5976 Federal Register / Vol. 71, No. 24 / Monday, February 6, 2006 / Rules and Regulations 

TABLE 4.—SERVICE INFORMATION FOR ACTIONS ACCOMPLISHED PREVIOUSLY

Airbus model Airbus service bulletin 

A330–201, –202, –203, –223, —243, –301, 

–321, –322, –323, –341, –342, and –343 airplanes.

A330–28–3087, dated July 24, 2003. 

A330–28–3089, Revision 01, dated May 12, 2004. 

A340–211, –212, –213, –311, –312, and —313 

airplanes.

A340–28–4100, dated July 24, 2003. 

A340–28–4101, dated July 24, 2003. 

A340–28–4103, Revision 01, dated May 12, 2004. 

A340–28–5010, dated May 7, 2004. 

A340–28–5021, dated April 6, 2005. 

No Submission of Information/Parts 

(j) Where any Airbus service bulletin 

specifies to submit information to Airbus, or 

send removed float valves to either ArgoTech or Intertechnique, those actions are not 

required by this AD. 

Alternative Methods of Compliance 

(AMOCs) 

(k)(1) The Manager, International Branch, 

ANM–116, Transport Airplane Directorate, 

FAA, has the authority to approve AMOCs 

for this AD, if requested in accordance with 

the procedures found in 14 CFR 39.19. 

(2) Before using any AMOC approved in 

accordance with 14 CFR 39.19 on any 

airplane to which the AMOC applies, notify 

the appropriate principal inspector in the 

FAA Flight Standards Certificate Holding 

District Office. 

Related Information 

(l) French airworthiness directives F–

2005–003, dated January 5, 2005, and F–

2005–004 R1 and F–2005–005 R1, both dated 

April 27, 2005, also address the subject of 

this AD. 

Material Incorporated by Reference 

(m) You must use the documents specified 

in Table 5 of this AD to perform the actions 

that are required by this AD, unless the AD 

specifies otherwise. The Director of the 

Federal Register approved the incorporation 

by reference of these documents in 

accordance with 5 U.S.C. 552(a) and 1 CFR 

part 51. Contact Airbus, 1 Rond Point 

Maurice Bellonte, 31707 Blagnac Cedex, 

France, for a copy of this service information. 

You may review copies at the Docket 

Management Facility, U.S. Department of 

Transportation, 400 Seventh Street, SW., 

room PL–401, Nassif Building, Washington, 

DC; on the Internet at http://dms.dot.gov; or 

at the National Archives and Records 

Administration (NARA). For information on 

the availability of this material at the NARA, 

call (202) 741–6030, or go to http:// 

www.archives.gov/federal_register/ 

code_of_federal_regulations/ 

ibr_locations.html. 

TABLE 5.—MATERIAL INCORPORATED BY REFERENCE

Airbus service bulletin Revision 

level Date 

A330–28–3086, excluding Appendix 01 ........................................................................... Original .... July 24, 2003. 

A330–28–3087, excluding Appendix 01 ........................................................................... 01 ............. August 16, 2004. 

A330–28–3088 ................................................................................................................. Original .... April 27, 2004. 

A330–28–3089 ................................................................................................................. 02 ............ April 1, 2005. 

A330–28–3093 ................................................................................................................. Original .... June 16, 2005. 

A330–28–3094 ................................................................................................................. Original .... April 7, 2005. 

A340–28–4100 ................................................................................................................. 01 ............ August 16, 2004. 

A340–28–4101, excluding Appendix 01 ........................................................................... 01 ............. August 16, 2004. 

A340–28–4102 ................................................................................................................. Original .... April 27, 2004. 

A340–28–4103 ................................................................................................................. 02 ............ April 1, 2005. 

A340–28–4111 ................................................................................................................. Original .... April 6, 2005. 

A340–28–5007 ................................................................................................................. Original .... May 7, 2004. 

A340–28–5010 ................................................................................................................. Original .... May 7, 2004. 

A340–28–5021 ................................................................................................................. Original .... April 6, 2005. 

Issued in Renton, Washington, on January 

27, 2006. 

Ali Bahrami, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 06–989 Filed 2–3–06; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. 2003–NM–271–AD; Amendment 

39–14470; AD 2006–03–06] 

RIN 2120–AA64 

Airworthiness Directives; Empresa 

Brasileira de Aeronautica S.A. 

(EMBRAER) Model EMB–135 Airplanes 

and Model EMB–145, –145ER, –145MR, 

–145LR, –145XR, –145MP, and –145EP 

Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: This amendment adopts a 

new airworthiness directive (AD), 

applicable to all Empresa Brasileira de 

Aeronautica S.A. (EMBRAER) Model 

EMB–135 airplanes, and EMB–145, 

–145ER, –145MR, –145LR, –145XR, 

–145MP, and –145EP airplanes. This AD 

requires inspecting the pilot’s and copilot’s seat tracks for proper locking of 

the seats, and adjusting or replacing the 

seat tracks if necessary. This AD also 

requires replacement of the seat locking 

pin on certain SICMA-brand seats. The 

actions specified by this AD are 

intended to prevent uncommanded 

movement of the pilot’s or co-pilot’s 

seat, which could interfere with the 


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Federal Register / Vol. 71, No. 24 / Monday, February 6, 2006 / Rules and Regulations 5977 

operation of the airplane and 

consequent temporary loss of airplane 

control. This action is intended to 

address the identified unsafe condition. 

DATES: Effective March 13, 2006. 

The incorporation by reference of 

certain publications listed in the 

regulations is approved by the Director 

of the Federal Register as of March 13, 

2006. 

ADDRESSES: The service information 

referenced in this AD may be obtained 

from Empresa Brasileira de Aeronautica 

S.A. (EMBRAER), P.O. Box 343—CEP 

12.225, Sao Jose dos Campos—SP, 

Brazil; or SICMA Aero Seat, 7 Rue 

Lucien Coupet, 3600 ISSOUDUN, 

France. This information may be 

examined at the Federal Aviation 

Administration (FAA), Transport 

Airplane Directorate, Rules Docket, 

1601 Lind Avenue, SW., Renton, 

Washington. 

FOR FURTHER INFORMATION CONTACT: 

Todd Thompson, Aerospace Engineer, 

International Branch, ANM–116, 

Transport Airplane Directorate, FAA, 

1601 Lind Avenue, SW., Renton, 

Washington 98055–4056; telephone 

(425) 227–1175; fax (425) 227–1149. 

SUPPLEMENTARY INFORMATION: A 

proposal to amend part 39 of the Federal 

Aviation Regulations (14 CFR part 39) to 

include an airworthiness directive (AD) 

that is applicable to certain Empresa 

Brasileira de Aeronautica S.A. 

(EMBRAER) Model EMB–135 airplanes, 

and EMB–145, –145ER, –145MR, 

–145LR, –145XR, –145MP, and –145EP 

airplanes, was published as a 

supplemental notice of proposed 

rulemaking (NPRM) in the Federal 

Register on November 9, 2005 (70 FR 

67935). That action proposed to require 

inspecting the pilot’s and co-pilot’s seat 

tracks for proper locking of the seats, 

and adjusting or replacing the seat 

tracks if necessary. That action revised 

the applicability and also proposed to 

require replacing the seat locking pin on 

certain SICMA-brand seats. 

Comments 

We provided the public the 

opportunity to participate in the 

development of this AD. No comments 

have been received on the supplemental 

NPRM or on the determination of the 

cost to the public. 

Clarification of Alternative Method of 

Compliance (AMOC) Paragraph 

We revised the supplemental NPRM 

to clarify the appropriate procedure for 

notifying the principal inspector before 

using any approved AMOC on any 

airplane to which the AMOC applies. 

Conclusion 

We have carefully reviewed the 

available data and determined that air 

safety and the public interest require 

adopting the AD with the change 

described previously. We have 

determined that this change will neither 

increase the economic burden on any 

operator nor increase the scope of the 

AD. 

Cost Impact 

The FAA estimates that 550 airplanes 

of U.S. registry are affected by this AD. 

The following table shows the estimated 

cost impact for airplanes affected by this 

AD. The average labor rate is $65 per 

work hour. 

ESTIMATED COSTS

Action 

Number of 

airplanes 

affected 

Work hours Parts cost Total fleet cost 

Inspection to determine seat and serial numbers ................... 550 1 $0 $35,750, or $65 per airplane 

Inspection (Part I of EMBRAER Service Bulletin 145–53–

0027, Revision 03, February 5, 2004).

459 4 0 $119,340, or $260 per airplane 

Inspection and Alignment (Part III of EMRAER SB145–53–

0027, Revision 03, February 5, 2004).

348 4 0 $90,480, or $260 per airplane 

Locking Pin and Spring Replacement (SICMA Aero Seat SB 

147–25–020, Issue 2, December 22, 2003).

459 1 684 $343,791, or $749 per airplane 

The cost impact figures discussed 

above are based on assumptions that no 

operator has yet accomplished any of 

the requirements of this AD action, and 

that no operator would accomplish 

those actions in the future if this AD 

were not adopted. The cost impact 

figures discussed in AD rulemaking 

actions represent only the time 

necessary to perform the specific actions 

actually required by the AD. These 

figures typically do not include 

incidental costs, such as the time 

required to gain access and close up, 

planning time, or time necessitated by 

other administrative actions. 

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 Impact 

The regulations adopted herein 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. Therefore, it is 

determined that this final rule does not 

have federalism implications under 

Executive Order 13132. 

For the reasons discussed above, I 

certify that this action (1) is not a 

‘‘significant regulatory action’’ under 

Executive Order 12866; (2) is not a 

‘‘significant rule’’ under 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. A final evaluation has 

been prepared for this action and it is 

contained in the Rules Docket. A copy 

of it may be obtained from the Rules 

Docket at the location provided under 

the caption ADDRESSES. 


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5978 Federal Register / Vol. 71, No. 24 / Monday, February 6, 2006 / Rules and Regulations 

List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation 

safety, Incorporation by reference, 

Safety. 

Adoption of the Amendment 

■ Accordingly, pursuant to the authority 

delegated to me by the Administrator, 

the Federal Aviation Administration 

amends part 39 of the Federal Aviation 

Regulations (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. Section 39.13 is amended by adding 

the following new airworthiness 

directive: 

2006–03–06 Empresa Brasileira de 

Aeronautica S.A. (EMBRAER): 

Amendment 39–14470. Docket 2003–

NM–271–AD. 

Applicability: All Model EMB–135BJ, 

–135ER, –135KE, –135KL, and –135LR 

airplanes; and Model EMB–145, –145ER, 

–145MR, –145LR, –145XR, –145MP, and 

–145EP airplanes; certificated in any 

category. 

Compliance: Required as indicated, unless 

accomplished previously. 

To prevent uncommanded movement of 

the pilot’s or copilot’s seat, which could 

interfere with the operation of the airplane 

and consequent temporary loss of airplane 

control, accomplish the following: 

Initial Inspection and Corrective Action 

(a) Within 500 flight hours after the 

effective date of this AD, do the actions 

specified in paragraphs (a)(1), (a)(2), and 

(a)(3), as applicable. 

(1) For all airplanes: Do an inspection of 

the pilot’s and co-pilot’s seats for part 

numbers (P/N) and serial numbers (S/N). A 

review of airplane maintenance records is 

acceptable in lieu of this inspection if the P/ 

N and S/N of the seats can be conclusively 

determined from that review. 

(i) If any seat is found to have P/N 

1471610–00 or 1471611–00, and the S/N is 

000 through 324 inclusive: Before further 

flight, do general visual and detailed 

inspection of the seat tracks for proper 

locking of the seats, and do all applicable 

related investigative actions and corrective 

actions, in accordance with Parts I and II, as 

applicable, of the Accomplishment 

Instructions of the EMBRAER Service 

Bulletin 145–53–0027, Revision 03, dated 

February 5, 2004. 

Note 1: For the purposes of this AD, a 

general visual inspection is: ‘‘A visual 

examination of an interior or exterior area, 

installation, or assembly to detect obvious 

damage, failure, or irregularity. This level of 

inspection is made from within touching 

distance unless otherwise specified. A mirror 

may be necessary to ensure visual access to 

all surfaces in the inspection area. This level 

of inspection is made under normally 

available lighting conditions such as 

daylight, hangar lighting, flashlight, or 

droplight and may require removal or 

opening of access panels or doors. Stands, 

ladders, or platforms may be required to gain 

proximity to the area being checked.’’

Note 2: For the purposes of this AD, a 

detailed inspection is: ‘‘An intensive 

examination of a specific item, installation, 

or assembly to detect damage, failure, or 

irregularity. Available lighting is normally 

supplemented with a direct source of good 

lighting at an intensity deemed appropriate. 

Inspection aids such as mirror, magnifying 

lenses, etc., may be necessary. Surface 

cleaning and elaborate procedures may be 

required.’’

Note 3: EMBRAER Service Bulletin 145–

53–0027, Revision 03, dated February 5, 

2004, refers to EMBRAER EMB–145 

Structural Repair Manual, Chapter 53–12–11, 

dated July 18, 2001, as an additional source 

of information on the limits of acceptable 

wear. 

(ii) If seats are found not to have P/N 

1471610–00 or 1471611–00, and a S/N that 

is up to and including 324 inclusive: No 

further action is required by this paragraph. 

(2) For airplanes having S/N 145004 

through 145290 inclusive, do the actions 

specified in paragraph (a)(2)(i) or (a)(2)(ii) of 

this AD, as applicable. 

(i) For airplanes with a seat track having 

P/N 145–33669–001: Do general visual and 

detailed inspections of the seat track(s) for 

proper locking of the seat and excessive 

wear, and do any applicable corrective 

action, in accordance with Parts I and II, as 

applicable, of the Accomplishment 

Instructions of EMBRAER Service Bulletin 

145–53–0027, Revision 03, dated February 5, 

2004. Replace seat tracks that are found to 

have excessive wear within 50 flight hours 

after the inspection with a new seat track 

having P/N 145–33669–003 or 145–33669–

601. Do any other applicable corrective 

action before further flight. Repeat the 

general visual and detailed inspections 

thereafter at intervals not to exceed 500 flight 

hours until the seat track is replaced by a 

new seat track having P/N 145–33669–003 or 

145–33669–601. 

(ii) For airplanes without a seat track 

having P/N 145–33669–001: No further 

action is required by this paragraph. 

(3) For airplanes having S/N 145002 

through 145560 inclusive: If any seat is found 

during the inspection required by paragraph 

(a)(1) of this AD that does not have a P/N and 

S/N specified in paragraph (a)(1)(i) of this 

AD, within 500 flight hours after the effective 

date of this AD, do a general visual and 

detailed inspection of the pilot’s and copilot’s seats for proper locking of the seats, 

and do all applicable related investigative 

and corrective actions in accordance with 

Part III of the Accomplishment Instructions 

of EMBRAER Service Bulletin 145–53–0027, 

Revision 03, dated February 5, 2004, except 

as provided by paragraph (d) of this AD. Do 

any corrective actions before further flight. 

Replacement 

(b) For airplanes with a SICMA seat(s) 

bearing a P/N listed in Table 1 of this AD, 

within 1,000 flight hours after the effective 

date of this AD, replace the seat locking pin 

with a new, improved seat locking pin in 

accordance with the Accomplishment 

Instructions of SICMA Aero Seat Service 

Bulletin 147–25–020, Issue 2, dated 

December 22, 2003. For airplanes without 

any SICMA seat bearing a P/N listed in Table 

1 of this AD, no further action is required by 

this paragraph. 

TABLE 1.—SICMA SEAT P/NS

Part number 

1471610–00 

1471610–01 

1471610–02 

1471610–03 

1471611–00 

1471611–01 

1471611–02 

1471611–03 

Parts Installation 

(c) As of the effective date of this AD, no 

SICMA seat bearing a P/N listed in Table 1 

of this AD may be installed on any airplane 

unless the seat locking pin has been replaced 

in accordance with paragraph (b) of this AD. 

Certain Repairs 

(d) Where the EMBRAER service bulletin 

recommends contacting EMBRAER for 

appropriate action: Before further flight, 

repair per a method approved by either the 

Manager, International Branch, ANM–116, 

Transport Airplane Directorate, FAA; or the 

Departamento de Aviacao Civil (or its 

delegated agent). 

Actions Accomplished Per Previous Issue of 

Service Bulletin 

(e) Accomplishment of the actions 

specified in EMBRAER Service Bulletin 145–

53–0027, dated May 31, 2001; Change 01, 

dated March 12, 2002; or Revision 02, dated 

January 24, 2003; before the effective date of 

this AD, is considered acceptable for 

compliance with the corresponding 

requirements of paragraph (a) of this AD. 

(f) Accomplishment of the actions 

specified in SICMA Aero Seat Service 

Bulletin 147–25–020, dated November 17, 

2003; or Issue 1, dated December 3, 2003; 

before the effective date of this AD, is 

considered acceptable for compliance with 

the requirements of paragraph (b) of this AD. 

Alternative Methods of Compliance 

(g)(1) In accordance with 14 CFR 39.19, the 

Manager, International Branch, ANM–116, 

FAA, is authorized to approve alternative 

methods of compliance (AMOCs) for this AD. 

(2) Before using any AMOC approved in 

accordance with 14 CFR 39.19 on any 

airplane to which the AMOC applies, notify 

the appropriate principal inspector in the 

FAA Flight Standards Certificate Holding 

District Office. 


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Federal Register / Vol. 71, No. 24 / Monday, February 6, 2006 / Rules and Regulations 5979 

Incorporation by Reference 

(h) Unless otherwise specified in this AD, 

the actions must be done in accordance with 

EMBRAER Service Bulletin 145–53–0027, 

Revision 03, dated February 5, 2004; and 

SICMA Aero Seat Service Bulletin 147–25–

020, Issue 2, dated December 22, 2003; as 

applicable. (Pages 6, 8, 10, 12, 14, 16, 18, 20, 

22, 24, 26, and 28 of EMBRAER Service 

Bulletin 145–53–0027 specify an incomplete 

document date; the date on those pages 

should read ‘‘05/Feb/2004.’’) This 

incorporation by reference was approved by 

the Director of the Federal Register in 

accordance with 5 U.S.C. 552(a) and 1 CFR 

part 51. To get copies of this service 

information, contact Empresa Brasileira de 

Aeronautica S.A. (EMBRAER), P.O. Box 

343—CEP 12.225, Sao Jose dos Campos—SP, 

Brazil; or SICMA Aero Seat, 7 Rue Lucien 

Coupet, 36100 ISSOUDUN, France. To 

inspect copies of this service information, go 

to the FAA, Transport Airplane Directorate, 

1601 Lind Avenue, SW., Renton, 

Washington; or to the National Archives and 

Records Administration (NARA). For 

information on the availability of this 

material at the NARA, call (202) 741–6030, 

or go to http://www.archives.gov/ 

federal_register/code_of_federal_regulations/ 

ibr_locations.html. 

Note 4: The subject of this AD is addressed 

in Brazilian airworthiness directive 2002–09–

01R1, effective June 2, 2004. 

Effective Date 

(i) This amendment becomes effective on 

March 13, 2006. 

Issued in Renton, Washington, on January 

24, 2006. 

Ali Bahrami, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 06–990 Filed 2–3–06; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF HEALTH AND 

HUMAN SERVICES 

Food and Drug Administration 

21 CFR Part 17 

Change of Address; Technical 

Amendment 

AGENCY: Food and Drug Administration, 

HHS. 

ACTION: Final rule; technical 

amendment. 

SUMMARY: The Food and Drug 

Administration (FDA) is amending its 

regulations to reflect a change in the 

address for the Departmental Appeals 

Board (DAB). This action is editorial in 

nature and is intended to improve the 

accuracy of the agency’s regulations. 

DATES: This rule is effective February 6, 

2006. 

FOR FURTHER INFORMATION CONTACT: 

Joyce A. Strong, Office of Policy (HF–

27), Food and Drug Administration, 

5600 Fishers Lane, rm. 12A–31, 

Rockville, MD 20857, 301–827–7010. 

SUPPLEMENTARY INFORMATION: This 

document amends FDA’s regulations to 

reflect the address change of the DAB by 

removing the outdated address in 

§ 17.47(a) (21 CFR 17.47(a)) and by 

adding the new address in its place. 

Publication of this document 

constitutes final action on these changes 

under the Administrative Procedure Act 

(5 U.S.C. 553). Notice and public 

procedures are unnecessary because 

FDA is merely correcting 

nonsubstantive errors. 

List of Subjects in 21 CFR Part 17 

Administrative practice and 

procedure, Penalties. 

■ Therefore, under the Federal Food, 

Drug, and Cosmetic Act and under 

authority delegated to the Commissioner 

of Food and Drugs, 21 CFR part 17 is 

amended as follows: 

PART 17—CIVIL MONEY PENALTIES 

HEARINGS 

■ 1. The authority citation for 21 CFR 

part 17 continues to read as follows: 

Authority: 21 U.S.C. 331, 333, 337, 351, 

352, 355, 360, 360c, 360f, 360i, 360j, 371; 42 

U.S.C. 262, 263b, 300aa–28; 5 U.S.C. 554, 

555, 556, 557. 

§ 17.47 [Amended] 

■ 2. Section 17.47 is amended in 

paragraph (a) by removing ‘‘rm. 637–D, 

Hubert H. Humphrey Bldg., 200 

Independence Ave. SW., Washington, 

DC 20201’’ and by adding in its place 

‘‘Appellate Division MS6127, 

Departmental Appeals Board, United 

States Department of Health and Human 

Services, 330 Independence Ave. SW., 

Cohen Bldg., rm. G–644, Washington, 

DC 20201’’. 

Dated: January 30, 2006. 

Jeffrey Shuren, 

Assistant Commissioner for Policy. 

[FR Doc. 06–1040 Filed 2–3–06; 8:45 am] 

BILLING CODE 4160–01–S 

ENVIRONMENTAL PROTECTION 

AGENCY 

40 CFR PART 52 

[EPA–R05–OAR–2005–WI–0003; FRL–8020–

1] 

Approval and Promulgation of 

Implementation Plans; Wisconsin; 

General and Registration Permit 

Programs 

AGENCY: Environmental Protection 

Agency (EPA). 

ACTION: Final rule. 

SUMMARY: EPA is taking final action to 

approve revisions to the Wisconsin 

State Implementation Plan (SIP) 

submitted by the State of Wisconsin on 

July 28, 2005. These revisions include 

General and Registration permit 

programs that provide for the issuance 

of general and registration permits as 

part of the State’s construction permit 

and operation permit programs. In 

addition, these permit programs may 

include the regulation of hazardous air 

pollutants (HAPs) which may be 

regulated under section 112 of the Clean 

Air Act (the Act). Thus, EPA is also 

approving Wisconsin’s general and 

registration permit program under 

section 112(l) of the Act. 

These SIP revisions also contain 

changes to definitions related to 

Wisconsin’s air permit program, as well 

as a minor technical change to provide 

correct references to the updated 

chapter NR 445, which was 

inadvertently omitted in the processing 

of that rule package. Additionally, these 

revisions clarify an existing 

construction permit exemption and 

operation permit exemption for certain 

grain storage and drying operations. 

This clarification is necessary to ensure 

that column dryers and rack dryers are 

included in the exemption criteria. 

DATES: This final rule is effective on 

March 8, 2006. 

ADDRESSES: EPA has established a 

docket for this action under Docket ID 

No. EPA–R05–OAR–2005–WI–0003. All 

documents in the docket are listed on 

the http://www.regulations.gov Web 

site. Although listed in the index, some 

information is not publicly available, 

i.e., 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 either electronically through 

http://www.regulations.gov or in hard 

copy at the Environmental Protection 


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