Federal Register / Vol. 73, No. 155 / Monday, August 11, 2008 / Proposed Rules 46569 

TABLE 3—ALLOWABLE NUMBER OF FLAWS IN PLATES OR FORGING—Continued 

ASME section XI flaw size per IWA–

3200 Range of Through-Wall Extent (TWE) of flaw [in.] 

Allowable number of cumulative flaws per 1000 

square inches of inside diameter surface area in forgings or plates in the ASME 

section XI Appendix VIII 

supplement 4 inspection 

volume 8

0.20 .................................................... 0.175 ≤ TWE < 0.225 .................................................................................... 0.853 

0.25 .................................................... 0.225 ≤ TWE < 0.275 .................................................................................... 0.293 

0.30 .................................................... 0.275 ≤ TWE < 0.325 .................................................................................... 0.0756 

0.35 .................................................... 0.325 ≤ TWE < 0.375 .................................................................................... 0.0144 

8Excluding underclad cracks in forgings. 

TABLE 4—CONSERVATIVE ESTIMATES

FOR CHEMICAL ELEMENT WEIGHT

PERCENTAGES

Materials P Mn 

Plates ................ 0.014 1.45 

TABLE 4—CONSERVATIVE ESTIMATES

FOR CHEMICAL ELEMENT WEIGHT

PERCENTAGES—Continued 

Materials P Mn 

Forgings ............ 0.016 1.11 

TABLE 4—CONSERVATIVE ESTIMATES

FOR CHEMICAL ELEMENT WEIGHT

PERCENTAGES—Continued 

Materials P Mn 

Welds ................ 0.019 1.63 

TABLE 5—MAXIMUM HEAT-AVERAGE RESIDUAL [°F] FOR RELEVANT MATERIAL GROUPS BY NUMBER OF AVAILABLE DATA

POINTS

[Significance level = 1%] 

Material group s [°F] 

Number of available data points 

3 4 5 6 7 8 

Welds, for Cu > 0.072 ...................................................................................... 26.4 35.5 30.8 27.5 25.1 23.2 21.7 

Plates, for Cu > 0.072 ...................................................................................... 21.2 28.5 24.7 22.1 20.2 18.7 17.5 

Forgings, for Cu > 0.072 .................................................................................. 19.6 26.4 22.8 20.4 18.6 17.3 16.1 

Weld, Plate or Forging, for Cu ≤ 0.072 ........................................................... 18.6 25.0 21.7 19.4 17.7 16.4 15.3 

TABLE 6—TMAX VALUES FOR THE

SLOPE DEVIATION TEST

[Significance level = 1%] 

Number of available data points 

(n) TMAX

3 ................................................ 31.82 

4 ................................................ 6.96 

5 ................................................ 4.54 

6 ................................................ 3.75 

7 ................................................ 3.36 

8 ................................................ 3.14 

9 ................................................ 3.00 

10 .............................................. 2.90 

11 .............................................. 2.82 

12 .............................................. 2.76 

14 .............................................. 2.68 

15 .............................................. 2.65 

TABLE 7—THRESHOLD VALUES FOR

THE OUTLIER DEVIATION TEST (SIGNIFICANCE LEVEL = 1%) 

Number of available data points 

(n) 

Second 

largest allowable normalized residual value 

(r*) 

Largest allowable normalized residual value 

(r*) 

3 ........................ 1.55 2.71 

4 ........................ 1.73 2.81 

5 ........................ 1.84 2.88 

TABLE 7—THRESHOLD VALUES FOR

THE OUTLIER DEVIATION TEST (SIGNIFICANCE LEVEL = 1%)—Continued 

Number of available data points 

(n) 

Second 

largest allowable normalized residual value 

(r*) 

Largest allowable normalized residual value 

(r*) 

6 ........................ 1.93 2.93 

7 ........................ 2.00 2.98 

8 ........................ 2.05 3.02 

9 ........................ 2.11 3.06 

10 ...................... 2.16 3.09 

11 ...................... 2.19 3.12 

12 ...................... 2.23 3.14 

13 ...................... 2.26 3.17 

14 ...................... 2.29 3.19 

15 ...................... 2.32 3.21 

Dated at Rockville, Maryland, this 24th day 

of July 2008. 

For the Nuclear Regulatory Commission. 

R.W. Borchardt, 

Executive Director for Operations. 

[FR Doc. E8–18429 Filed 8–8–08; 8:45 am] 

BILLING CODE 7590–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2008–0857; Directorate 

Identifier 2007–NM–317–AD] 

RIN 2120–AA64 

Airworthiness Directives; Dornier 

Model 328–300 Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: The FAA proposes to 

supersede an existing airworthiness 

directive (AD) that applies to all AvCraft 

Dornier Model 328–300 airplanes. The 

existing AD currently requires 

modifying the electrical wiring of the 

fuel pumps; installing insulation at the 

flow control and shut-off valves, and 

other components of the environmental 

control system; installing markings at 

fuel wiring harnesses; replacing the 

wiring harness of the auxiliary fuel 

system with a new wiring harness; and 

installing insulated couplings in the fuel 


rwilkins on PROD1PC63 with PROPOSALS
46570 Federal Register / Vol. 73, No. 155 / Monday, August 11, 2008 / Proposed Rules 

system; as applicable. The existing AD 

also requires revising the Airworthiness 

Limitations section of the Instructions 

for Continued Airworthiness to 

incorporate new inspections of the fuel 

tank system. This proposed AD would 

replace the flight-hour-based threshold 

for conducting certain initial 

inspections, with a calendar-based 

threshold. This proposed AD results 

from fuel system reviews conducted by 

the manufacturer. We are proposing this 

AD to reduce the potential of ignition 

sources inside fuel tanks, which, in 

combination with flammable fuel 

vapors, could result in fuel tank 

explosions and consequent loss of the 

airplane. 

DATES: We must receive comments on 

this proposed AD by September 10, 

2008. 

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 20590, between 9 a.m. 

and 5 p.m., Monday through Friday, 

except Federal holidays. 

For service information identified in 

this AD, contact 328 Support Services 

GmbH, Post Box 1252, D–82231 

Wessling, Germany. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http:// 

www.regulations.gov; or in person at the 

Docket Management Facility between 9 

a.m. and 5 p.m., Monday through 

Friday, except Federal holidays. The AD 

docket contains this proposed AD, the 

regulatory evaluation, any comments 

received, and other information. The 

street address for the Docket 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 

Groves, Aerospace Engineer, 

International Branch, ANM–116, 

Transport Airplane Directorate, FAA, 

1601 Lind Avenue, SW., Renton, 

Washington 98057–3356; telephone 

(425) 227–1503; fax (425) 227–1149. 

SUPPLEMENTARY INFORMATION: 

Comments Invited 

We invite you to send any written 

relevant data, views, or arguments about 

this proposed AD. Send your comments 

to an address listed under the 

ADDRESSES section. Include ‘‘Docket No. 

FAA–2008–0857; Directorate Identifier 

2007–NM–317–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 

On July 20, 2005, we issued AD 2005–

15–16, amendment 39–14205 (70 FR 

44046, August 1, 2005), for certain 

AvCraft Dornier Model 328–300 

airplanes. That AD requires modifying 

the electrical wiring of the fuel pumps; 

installing insulation at the flow control 

and shut-off valves, and other 

components of the environmental 

control system; installing markings at 

fuel wiring harnesses; replacing the 

wiring harness of the auxiliary fuel 

system with a new wiring harness; and 

installing insulated couplings in the fuel 

system; as applicable. That AD also 

requires revising the Airworthiness 

Limitations section (ALS) of the 

Instructions for Continued 

Airworthiness to incorporate new 

inspections of the fuel tank system. That 

AD resulted from fuel system reviews 

conducted by the manufacturer. We 

issued that AD to reduce the potential 

of ignition sources inside fuel tanks, 

which, in combination with flammable 

fuel vapors, could result in fuel tank 

explosions and consequent loss of the 

airplane. 

Actions Since Existing AD Was Issued 

Since we issued AD 2005–15–16, the 

European Aviation Safety Agency 

(EASA), which is the Technical Agent 

for the Member States of the European 

Community, has assumed responsibility 

for the airplane model subject to this 

AD, and has issued EASA 

Airworthiness Directive 2006–0197 

[Corrected], dated July 11, 2006. The 

EASA airworthiness directive revises 

the threshold for conducting the initial 

inspections specified in the 

Airworthiness Limitations section. The 

threshold that we propose to revise was 

originally specified in two German 

airworthiness directives that correspond 

to AD 2005–15–16: German 

airworthiness directives D–2005–002 

and D–2005–063, both dated January 26, 

2005. 

Relevant Service Information 

Dornier has issued Section G, ‘‘Fuel 

Tank System Limitations,’’ Revision 2, 

dated January 31, 2005, of the Dornier 

328 JET Airworthiness Limitations 

Document. The limitations in the 

document are divided into two sections 

as follows: 

• System Code 28–00–00 (sub-tasks 

28–00–00–02 and 28–00–00–03) 

specifies the scheduled maintenance 

tasks, which are detailed inspections of 

the outer and inner internal fuel tank 

harnesses. 

• System Code 28–00–99–00 (subtasks 28–00–99–01, 28–00–99–02, 28–

00–99–03, 28–00–99–04, and 28–00–99–

05) specifies critical design 

configuration control limitations 

(CDCCLs). The limitations apply to the 

cable bundle between the fuel quantity 

indication system and the tank wall, 

and to separation of certain power 

cables and lines from fuel lines. 

FAA’s Determination and Requirements 

of the 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. 

This proposed AD would supersede 

AD 2005–15–16 and would retain the 

requirements of the existing AD. This 

proposed AD would also replace the 

flight-hour-based threshold for 

conducting certain initial inspections, 

with a calendar-based threshold. 

Costs of Compliance 

The following table provides the 

estimated costs for U.S. operators to 

comply with this proposed AD. The 

average labor rate is $80 per work hour. 


rwilkins on PROD1PC63 with PROPOSALS
Federal Register / Vol. 73, No. 155 / Monday, August 11, 2008 / Proposed Rules 46571 

ESTIMATED COSTS

Actions— Work hours Parts Number of U.S.-registered airplanes Cost per airplane Fleet cost 

Modification/installation with option 

033F003 installed (required by AD 

2005–15–16 and retained in this proposed AD).

95 $9,402 None, currently ....... $17,002 if an affected airplane is 

placed on the 

U.S. Register in 

the future.

None. 

Modification/installation without option 

033F003 installed (required by AD 

2005–15–16 and retained in this proposed AD).

70 14,118 28 ............................ 19,718 ..................... $552,104. 

Airworthiness limitations revision ............. 1 None 28 ............................ 80 ............................ $2,240. 

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 have 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 that the 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); 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 proposed AD and placed it in the 

AD docket. See the ADDRESSES section 

for a location to examine the regulatory 

evaluation. 

List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation 

safety, 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 Federal Aviation 

Administration (FAA) amends § 39.13 

by removing amendment 39–14205 (70 

FR 44046, August 1, 2005) and adding 

the following new airworthiness 

directive (AD): 

328 Support Services GMBH (Formerly 

Avcraft Aerospace GmbH): Docket No. 

FAA–2008–0857; Directorate Identifier 

2007–NM–317–AD. 

Comments Due Date 

(a) The FAA must receive comments on 

this AD action by September 10, 2008. 

Affected ADs 

(b) This AD supersedes AD 2005–15–16. 

Applicability 

(c) This AD applies to all Dornier Model 

328–300 airplanes, certificated in any 

category, serial numbers 3105 through 3223 

inclusive. 

Unsafe Condition 

(d) This AD results from fuel system 

reviews conducted by the manufacturer. We 

are issuing this AD to reduce the potential of 

ignition sources inside fuel tanks, which, in 

combination with flammable fuel vapors, 

could result in fuel tank explosions and 

consequent loss of the airplane. 

Compliance 

(e) You are responsible for having the 

actions required by this AD performed within 

the compliance times specified, unless the 

actions have already been done. 

Note 1: This AD requires revisions to 

certain operator maintenance documents to 

include inspections. Compliance with these 

inspections is required by 14 CFR 91.403(c). 

For airplanes that have been previously 

modified, altered, or repaired in the areas 

addressed by these inspections, the operator 

may not be able to accomplish the 

inspections described in the revisions. In this 

situation, to comply with 14 CFR 91.403(c), 

the operator must request approval for an 

alternative method of compliance according 

to paragraph (k) of this AD. The request 

should include a description of changes to 

the required inspections that will ensure the 

continued operational safety of the airplane. 

Restatement of the Requirements of AD 

2005–15–16 

Without Option 033F003 Installed: 

Modification and Installations 

(f) For airplanes without option 033F003 

installed: Within 12 months after September 

6, 2005 (the effective date of AD 2005–15–

16), do the actions in Table 1 of this AD in 

accordance with the Accomplishment 

Instructions of AvCraft Service Bulletin SB–

328J–00–197, dated August 23, 2004. 

TABLE 1—REQUIREMENTS FOR AIRPLANES WITHOUT OPTION 033F003 

INSTALLED

Do the following actions—

By accomplishing all the 

actions specified in—

(1) Modify the electrical wiring of the left-hand and 

right-hand fuel pumps.

Paragraph 

1.B(1) of 

the service 

bulletin. 

(2) Install insulation at the 

left-hand and right-hand 

flow control and shut-off 

valves and other components of the environmental 

control system.

Paragraph 

1.B(2) of 

the service 

bulletin. 

(3) Install markings at fuel 

wiring harnesses.

Paragraph 

1.B(3) of 

the service 

bulletin. 


rwilkins on PROD1PC63 with PROPOSALS
46572 Federal Register / Vol. 73, No. 155 / Monday, August 11, 2008 / Proposed Rules 

With Option 033F003 Installed: Modification, 

Replacement, and Installation 

(g) For airplanes with option 033F003 

installed: Within 12 months after September 

6, 2005, do the actions in Table 2 of this AD 

in accordance with the Accomplishment 

Instructions of AvCraft Service Bulletin SB–

328J–00–198, dated August 23, 2004. 

TABLE 2—REQUIREMENTS FOR AIRPLANES WITH OPTION 033F003 INSTALLED

Do the following actions—

By accomplishing all the 

actions specified in—

(1) Modify the electrical wiring of the left-hand and 

right-hand fuel pumps.

Paragraph 

2.B(1) of 

the service 

bulletin. 

(2) Replace the wiring harness of the auxiliary fuel 

system with a new wiring 

harness.

Paragraph 

2.B(2) of 

the service 

bulletin. 

(3) Install markings at fuel 

wiring harnesses.

Paragraph 

2.B(3) of 

the service 

bulletin. 

(4) Install insulated couplings 

in the fuel system.

Paragraph 

2.B(5) of 

the service 

bulletin. 

Revision to Airworthiness Limitations 

(h) Within 12 months after September 6, 

2005, revise the Airworthiness Limitations 

section of the Instructions for Continued 

Airworthiness to incorporate the information 

in AvCraft Temporary Revision (TR) ALD–

028, dated October 15, 2003, into the AvCraft 

328JET Airworthiness Limitations Document. 

Thereafter, except as provided by paragraph 

(k) of this AD, no alternative inspection 

intervals may be approved for this fuel tank 

system. 

Note 2: This may be done by inserting a 

copy of AvCraft TR ALD–028, dated October 

15, 2003, in the AvCraft 328JET 

Airworthiness Limitations Document. When 

this TR has been included in general 

revisions of the AvCraft 328JET 

Airworthiness Limitations Document, the 

temporary revision no longer needs to be 

inserted into the revised Airworthiness 

Limitations document. 

New Requirements of This AD 

Revised Initial Compliance Time 

(i) For Sub-tasks 28–00–00–02 and 28–00–

00–03 (‘‘Detailed Inspection of Outer and 

Inner Fuel Tank Harness Internal’’), as 

identified in AvCraft TR ALD–028, dated 

October 15, 2003; or Section G, ‘‘Fuel Tank 

System Limitations,’’ Revision 2, dated 

January 31, 2005, of the Dornier 328 JET 

Airworthiness Limitations Document (ALD), 

the initial compliance time is within 8 years 

after the effective date of this AD. Thereafter, 

except as provided by paragraph (k) of this 

AD, these tasks must be accomplished at the 

repetitive interval specified in Section G, 

‘‘Fuel Tank System Limitations,’’ Revision 2, 

dated January 31, 2005, of the Dornier 328 

JET Airworthiness Limitations Document. 

No Alternative Inspections, Inspection 

Intervals, or Critical Design Configuration 

Control Limitations (CDCCLs) 

(j) After accomplishing the actions 

specified in paragraphs (f), (g), and (h), and 

the initial inspections in paragraph (i) of this 

AD, no alternative inspections, inspection 

intervals, or critical design configuration 

control limitations (CDCCLs) may be used 

unless the inspections, intervals, or CDCCLs 

are approved as an alternative method of 

compliance (AMOC) in accordance with the 

procedures specified in paragraph (k) of this 

AD. 

Alternative Methods of Compliance (AMOCs) 

(k) 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: Tom Groves, Aerospace Engineer, 

International Branch, ANM–116, Transport 

Airplane Directorate, FAA, 1601 Lind 

Avenue, SW., Renton, Washington 98057–

3356; telephone (425) 227–1503; fax (425) 

227–1149. Before using any approved AMOC 

on any airplane to which the AMOC applies, 

notify your appropriate principal inspector 

(PI) in the FAA Flight Standards District 

Office (FSDO), or lacking a PI, your local 

FSDO. 

Related Information 

(l) EASA airworthiness directive 2006–

0197 [Corrected], dated July 11, 2006, also 

addresses the subject of this AD. 

Issued in Renton, Washington, on July 29, 

2008. 

Ali Bahrami, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. E8–18434 Filed 8–8–08; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF THE TREASURY 

Internal Revenue Service 

26 CFR Part 1 

[REG–149404–07] 

RIN 1545–BH34 

Amendments to New Markets Tax 

Credit Regulations 

AGENCY: Internal Revenue Service (IRS), 

Treasury. 

ACTION: Notice of proposed rulemaking 

and notice of public hearing. 

SUMMARY: This document contains 

proposed regulations relating to the new 

markets tax credit under section 45D of 

the Internal Revenue Code (Code). The 

proposed regulations revise and clarify 

certain rules relating to recapture of the 

new markets tax credit and will affect 

certain taxpayers claiming the new 

markets tax credit. This document also 

provides a notice of a public hearing on 

these proposed regulations. 

DATES: Written or electronic comments 

must be received by November 10, 2008. 

Outlines of topics to be discussed at the 

public hearing scheduled for December 

12, 2008, at 10 a.m. must be received by 

November 3, 2008. 

ADDRESSES: Send submissions to: 

CC:PA:LPD:PR (REG–149404–07), room 

5203, Internal Revenue Service, PO Box 

7604, Ben Franklin Station, Washington, 

DC 20044. Submissions may be hand 

delivered Monday through Friday 

between the hours of 8 a.m. and 4 p.m. 

to: CC:PA:LPD:PR (REG–149404–07), 

Courier’s Desk, Internal Revenue 

Service, 1111 Constitution Avenue, 

NW., Washington, DC, or sent 

electronically, via the Federal 

eRulemaking Portal at http:// 

www.regulations.gov (IRS REG–149404–

07). The public hearing will be held in 

the IRS Auditorium, Internal Revenue 

Building, 1111 Constitution Avenue, 

NW., Washington, DC. 

FOR FURTHER INFORMATION CONTACT: 

Concerning the proposed regulations, 

Julie Hanlon-Bolton, (202) 622–7028; 

concerning submission of comments, 

the hearing, and/or to be placed on the 

building access list to attend the 

hearing, Regina Johnson, (202) 622–

7180 (not toll-free numbers). 

SUPPLEMENTARY INFORMATION: 

Background 

This document amends 26 CFR part 1 

to provide and clarify rules relating to 

the new markets tax credit under 

section 45D of the Code. Section 45D 

was added to the Code by section 121 

of the Community Renewal Tax Relief 

Act of 2000, Public Law 106–554 (114 

Stat. 2763 (2000)) and amended by 

section 221 of the American Jobs 

Creation Act of 2004, Public Law 108–

357 (118 Stat. 1418 (2004)), section 101 

of the Gulf Opportunity Zone Act of 

2005, Public Law 109–135 (119 Stat. 25 

(2005)), and Division A, section 102 of 

the Tax Relief and Health Care Act of 

2006, Public Law 109–432 (120 Stat. 

2922 (2006)). On December 28, 2004, the 

IRS and the Treasury Department 

published final regulations under 

section 45D (69 FR 77625), with 

corrections on January 28, 2005 (70 FR 

4012). 

Groups and organizations 

representing investors, qualified 

community development entities, 

businesses, and other entities involved 

with the new markets tax credit program 

have since submitted comments 

requesting further guidance on the 


rwilkins on PROD1PC63 with PROPOSALS