace the fire extinguisher bottle 

with a serviceable part, in accordance with 

a method approved by the Manager, 

International Branch, ANM–116, Transport 

Airplane Directorate, FAA; or the EASA; or 

Dassault Aviation’s EASA DOA. 

Note 4 to paragraphs (h)(2)(iv), (i)(4), and 

(j)(4) of this AD: Procedure 1, ‘‘Removal/

Installation,’’ of Falcon 200 Maintenance 

Requirement Card 171.0, Revised December 

2011, of Chapter 26, ‘‘Fire Protection’’, in 

Book 1, ‘‘Work Cards,’’ of the Dassault Falcon 

200 Maintenance Manual, Revision 30, dated 

December 2011, is a source of guidance for 

replacing the fire extinguisher bottle. This 

service information is not incorporated by 

reference in this AD. 

(i) Retained Repetitive Inspections To 

Determine if Charge Indicator Cartridge Was 

Fired, With Revised Method of Compliance 

Language 

This paragraph restates the requirements of 

paragraph (i) of AD 2013–26–05, Amendment 

39–17714 (79 FR 54897, September 15, 2014), 

with revised method of compliance language 

in paragraphs (i), (i)(1), (i)(2), (i)(3) and (i)(4) 

of this AD. Within 6 months after October 20, 

2014 (the effective date of AD 2013–26–05): 

Do an inspection to determine if the charge 

indicator cartridge installed on each engine 

and APU fire extinguisher bottle, as 

identified in table 1 to the introductory text 

of paragraph (h) of this AD, was fired, in 

accordance with a method approved by the 

Manager, International Branch, ANM–116, 

Transport Airplane Directorate, FAA; or the 

EASA; or Dassault Aviation’s EASA DOA. 

Repeat the inspection thereafter at intervals 

not to exceed 6 months until the replacement 

specified in paragraph (i)(1), (i)(2), (i)(3), 

(i)(4), or (j) of this AD is accomplished. If it 

is determined that any charge indicator 

cartridge was fired, before further flight, 

replace the affected fire extinguisher bottle 

and charge indicator cartridge with a 

serviceable part, in accordance with a 

method approved by the Manager, 

International Branch, ANM–116, Transport 

Airplane Directorate, FAA; or the EASA; or 

Dassault Aviation’s EASA DOA. 

(1) For Model FAN JET FALCON, FAN JET 

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

and Model MYSTERE–FALCON 20–C5, 2– 

D5, 20–E5, and 20–F5 airplanes: Replace the 

charge indicator cartridge with a serviceable 

part, in accordance with a method approved 

by the Manager, International Branch, ANM– 

116, Transport Airplane Directorate, FAA; or 

the EASA; or Dassault Aviation’s EASA 

DOA. 

(2) For Model FAN JET FALCON, FAN JET 

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

and Model MYSTERE–FALCON 20–C5, 20– 

D5, 20–E5, and 20–F5 airplanes: Replace the 


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22638 Federal Register / Vol. 80, No. 78 / Thursday, April 23, 2015 / Rules and Regulations 

fire extinguisher bottle with a serviceable 

part, in accordance with a method approved 

by the Manager, International Branch, ANM– 

116, Transport Airplane Directorate, FAA; or 

the EASA; or Dassault Aviation’s EASA 

DOA. 

(3) For Model MYSTERE–FALCON 200 

airplanes: Replace the charge indicator 

cartridge with a serviceable part, in 

accordance with a method approved by the 

Manager, International Branch, ANM–116, 

Transport Airplane Directorate, FAA; or the 

EASA; or Dassault Aviation’s EASA DOA. 

(4) For Model MYSTERE–FALCON 200 

airplanes: Replace the fire extinguisher bottle 

with a serviceable part, in accordance with 

a method approved by the Manager, 

International Branch, ANM–116, Transport 

Airplane Directorate, FAA; or the EASA; or 

Dassault Aviation’s EASA DOA. 

(j) Retained Replacement of Fire 

Extinguisher Bottle and Charge Indicator 

Cartridge, With Revised Method of 

Compliance Language 

This paragraph restates the requirements of 

paragraph (j) of AD 2013–26–05, Amendment 

39–17714 (79 FR 54897, September 15, 2014), 

with revised method of compliance language 

specified in paragraphs (j)(1), (j)(2), (j)(3), and 

(j)(4) of this AD. Unless previously 

accomplished as specified in paragraph 

(h)(2)(i), (h)(2)(ii), (h)(2)(iii), (h)(2)(iv), (i)(1), 

(i)(2), (i)(3), or (i)(4) of this AD: Within 60 

months after October 20, 2014 (the effective 

date of AD 2013–26–05), replace any affected 

fire extinguisher bottle and charge indicator 

cartridge, as specified in paragraph (g)(1) of 

this AD, with a serviceable part, in 

accordance with the method specified in 

paragraph (j)(1), (j)(2), (j)(3), or (j)(4) of this 

AD, as applicable. Replacement of any 

affected fire extinguisher bottle and charge 

indicator cartridge with a serviceable part 

terminates the repetitive actions specified in 

paragraphs (h) and (i) of this AD. 

(1) For Model FAN JET FALCON, FAN JET 

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

and Model MYSTERE–FALCON 20–C5, 20– 

D5, 20–E5, and 20–F5 airplanes: Replace the 

charge indicator cartridge with a serviceable 

part, in accordance with a method approved 

by the Manager, International Branch, ANM– 

116, Transport Airplane Directorate, FAA; or 

the EASA; or Dassault Aviation’s EASA 

DOA. 

(2) For Model FAN JET FALCON, FAN JET 

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

and Model MYSTERE–FALCON 20–C5, 20– 

D5, 20–E5, and 20–F5 airplanes: Replace the 

fire extinguisher bottle with a serviceable 

part, in accordance with a method approved 

by the Manager, International Branch, ANM– 

116, Transport Airplane Directorate, FAA; or 

the EASA; or Dassault Aviation’s EASA 

DOA. 

(3) For Model MYSTERE–FALCON 200 

airplanes: Replace the charge indicator 

cartridge with a serviceable part, in 

accordance with a method approved by the 

Manager, International Branch, ANM–116, 

Transport Airplane Directorate, FAA; or the 

EASA; or Dassault Aviation’s EASA DOA. 

(4) For Model MYSTERE–FALCON 200 

airplanes: Replace the fire extinguisher bottle 

with a serviceable part, in accordance with 

a method approved by the Manager, 

International Branch, ANM–116, Transport 

Airplane Directorate, FAA; or the EASA; or 

Dassault Aviation’s EASA DOA. 

(k) Retained Parts Installation Prohibition, 

With No Changes 

This paragraph restates the requirements of 

paragraph (k) of AD 2013–26–05, 

Amendment 39–17714 (79 FR 54897, 

September 15, 2014), with no changes. As of 

October 20, 2014 (the effective date of AD 

2013–26–05), no person may install, on any 

airplane, a fire extinguisher bottle having a 

part number included in table 1 to the 

introductory text of paragraph (h) of this AD, 

fitted with a charge indicator having a 

manufacturing batch number on the data 

plate of 168 through 200 inclusive. 

(l) 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: 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 Branch, ANM– 

116, Transport Airplane Directorate, FAA; or 

the EASA; or Dassault Aviation’s EASA 

DOA. If approved by the DOA, the approval 

must include the DOA-authorized signature. 

(m) Related Information 

Refer to Mandatory Continuing 

Airworthiness Information (MCAI) EASA 

Airworthiness Directive 2012–0189, dated 

September 24, 2012, 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–2015–0830. 

(n) 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 20, 2014, (79 FR 

54897, September 15, 2014). 

(i) Dassault Service Bulletin F20–785, also 

referred to as 785, dated June 11, 2012. 

(ii) Dassault Service Bulletin F200–131, 

also referred to as 131, dated June 11, 2012. 

(4) For service information identified in 

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

2000, South Hackensack, NJ 07606; 

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

www.dassaultfalcon.com. 

(5) You may view this 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. 

(6) 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 9, 

2015. 

Jeffrey E. Duven, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2015–09290 Filed 4–22–15; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF COMMERCE 

Bureau of Industry and Security 

15 CFR Part 744 

[Docket No. 150318286–5286–01] 

RIN 0694–AG58 

Addition of Certain Persons to the 

Entity List 

AGENCY: Bureau of Industry and 

Security, Commerce. 

ACTION: Final rule. 

SUMMARY: This rule amends the Export 

Administration Regulations (EAR) by 

adding eight persons under nine entries 

to the Entity List. The eight persons who 

are added to the Entity List have been 

determined by the U.S. Government to 

be acting contrary to the national 

security or foreign policy interests of the 

United States. These eight persons will 

be listed on the Entity List under the 

destinations of China, Iran, Taiwan, and 

Turkey. There are nine entries for the 

eight persons because one person is 

listed in two locations, resulting in an 

additional entry. Specifically, the 

additional entry covers one person that 

will be listed on the Entity List under 

the destination of Iran and Turkey. 

DATE: Effective Date: This rule is 

effective April 23, 2015. 

FOR FURTHER INFORMATION CONTACT: 

Chair, End-User Review Committee, 


rljohnson on DSK7TPTVN1PROD with RULES