Federal Register / Vol. 75, No. 98 / Friday, May 21, 2010 / Rules and Regulations 28485 

(1) The operator can show that no 

cadmium plating exists in the prohibited 

areas of that propeller; or 

(2) It is a new propeller that has never been 

overhauled. 

Alternative Methods of Compliance 

(l) The Manager, Boston Aircraft 

Certification Office, FAA, has the authority to 

approve alternative methods of compliance 

for this AD if requested using the procedures 

found in 14 CFR 39.19. 

Related Information 

(m) Contact Terry Fahr, Aerospace 

Engineer, Boston Aircraft Certification Office, 

FAA, Engine and Propeller Directorate, 12 

New England Executive Park, Burlington, 

MA 01803; e-mail: terry.fahr@faa.gov; 

telephone (781) 238–7155; fax (781) 238– 

7170, for more information about this AD. 

Material Incorporated by Reference 

(n) You must use Dowty Rotol Service 

Bulletin No. 61–754, dated June 12, 1970 to 

perform the heat treatment required by this 

AD. The Director of the Federal Register 

approved the incorporation by reference of 

this service bulletin in accordance with 5 

U.S.C. 552(a) and 1 CFR part 51. Contact 

Dowty Propellers, Anson Business Park, 

Cheltenham Road East, Gloucester GL2 9QN, 

UK; Telephone 44 (0) 1452 716000; fax 44 (0) 

1452 716001 for a copy of this service 

information. You may review copies at the 

FAA, New England Region, 12 New England 

Executive Park, Burlington, MA; or 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 Burlington, Massachusetts on 

May 5, 2010. 

Peter A. White, 

Assistant Manager, Engine and Propeller 

Directorate, Aircraft Certification Service. 

[FR Doc. 2010–11764 Filed 5–20–10; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2010–0034; Directorate 

Identifier 2009–NM–120–AD; Amendment 

39–16307; AD 2010–11–02] 

RIN 2120–AA64 

Airworthiness Directives; Gulfstream 

Aerospace LP (Type Certificate 

Previously Held by Israel Aircraft 

Industries, Ltd.) Model Gulfstream 100 

Airplanes, and Model Astra SPX and 

1125 Westwind Astra Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: We are superseding an 

existing airworthiness directive (AD) for 

the products listed above. This AD 

results from mandatory continuing 

airworthiness information (MCAI) 

originated by an aviation authority of 

another country to identify and correct 

an unsafe condition on an aviation 

product. The MCAI describes the unsafe 

condition as: 

* * * * * 

Incomplete closure of the MED [main entry 

door] may be followed by in-flight opening 

of the door. As a result, the MED and the 

adjacent fuselage structure may be damaged 

during opening and landing impact. Damage 

to the left engine by flying debris and objects 

may also occur. 

We are issuing this AD to require 

actions to correct the unsafe condition 

on these products. 

DATES: This AD becomes effective June 

25, 2010. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in this AD 

as of June 25, 2010. 

ADDRESSES: You may examine the AD 

docket on the Internet at http:// 

www.regulations.gov or in person at the 

U.S. Department of Transportation, 

Docket Operations, M–30, West 

Building Ground Floor, Room W12–140, 

1200 New Jersey Avenue, SE., 

Washington, DC. 

FOR FURTHER INFORMATION CONTACT: 

Mike Borfitz, Aerospace Engineer, 

International Branch, ANM–116, 

Transport Airplane Directorate, FAA, 

1601 Lind Avenue, SW., Renton, 

Washington 98057–3356; telephone 

(425) 227–2677; fax (425) 227–1149. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 to include an AD that would 

apply to the specified products. That 

NPRM was published in the Federal 

Register on February 8, 2010 (75 FR 

6157), and proposed to supersede AD 

2007–03–05, Amendment 39–14916 (72 

FR 4414, January 31, 2007). That NPRM 

proposed to correct an unsafe condition 

for the specified products. The MCAI 

states: 

To increase pilots’ awareness to the 

possibility of incomplete closure of the Main 

Entry Door (MED) by the following means: 

1. Splitting the common caution light 

CABIN DOOR signaling both MED Improper 

Closure and MED Inflatable Seal Failure into 

two separate lights: CABIN DOOR and 

CABIN DOOR SEAL. 

2. Converting the separated CABIN DOOR 

Caution light into a Warning light by 

changing its color to red. 

Note: Aircraft Flight Manuals (AFM’S) 

refer to these changes as MOD G1–20052. 

Incomplete closure of the MED may be 

followed by in-flight opening of the door. As 

a result, the MED and the adjacent fuselage 

structure may be damaged during opening 

and landing impact. Damage to the left 

engine by flying debris and objects may also 

occur. 

Required actions include modifying the 

warning and caution lights panel 

(WACLP), changing the WACLP and 

MED wiring, changing the wiring 

harness connecting the MED to the 

WACLP, and ensuring the Log of 

Modification of the AFM includes 

reference to MOD G1–20052. You may 

obtain further information by examining 

the MCAI in the AD docket. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

received no comments on the NPRM or 

on the determination of the cost to the 

public. 

Explanation of Change to Applicability 

We have revised the applicability of 

the existing AD to identify model 

designations as published in the most 

recent type certificate data sheet for the 

affected models. 

Conclusion 

We reviewed the available data and 

determined that air safety and the 

public interest require adopting the AD 

with the changes described previously. 

We determined that these changes will 

not increase the economic burden on 

any operator or increase the scope of the 

AD. 

Differences Between This AD and the 

MCAI or Service Information 

We have reviewed the MCAI and 

related service information and, in 

general, agree with their substance. But 

we might have found it necessary to use 

different words from those in the MCAI 

to ensure the AD is clear for U.S. 

operators and is enforceable. In making 

these changes, we do not intend to differ 

substantively from the information 

provided in the MCAI and related 

service information. 

We might also have required different 

actions in this AD from those in the 

MCAI in order to follow our FAA 

policies. Any such differences are 

highlighted in a Note within the AD. 

Explanation of Change to Costs of 

Compliance 

Since issuance of the NPRM, we have 

increased the labor rate used in the 

Costs of Compliance from $80 per workhour to $85 per work-hour. The Costs of 

Compliance information, below, reflects 


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28486 Federal Register / Vol. 75, No. 98 / Friday, May 21, 2010 / Rules and Regulations 

this increase in the specified hourly 

labor rate. 

Costs of Compliance 

Based on the service information, we 

estimate that this AD will affect about 

120 products of U.S. registry. 

The actions that are required by AD 

2007–03–05 and retained in this AD 

take about 1 work-hour per product, at 

an average labor rate of $85 per work 

hour. Based on these figures, the 

estimated cost of the currently required 

actions is $85 per product. 

We estimate that it will take about 60 

additional work-hours per product to 

comply with the new basic 

requirements of this AD. Required parts 

will cost about $600 per product. The 

average labor rate is $85 per work-hour. 

Where the service information lists 

required parts costs that are covered 

under warranty, we have assumed that 

there will be no charge for these costs. 

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 AD on U.S. operators to be 

$684,000, or $5,700 per product. 

Authority for This Rulemaking 

Title 49 of the United States Code 

specifies the FAA’s authority to issue 

rules on aviation safety. Subtitle I, 

section 106, describes the authority of 

the FAA Administrator. ‘‘Subtitle VII: 

Aviation Programs,’’ describes in more 

detail the scope of the Agency’s 

authority. 

We are issuing this rulemaking under 

the authority described in ‘‘Subtitle VII, 

Part A, Subpart III, Section 44701: 

General requirements.’’ Under that 

section, Congress charges the FAA with 

promoting safe flight of civil aircraft in 

air commerce by prescribing regulations 

for practices, methods, and procedures 

the Administrator finds necessary for 

safety in air commerce. This regulation 

is within the scope of that authority 

because it addresses an unsafe condition 

that is likely to exist or develop on 

products identified in this rulemaking 

action. 

Regulatory Findings 

We determined that this AD will not 

have federalism implications under 

Executive Order 13132. This AD will 

not have a substantial direct effect on 

the States, on the relationship between 

the national government and the States, 

or on the distribution of power and 

responsibilities among the various 

levels of government. 

For the reasons discussed above, I 

certify 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); and 

3. Will not have a significant 

economic impact, positive or negative, 

on a substantial number of small entities 

under the criteria of the Regulatory 

Flexibility Act. 

We prepared a regulatory evaluation 

of the estimated costs to comply with 

this AD and placed it in the AD docket. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http:// 

www.regulations.gov; or in person at the 

Docket Operations office between 9 a.m. 

and 5 p.m., Monday through Friday, 

except Federal holidays. The AD docket 

contains the NPRM, 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. 

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 Amendment 39–14916 (72 FR 

4414, January 31, 2007) and adding the 

following new AD: 

2010–11–02 Gulfstream Aerospace LP 

(Type Certificate Previously Held by 

Israel Aircraft Industries, Ltd.): 

Amendment 39–16307. Docket No. 

FAA–2010–0034; Directorate Identifier 

2009–NM–120–AD. 

Effective Date 

(a) This airworthiness directive (AD) 

becomes effective June 25, 2010. 

Affected ADs 

(b) This AD supersedes AD 2007–03–05, 

Amendment 39–14916. 

Applicability 

(c) This AD applies to Gulfstream 

Aerospace LP (Type Certificate previously 

held by Israel Aircraft Industries, Ltd.) Model 

Gulfstream 100 airplanes; and Model Astra 

SPX and 1125 Westwind Astra airplanes; 

certificated in any category; all serial 

numbers. 

Subject 

(d) Air Transport Association (ATA) of 

America Code 31: Instruments. 

Reason 

(e) The mandatory continuing 

airworthiness information (MCAI) states: 

To increase pilots’ awareness to the 

possibility of incomplete closure of the Main 

Entry Door (MED) by the following means: 

1. Splitting the common caution light 

CABIN DOOR signaling both MED Improper 

Closure and MED Inflatable Seal Failure into 

two separate lights: CABIN DOOR and 

CABIN DOOR SEAL. 

2. Converting the separated CABIN DOOR 

Caution light into a Warning light by 

changing its color to red. 

Note: Aircraft Flight Manuals (AFMs) refer 

to these changes as MOD G1–20052. 

Incomplete closure of the MED may be 

followed by in-flight opening of the door. As 

a result, the MED and the adjacent fuselage 

structure may be damaged during opening 

and landing impact. Damage to the left 

engine by flying debris and objects may also 

occur. 

Required actions include modifying the 

warning and caution lights panel (WACLP), 

changing the WACLP and MED wiring, 

changing the wiring harness connecting the 

MED to the WACLP, and ensuring the Log of 

Modification of the AFM includes reference 

to MOD G1–20052. 

Restatement of Requirements of AD 2007– 

03–05, With No Changes 

(f) Unless already done, do the following 

actions. Within 10 days after February 15, 

2007 (the effective date of AD 2007–03–05), 

amend Section IV, Normal Procedures, of the 

following Gulfstream airplane flight manuals 

(AFMs): Model 1125 Astra, 25W–1001–1; 

Model Astra SPX, SPX–1001–1; and Model 

G100, G100–1001–1; as applicable; to include 

the following statement. Insertion of copies 

of this AD at the appropriate places of the 

AFMs is acceptable. 

‘‘1. BEFORE ENGINE START: 

(PRE and POST Mod 20052/Gulfstream 

Service Bulletin 100–31–284): 

CABIN DOOR—CLOSED (Physically verify 

door latch handle pin is fully engaged in the 

handle lock) 

2. BEFORE TAXIING: 

Change the CABIN DOOR procedure as 

follows (POST Mod 20052/Gulfstream 

Service Bulletin 100–31–284): 

Check CABIN DOOR light—OUT 

3. BEFORE TAKE–OFF: 

Insert between the POSITION lights switch 

and the THRUST LEVERS procedures: 

(PRE Mod 20052/Gulfstream Service 

Bulletin 100–31–284): 

Check CABIN DOOR light—OUT (50% N1 

may be required) 

(POST Mod 20052/Gulfstream Service 

Bulletin 100–31–284): 

Check CABIN DOOR light—OUT 

CABIN DOOR SEAL light—OUT (50% N1 

may be required)’’ 


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Federal Register / Vol. 75, No. 98 / Friday, May 21, 2010 / Rules and Regulations 28487 

Note 1: Mod 20052 is equivalent to 

Gulfstream Service Bulletin 100–31–284, 

dated August 17, 2006. 

Note 2: This AD may be accomplished by 

a holder of a Private Pilot’s License. 

NEW REQUIREMENTS OF THIS AD: 

Actions and Compliance 

(g) Unless already done, for all airplanes 

except airplane serial number 158, do the 

following actions. 

(1) Within 250 flight hours after the 

effective date of this AD: Modify the WACLP 

in accordance with the Accomplishment 

Instructions of the applicable service bulletin 

identified in Table 1 of this AD. 

TABLE 1—MODIFICATION SERVICE

INFORMATION

Honeywell Service 

Bulletin— Dated— 

80–0548–31–0001 ....... April 1, 2006. 

80–0548–31–0002 ....... March 1, 2006. 

80–5090–31–0001 ....... March 1, 2006. 

(2) Within 250 flight hours after the 

effective date of this AD: Change the WACLP 

and MED wiring in accordance with the 

Accomplishment Instructions of Gulfstream 

Service Bulletin 100–31–284, dated August 

17, 2006. 

(3) Within 250 flight hours after the 

effective date of this AD: Change the wiring 

harness connecting the MED to the WACLP 

in accordance with the Accomplishment 

Instructions of Gulfstream Service Bulletin 

100–31–284, dated August 17, 2006. 

(4) Within 250 flight hours after the 

effective date of this AD: Verify that the Log 

of Modification of the relevant airplane flight 

manual (AFM) includes reference to MOD 

G1–20052, and, if no reference is found, 

revise the Log of Modification of the AFM to 

include reference to the modification. 

(5) Doing the modifications specified in 

paragraphs (g)(1), (g)(2), (g)(3), and (g)(4) of 

this AD terminates the requirements of 

paragraph (f) of this AD, and after the 

modifications have been done, the AFM 

limitation required by paragraph (f) of this 

AD may be removed from the AFM. 

FAA AD Differences 

Note 3: This AD differs from the MCAI 

and/or service information as follows: 

Paragraph (g)(5) of this AD mandates a 

terminating action. However, Israeli 

Airworthiness Directive 31–06–11–05, dated 

May 27, 2009, does not explicitly mandate a 

terminating action. This difference has been 

coordinated with the Civil Aviation 

Authority of Israel. 

Other FAA AD Provisions 

(h) 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. 

Send information to Attn: Mike Borfitz, 

Aerospace Engineer, International Branch, 

ANM–116, Transport Airplane Directorate, 

FAA, 1601 Lind Avenue, SW., Renton, 

Washington 98057–3356; telephone (425) 

227–2677; fax (425) 227–1149. Before using 

any approved AMOC on any airplane to 

which the AMOC applies, notify your 

principal maintenance inspector (PMI) or 

principal avionics inspector (PAI), as 

appropriate, or lacking a principal inspector, 

your local Flight Standards 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. 

(3) Reporting Requirements: For any 

reporting requirement in this AD, under the 

provisions of the Paperwork Reduction Act 

(44 U.S.C. 3501 et seq.), the Office of 

Management and Budget (OMB) has 

approved the information collection 

requirements and has assigned OMB Control 

Number 2120–0056. 

Related Information 

(i) Refer to MCAI Israeli Airworthiness 

Directive 31–06–11–05, dated May 27, 2009, 

and the applicable service information 

identified in Table 2 of this AD for related 

information. 

TABLE 2—SERVICE INFORMATION

Service information Date 

Gulfstream Service Bulletin 100–31–284 .................................................................................................................................... August 17, 2006. 

Honeywell Service Bulletin 80–0548–31–0001 ........................................................................................................................... April 1, 2006. 

Honeywell Service Bulletin 80–0548–31–0002 ........................................................................................................................... March 1, 2006. 

Honeywell Service Bulletin 80–5090–31–0001 ........................................................................................................................... March 1, 2006. 

Material Incorporated by Reference 

(j) You must use the service information 

contained in Table 3 of this AD to do the 

actions required by this AD, unless the AD 

specifies otherwise. 

(1) The Director of the Federal Register 

approved the incorporation by reference of 

the service information contained in Table 3 

of this AD under 5 U.S.C. 552(a) and 1 CFR 

part 51. 

TABLE 3—MATERIAL INCORPORATED BY REFERENCE

Service information Date 

Gulfstream Service Bulletin 100–31–284 .................................................................................................................................... August 17, 2006. 

Honeywell Service Bulletin 80–0548–31–0001 ........................................................................................................................... April 1, 2006. 

Honeywell Service Bulletin 80–0548–31–0002 ........................................................................................................................... March 1, 2006. 

Honeywell Service Bulletin 80–5090–31–0001 ........................................................................................................................... March 1, 2006. 

(2) For Gulfstream service information 

identified in this AD, contact Gulfstream 

Aerospace Corporation, P.O. Box 2206, Mail 

Station D–25, Savannah, Georgia 31402– 

2206; telephone 800–810–4853; fax 912–965– 

3520; e-mail pubs@gulfstream.com; Internet 

http://www.gulfstream.com/ 

product_support/technical_pubs/pubs/ 

index.htm. For Honeywell service 

information identified in this AD, contact 

Honeywell Aerospace, Technical 

Publications and Distribution, M/S 2101– 

201, P.O. Box 52170, Phoenix, Arizona 

85072–2170; telephone 602–365–5535; fax 

602–365–5577; Internet http:// 

www.honeywell.com. 

(3) You may review copies of the service 

information at the FAA, Transport Airplane 

Directorate, 1601 Lind Avenue, SW., Renton, 

Washington. For information on the 

availability of this material at the FAA, call 

425–227–1221. 

(4) You may also review copies of the 

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/ 


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28488 Federal Register / Vol. 75, No. 98 / Friday, May 21, 2010 / Rules and Regulations 

code_of_federal_regulations/ 

ibr_locations.html. 

Issued in Renton, Washington, on May 7, 

2010. 

Ali Bahrami, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2010–11760 Filed 5–20–10; 8:45 am] 

BILLING CODE 4910–13–P 

ENVIRONMENTAL PROTECTION 

AGENCY 

40 CFR Part 180 

[EPA–HQ–OPP–2009–0663; FRL–8824–9] 

Silver Nitrate; Exemption from the 

Requirement of a Tolerance 

AGENCY: Environmental Protection 

Agency (EPA). 

ACTION: Final rule. 

SUMMARY: This regulation establishes an 

exemption from the requirement of a 

tolerance for residues of silver nitrate 

(CAS Reg. No. 7761–88–8) when used as 

an inert ingredient under 40 CFR 

180.910 as stabilizer at a maximum of 

0.06% by weight in pesticide 

formulations as post–harvest treatment 

for potatoes to control sprouting. 

Wagner Regulatory Associates on behalf 

of Pimi Agro CleanTech, Ltd. submitted 

a petition to EPA under the Federal 

Food, Drug, and Cosmetic Act (FFDCA), 

requesting establishment of an 

exemption from the requirement of a 

tolerance. This regulation eliminates the 

need to establish a maximum 

permissible level for residues of silver 

nitrate. 

DATES: This regulation is effective May 

21, 2010. Objections and requests for 

hearings must be received on or before 

July 20, 2010, and must be filed in 

accordance with the instructions 

provided in 40 CFR part 178 (see also 

Unit I.C. of the SUPPLEMENTARY

INFORMATION). 

ADDRESSES: EPA has established a 

docket for this action under docket 

identification (ID) number EPA–HQ– 

OPP–2009–0663. All documents in the 

docket are listed in the docket index 

available at http://www.regulations.gov. 

Although listed in the index, some 

information is not publicly available, 

e.g., Confidential Business Information 

(CBI) or other information whose 

disclosure is restricted by statute. 

Certain other material, such as 

copyrighted material, is not placed on 

the Internet and will be publicly 

available only in hard copy form. 

Publicly available docket materials are 

available in the electronic docket at 

http://www.regulations.gov, or, if only 

available in hard copy, at the OPP 

Regulatory Public Docket in Rm. S– 

4400, One Potomac Yard (South Bldg.), 

2777 S. Crystal Dr., Arlington, VA. The 

Docket Facility is open from 8:30 a.m. 

to 4 p.m., Monday through Friday, 

excluding legal holidays. The Docket 

Facility telephone number is (703) 305– 

5805. 

FOR FURTHER INFORMATION CONTACT: 

Alganesh Debesai, Registration Division 

(7505P), Office of Pesticide Programs, 

Environmental Protection Agency, 1200 

Pennsylvania Ave., NW., Washington, 

DC 20460–0001; telephone number: 

(703) 308–8353; e-mail address: 

debesai.alganesh@epa.gov. 

SUPPLEMENTARY INFORMATION: 

I. General Information 

A. Does this Action Apply to Me? 

You may be potentially affected by 

this action if you are an agricultural 

producer, food manufacturer, or 

pesticide manufacturer. Potentially 

affected entities may include, but are 

not limited to: 

• Crop production (NAICS code 111). 

• Animal production (NAICS code 

112). 

• Food manufacturing (NAICS code 

311). 

• Pesticide manufacturing (NAICS 

code 32532). 

This listing is not intended to be 

exhaustive, but rather provides a guide 

for readers regarding entities likely to be 

affected by this action. Other types of 

entities not listed in this unit could also 

be affected. The North American 

Industrial Classification System 

(NAICS) codes have been provided to 

assist you and others in determining 

whether this action might apply to 

certain entities. If you have any 

questions regarding the applicability of 

this action to a particular entity, consult 

the person listed under FOR FURTHER

INFORMATION CONTACT. 

B. How Can I Get Electronic Access to 

Other Related Information? 

You may access a frequently updated 

electronic version of 40 CFR part 180 

through the Government Printing 

Office’s e-CFR cite at http:// 

www.gpoaccess.gov/ecfr 

C. Can I File an Objection or Hearing 

Request? 

Under section 408(g) of FFDCA, 21 

U.S.C. 346a, and any person may file an 

objection to any aspect of this regulation 

and may also request a hearing on those 

objections. The EPA procedural 

regulations which govern the 

submission of objections and requests 

for hearings appear in 40 CFR part 178. 

You must file your objection or request 

a hearing on this regulation in 

accordance with the instructions 

provided in 40 CFR part 178. To ensure 

proper receipt by EPA, you must 

identify docket ID number EPA–HQ– 

OPP–2009–0663 in the subject line on 

the first page of your submission. All 

objections and requests for a hearing 

must be in writing, and must be 

received by the Hearing Clerk on or 

before [date 60 days after date of 

publication in the Federal Register]. 

Addresses for mail and hand delivery of 

objections and hearing requests are 

provided in 40 CFR 178.25(b). 

In addition to filing an objection or 

hearing request with the Hearing Clerk 

as described in 40 CFR part 178, please 

submit a copy of the filing that does not 

contain any CBI for inclusion in the 

public docket that is described in 

ADDRESSES. Information not marked 

confidential pursuant to 40 CFR part 2 

may be disclosed publicly by EPA 

without prior notice. Submit your 

copies, identified by docket ID number 

EPA–HQ–OPP–2009–0663 by one 

following methods: 

• Federal eRulemaking Portal: http:// 

www.regulations.gov. Follow the on-line 

instructions for submitting comments. 

• Mail: Office of Pesticide Programs 

(OPP) Regulatory Public Docket (7502P), 

Environmental Protection Agency, 1200 

Pennsylvania Ave., NW., Washington, 

DC 20460–0001. 

• Delivery: OPP Regulatory Public 

Docket (7502P), Environmental 

Protection Agency, Rm. S–4400, One 

Potomac Yard (South Bldg.), 2777 S. 

Crystal Dr., Arlington, VA. Deliveries 

are only accepted during the Docket 

Facility’s normal hours of operation 

(8:30 a.m. to 4 p.m., Monday through 

Friday, excluding legal holidays). 

Special arrangements should be made 

for deliveries of boxed information. The 

Docket Facility telephone number is 

(703) 305–5805. 

II. Petition for Exemption 

In the Federal Register of October 7, 

2009 (74 FR 5159) (FRL–8792–7), EPA 

issued a notice pursuant to section 408 

of FFDCA, 21 U.S.C. 346a, announcing 

the filing of a pesticide petition (PP 

9E7584) by Wagner Regulatory 

Associates on behalf of Pimi Agro 

CleanTech, Ltd., P.O.Box. 117, Hutzot 

Alonim 30049, Israel. The petition 

requested that 40 CFR 180.910 be 

amended establishing an exemption 

from the requirement of a tolerance for 

residues of silver nitrate (CAS Reg. No. 

7761–88–8) when used as an inert 

ingredient stabilizer at 0.06% by weight 

in pesticide formulations applied to 


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