Federal Register / Vol. 78, No. 98 / Tuesday, May 21, 2013 / Proposed Rules 29669 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2013–0423; Directorate 

Identifier 2012–NM–176–AD] 

RIN 2120–AA64 

Airworthiness Directives; DASSAULT 

AVIATION Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: We propose to adopt a new 

airworthiness directive (AD) 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. This 

proposed AD was prompted by reports 

of a manufacturing defect in the charge 

indicator on fire extinguisher bottles. 

This proposed AD would require 

repetitive weighing of fire extinguisher 

bottles having a certain part number, 

and eventual replacement of those 

bottles to terminate the repetitive 

weighing. We are proposing 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, 

or rear compartment. 

DATES: We must receive comments on 

this proposed AD by July 5, 2013. 

ADDRESSES: You may send comments by 

any of the following methods: 

• Federal eRulemaking Portal: Go to 

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

instructions for submitting comments. 

• Fax: 202–493–2251. 

• Mail: U.S. Department of 

Transportation, Docket Operations, M– 

30, West Building Ground Floor, Room 

W12–140, 1200 New Jersey Avenue SE., 

Washington, DC 20590. 

• Hand Delivery: U.S. Department of 

Transportation, Docket Operations, M– 

30, West Building Ground Floor, Room 

W12–140, 1200 New Jersey Avenue SE., 

Washington, DC, between 9 a.m. and 5 

p.m., Monday through Friday, except 

Federal holidays. 

For service information identified in 

this proposed AD, contact 

Dassault Falcon Jet, P.O. Box 2000, 

South Hackensack, NJ 07606; telephone 

201–440–6700; Internet http:// 

www.dassaultfalcon.com. You may 

review copies of the referenced service 

information at the FAA, Transport 

Airplane Directorate, 1601 Lind Avenue 

SW., Renton, WA. For information on 

the availability of this material at the 

FAA, call 425–227–1221. 

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 this proposed 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; phone: 425–227–1137; fax: 

425–227–1149. 

SUPPLEMENTARY INFORMATION: 

Comments Invited 

We invite you to send any written 

relevant data, views, or arguments about 

this proposal. Send your comments to 

an address listed under the ADDRESSES

section. Include ‘‘Docket No. FAA– 

2013–0423; Directorate Identifier 2012– 

NM–176–AD’’ at the beginning of your 

comments. We specifically invite 

comments on the overall regulatory, 

economic, environmental, and energy 

aspects of this proposed AD. We will 

consider all comments received by the 

closing date and may amend this 

proposed 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 proposed AD. 

Discussion 

The European Aviation Safety Agency 

(EASA), which is the Technical Agent 

for Member States of the European 

Community, has issued EASA 

Airworthiness Directive 2012–0189, 

dated September 24, 2012 (referred to 

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

unsafe condition for the specified 

products. The MCAI states: 

A manufacturing defect of the charge 

indicator of fire extinguisher bottles has been 

reported on Dassault Aviation Fan Jet Falcon 

and Myste`re-Falcon 20 series aeroplanes. 

The results of the investigations concluded 

that this defect may lead to corrosion of the 

charge indicator, causing improper 

indication of loss of pressure inside the 

bottle. In addition, the Part Numbers (P/N) of 

the fire extinguishers and batch numbers of 

the affected charge indicators have been 

identified. 

This condition, if not detected and 

corrected, could constitute a dormant failure 

that might impact the capability to extinguish 

a fire, either in an engine or the Auxiliary 

Power Unit (APU) or the rear compartment, 

possibly resulting in damage to the aeroplane 

and injury to the occupants. 

For the reasons described above, this 

[EASA] AD requires repetitive weighing of 

the affected fire extinguishers bottles and, 

ultimately replacement of the affected bottles 

with serviceable bottles. In addition, this AD 

prohibits installation of an affected fire 

extinguisher bottle. 

You may obtain further information 

by examining the MCAI in the AD 

docket. 

Relevant Service Information 

Dassault Aviation has issued the 

following service information: 

• Mandatory Service Bulletin F20– 

785, dated June 11, 2012 (for Model 

FAN JET FALCON, FAN JET FALCON 

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

MYSTERE–FALCON 20–C5, 20–D5, 20– 

E5, and 20–F5 airplanes); 

• Mandatory Service Bulletin F200– 

131, dated June 11, 2012 (for Model 

MYSTERE–FALCON 200 airplanes); 

• Dassault Maintenance Procedure 

26–20–3, ‘‘Weighing of Engine Freon 

Fire Extinguishers,’’ dated October 

2009, of Chapter 26 of Book 2 of the 

Falcon 20 Maintenance Manual (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); 

• Dassault Aviation Maintenance 

Procedure 26–20–2, ‘‘Removal of 

Pyrotechnical Cartridge for Check/ 

Replacement,’’ dated October 2010, of 

Chapter 26 of Book 2 of the Falcon 20 

Maintenance Manual (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); 

• Dassault Aviation Falcon 200 

Maintenance Requirement Card 171.0, 

‘‘Engine/Rear compartment Extinguisher 

(14W1–14W2)—Removal/Installation 

(ATA 26–20–06), dated December 2011, 

of Chapter 26 of Book 1 of the Falcon 

200 Maintenance Manual (for Model 

MYSTERE–FALCON 200 airplanes); and 

• Dassault Aviation Falcon 200 

Maintenance Requirement Card 171.0, 

‘‘Engine/Rear compartment Extinguisher 

(14W1–14W2)—Check/Replacement of 

Percussion Cartridge (ATA 26–20–08),’’ 

dated December 2011, of Chapter 26 of 

Book 1 of the Falcon 200 Maintenance 


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29670 Federal Register / Vol. 78, No. 98 / Tuesday, May 21, 2013 / Proposed Rules 

Manual (for Model MYSTERE–FALCON 

200 airplanes). 

The actions described in this service 

information are intended to correct the 

unsafe condition identified in the 

MCAI. 

FAA’s Determination and Requirements 

of This Proposed 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 proposing this 

AD because we evaluated all pertinent 

information and determined an unsafe 

condition exists and is likely to exist or 

develop on other products of the same 

type design. 

Costs of Compliance 

Based on the service information, we 

estimate that this proposed AD would 

affect about 185 products of U.S. 

registry. We also estimate that it would 

take about 4 work-hours per product to 

comply with the basic requirements of 

this proposed AD. The average labor 

rate is $85 per work-hour. Required 

parts would cost about $6,400 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 the 

proposed AD on U.S. operators to be up 

to $1,246,900, or $6,740 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 proposed AD 

would not have federalism implications 

under Executive Order 13132. This 

proposed AD would 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 this proposed regulation: 

(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 proposed AD and placed it in the 

AD docket. 

List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation 

safety, Incorporation by reference, 

Safety. 

The Proposed Amendment 

Accordingly, under the authority 

delegated to me by the Administrator, 

the FAA proposes to amend 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): 

Dassault Aviation: Docket No. FAA–2013– 

0423; Directorate Identifier 2012–NM– 

176–AD. 

(a) Comments Due Date 

We must receive comments by July 5, 2013. 

(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 serial numbers. 

(d) Subject 

Joint Aircraft System Component (JASC)/ 

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. 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, or rear 

compartment. 

(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) Definitions 

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 (P/N) included in table 1 to 

paragraph (h) of this AD and having a 

manufacturing batch number 168 through 

200 inclusive on the data plate of the charge 

indicator. 

(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 charge indicator 

data plate. 

(h) Determining Charge Indicator Batch 

Number 

Within 30 days or 100 flight hours after the 

effective date of this AD, whichever occurs 

first: Determine the manufacturing batch 

number for the charge indicator installed on 

each engine and auxiliary power unit (APU) 

fire extinguisher bottle having a part number 

(P/N) included in table 1 to paragraph (h) of 

this AD, in accordance with the 

Accomplishment Instructions of Dassault 

Mandatory Service Bulletin F20–785, 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 Mandatory Service Bulletin 

F200–131, dated June 11, 2012 (for Model 

MYSTERE-FALCON 200 airplanes). 

TABLE 1 TO PARAGRAPH (h) OF THIS

AD—AFFECTED FIRE EXTINGUISHER

BOTTLES

Type of Bottle— P/N— 

Engine Fire Extinguisher Bottle.P/N 111–1555–324– 

12A. 

P/N 811456. 

P/N 111–355–32142A. 

APU Fire Extinguisher Bottle.P/N 111–011–324– 

12A. 

P/N 811475. 


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Federal Register / Vol. 78, No. 98 / Tuesday, May 21, 2013 / Proposed Rules 29671 

(1) For fire extinguisher bottles with P/Ns 

that are not included in table 1 to paragraph 

(h) of this AD, no further action is required 

by this paragraph. 

(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 the 

instructions specified in Dassault 

Maintenance Procedure 26–20–3, ‘‘Weighing 

of Engine Freon Fire Extinguishers,’’ dated 

October 2009, of Chapter 26 of Book 2 of the 

Falcon 20 Maintenance Manual (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 

Aviation Falcon 200 Maintenance 

Requirement Card 171.0, ‘‘Engine/Rear 

compartment Extinguisher (14W1–14W2)— 

Removal/Installation (ATA 26–20–06),’’ 

dated December 2011, of Chapter 26 of Book 

1 of the Falcon 200 Maintenance Manual (for 

Model MYSTERE-FALCON 200 airplanes). 

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 service information or method 

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

(h)(2)(iii), or (h)(2)(iv) of 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 the instructions 

specified in Dassault Aviation Maintenance 

Procedure 26–20–2, ‘‘Removal of 

Pyrotechnical Cartridge for Check/ 

Replacement,’’ dated October 2010, of 

Chapter 26 of Book 2 of the Falcon 20 

Maintenance Manual. 

(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 European Aviation Safety Agency (EASA) 

(or its delegated agent). 

(iii) For Model MYSTERE-FALCON 200 

airplanes: Replace the charge indicator 

cartridge with a serviceable part, in 

accordance with Dassault Aviation Falcon 

200 Maintenance Requirement Card 171.0, 

‘‘Engine/Rear compartment Extinguisher 

(14W1–14W2)—Check/Replacement of 

Percussion Cartridge (ATA 26–20–08),’’ 

dated December 2011, of Chapter 26 of Book 

1 of the Falcon 200 Maintenance Manual. 

(iv) For Model MYSTERE-FALCON 200 

airplanes: Replace the fire extinguisher bottle 

with a serviceable part, in accordance with 

the instructions specified in Dassault 

Aviation Falcon 200 Maintenance 

Requirement Card 171.0, ‘‘Engine/Rear 

compartment Extinguisher (14W1–14W2)— 

Removal/Installation (ATA 26–20–06),’’ 

dated December 2011, of Chapter 26 of Book 

1 of the Falcon 200 Maintenance Manual. 

(i) Repetitive Inspection To Determine If 

Charge Indicator Cartridge Was Fired 

Within 6 months after the effective date of 

this AD: 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 paragraph (h) of this 

AD, was fired, in accordance with the 

instructions specified in Dassault Aviation 

Maintenance Procedure 26–20–2, ‘‘Removal 

of Pyrotechnical Cartridge for Check/ 

Replacement,’’ dated October 2010, of 

Chapter 26 of Book 2 of the Falcon 20 

Maintenance Manual (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 Aviation Falcon 200 

Maintenance Requirement Card 171.0, 

‘‘Engine/Rear compartment Extinguisher 

(14W1–14W2)—Check/Replacement of 

Percussion Cartridge (ATA 26–20–08),’’ 

dated December 2011, of Chapter 26 of Book 

1 of the Falcon 200 Maintenance Manual (for 

Model MYSTERE–FALCON 200 airplanes). 

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 the 

applicable service information or method 

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

(i)(4) 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, 2– 

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

charge indicator cartridge with a serviceable 

part, in accordance with the instructions 

specified in Dassault Aviation Maintenance 

Procedure 26–20–2, ‘‘Removal of 

Pyrotechnical Cartridge for Check/ 

Replacement,’’ dated October 2010, of 

Chapter 26 of Book 2 of the Falcon 20 

Maintenance Manual. 

(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 European Aviation Safety Agency (EASA) 

(or its delegated agent). 

(3) For Model MYSTERE–FALCON 200 

airplanes: Replace the charge indicator 

cartridge with a serviceable part, in 

accordance with the instructions specified in 

Dassault Aviation Falcon 200 Maintenance 

Requirement Card 171.0, ‘‘Engine/Rear 

compartment Extinguisher (14W1–14W2)— 

Check/Replacement of Percussion Cartridge 

(ATA 26–20–08),’’ dated December 2011, of 

Chapter 26 of Book 1 of the Falcon 200 

Maintenance Manual. 

(4) For Model MYSTERE–FALCON 200 

airplanes: Replace the fire extinguisher bottle 

with a serviceable part, in accordance with 

the instructions specified in Dassault 

Aviation Falcon 200 Maintenance 

Requirement Card 171.0, ‘‘Engine/Rear 

compartment Extinguisher (14W1–14W2)— 

Removal/Installation (ATA 26–20–06), dated 

December 2011, of Chapter 26 of Book 1 of 

the Falcon 200 Maintenance Manual. 

(j) Replacement of Fire Extinguisher Bottle 

and Charge Indicator Cartridge 

Unless previously accomplished as 

specified in paragraphs (h) or (i) of this AD: 

Within 60 months after the effective date of 

this AD, 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 applicable service 

information or method specified in paragraph 

(j)(1), (j)(2), (j)(3), or (j)(4) of this AD. 

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 the instructions 

specified in Dassault Aviation Maintenance 

Procedure 26–20–2, ‘‘Removal of 

Pyrotechnical Cartridge for Check/ 

Replacement,’’ dated October 2010, of 

Chapter 26 of Book 2 of the Falcon 20 

Maintenance Manual. 

(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 its delegated agent). 

(3) For Model MYSTERE-FALCON 200 

airplanes: Replace the charge indicator 

cartridge with a serviceable part, in 

accordance with the instructions specified in 

Dassault Aviation Falcon 200 Maintenance 

Requirement Card 171.0, ‘‘Engine/Rear 

compartment Extinguisher (14W1–14W2)— 

Check/Replacement of Percussion Cartridge 

(ATA 26–20–08),’’ dated December 2011, of 

Chapter 26 of Book 1 of the Falcon 200 

Maintenance Manual. 

(4) For Model MYSTERE-FALCON 200 

airplanes: Replace the fire extinguisher bottle 

with a serviceable part, in accordance with 

the instructions specified in Dassault 

Aviation Falcon 200 Maintenance 

Requirement Card 171.0, ‘‘Engine/Rear 

compartment Extinguisher (14W1–14W2)— 

Removal/Installation (ATA 26–20–06), dated 

December 2011, of Chapter 26 of Book 1 of 

the Falcon 200 Maintenance Manual. 

(k) Parts Installation Prohibition 

As of the effective date of this AD, no 

person may install, on any airplane, a fire 

extinguisher bottle having a P/N included in 

table 1 to paragraph (h) of this AD, fitted with 

a charge indicator having a manufacturing 

batch number on the data plate of 168 

through 200 inclusive. 


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29672 Federal Register / Vol. 78, No. 98 / Tuesday, May 21, 2013 / Proposed Rules 

(l) Other FAA AD Provisions 

The following provisions also apply to this 

AD: 

(1) 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, Washington 98057– 

3356; telephone 425–227–1137; fax 425–227– 

1137. 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. 

(m) Related Information 

(1) Refer to MCAI EASA Airworthiness 

Directive 2012–0189, dated September 24, 

2012, and the following service information 

for related information. 

(i) Dassault Mandatory Service Bulletin 

F20–785, dated June 11, 2012. 

(ii) Dassault Mandatory Service Bulletin 

F200–131, dated June 11, 2012. 

(iii) Dassault Aviation Maintenance 

Procedure 26–20–2, ‘‘Removal of 

Pyrotechnical Cartridge for Check/ 

Replacement,’’ dated October 2010, of 

Chapter 26 of Book 2 of the Falcon 20 

Maintenance Manual. 

(iv) Dassault Maintenance Procedure 26– 

20–3, ‘‘Weighing of Engine Freon Fire 

Extinguishers,’’ dated October 2009, of 

Chapter 26 of Book 2 of the Falcon 20 

Maintenance Manual. 

(v) Dassault Aviation Falcon 200 

Maintenance Requirement Card 171.0, 

‘‘Engine/Rear compartment Extinguisher 

(14W1–14W2)—Removal/Installation (ATA 

26–20–06),’’ dated December 2011, of 

Chapter 26 of Book 1 of the Falcon 200 

Maintenance Manual. 

(vi) Dassault Aviation Falcon 200 

Maintenance Requirement Card 171.0, 

‘‘Engine/Rear compartment Extinguisher 

(14W1–14W2)—Check/Replacement of 

Percussion Cartridge (ATA 26–20–08),’’ 

dated December 2011, of Chapter 26 of Book 

1 of the Falcon 200 Maintenance Manual. 

(2) 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 review 

copies of the referenced service information 

at the FAA, Transport Airplane Directorate, 

1601 Lind Avenue SW., Renton, WA. For 

information on the availability of this 

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

Issued in Renton, Washington, on May 13, 

2013. 

Ali Bahrami, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2013–12077 Filed 5–20–13; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF ENERGY 

Federal Energy Regulatory 

Commission 

18 CFR Part 35 

[Docket No. RM13–2–000] 

Small Generator Interconnection 

Agreements and Procedures 

AGENCY: Federal Energy Regulatory 

Commission. 

ACTION: Notice of Proposed Rulemaking; 

correction. 

SUMMARY: This document contains 

corrections to the proposed rule (RM13– 

2–000) which was published in the 

Federal Register of Friday, February 1, 

2013 (78 FR 7524). The regulations 

revised the pro forma Small Generator 

Interconnection Procedures (SGIP) and 

pro forma Small Generator 

Interconnection Agreement (SGIA) 

originally set forth in Order No. 2006. 

DATES: Effective on [June 3, 2013]. 

FOR FURTHER INFORMATION CONTACT: 

Leslie Kerr (Technical Information), 

Office of Energy Policy and 

Innovation, Federal Energy Regulatory 

Commission, 888 First Street NE., 

Washington, DC 20426, (202) 502– 

8540, Leslie.Kerr@ferc.gov. 

Monica Taba (Technical Information), 

Office of Electric Reliability, Federal 

Energy Regulatory Commission, 888 

First Street NE., Washington, DC 

20426, (202) 502–6789, 

Monica.Taba@ferc.gov. 

Elizabeth Arnold (Legal Information), 

Office of the General Counsel, Federal 

Energy Regulatory Commission, 888 

First Street NE., Washington, DC 

20426, (202) 502–8687, 

Elizabeth.Arnold@ferc.gov. 

SUPPLEMENTARY INFORMATION: 

Errata Notice 

On January 17, 2013, the Commission 

issued an order in the above-referenced 

docket. Small Generator Interconnection 

Agreements and Procedures, 142 FERC 

¶ 61,049 (2013). The order is revised as 

follows: 

The fourth sentence of paragraph 45 

should read, ‘‘This requirement was 

included in Order No. 2006 62 but was 

not made clear in the pro forma SGIP.’’ 

Footnote 62 should read, ‘‘Order No. 

2006, FERC Stats. & Regs. ¶ 31,180 at P 

140.’’ 

In FR Doc. 2013–01366 appearing on 

page 7523 in the Federal Register of 

Friday, February 1, 2013, the same 

corrections are made: 

1. On page 7531, the fourth sentence 

of paragraph 45 should read, ‘‘This 

requirement was included in Order No. 

2006 62 but was not made clear in the 

pro forma SGIP.’’ 

2. On page 7531, Footnote 62 should 

read, ‘‘Order No. 2006, FERC Stats. & 

Regs. ¶ 31,180 at P 140.’’ 

Dated: April 25, 2013. 

Kimberly D. Bose, 

Secretary. 

[FR Doc. 2013–12079 Filed 5–20–13; 8:45 am] 

BILLING CODE 6717–01–P 

DEPARTMENT OF HEALTH AND 

HUMAN SERVICES 

Food and Drug Administration 

21 CFR Part 870 

[Docket No. FDA–2013–N–0487] 

Cardiovascular Devices; 

Reclassification of External CounterPulsating Devices for Treatment of 

Chronic Stable Angina; Effective Date 

of Requirement for Premarket 

Approval for External CounterPulsating Devices for Other Specified 

Intended Uses 

AGENCY: Food and Drug Administration, 

HHS. 

ACTION: Proposed order. 

SUMMARY: The Food and Drug 

Administration (FDA) is issuing a 

proposed administrative order to 

reclassify external counter-pulsating 

(ECP) devices for treatment of chronic 

stable angina that is refractory to 

optimal anti-anginal medical therapy 

and without options for 

revascularization, which is a 

preamendments class III device, into 

class II (special controls) based on new 

information. FDA is also proposing to 

require the filing of a premarket 

approval application (PMA) or a notice 

of completion of a product development 

protocol (PDP) for ECP devices for other 

intended uses specified in this proposed 

order. The Agency is also summarizing 

its proposed findings regarding the 

degree of risk of illness or injury 

designed to be eliminated or reduced by 


erowe on DSK2VPTVN1PROD with PROPOSALS-1