This section of the FEDERAL REGISTER

contains regulatory documents having general

applicability and legal effect, most of which

are keyed to and codified in the Code of

Federal Regulations, which is published under

50 titles pursuant to 44 U.S.C. 1510.

The Code of Federal Regulations is sold by

the Superintendent of Documents. Prices of

new books are listed in the first FEDERAL

REGISTER issue of each week.

Rules and Regulations Federal Register

33013

Vol. 66, No. 119

Wednesday, June 20, 2001

NUCLEAR REGULATORY

COMMISSION

10 CFR Part 2

RIN 3150–AG44

Licensing Proceedings for the Receipt

of High-Level Radioactive Waste at a

Geologic Repository; Licensing

Support Network, Design Standards

for Participating Websites; Correction

AGENCY: Nuclear Regulatory

Commission.

ACTION: Final rule; correction.

SUMMARY: This document corrects a

rulemaking appearing in the Federal

Register on May 31, 2001 (66 FR 29453).

This document is necessary to correct

the omission of a word.

FOR FURTHER INFORMATION CONTACT:

Francis X. Cameron, Office of the

General Counsel, Nuclear Regulatory

Commission, telephone 301–415–1642,

e-mail: fxc@nrc.gov.

SUPPLEMENTARY INFORMATION: On page

29460, in the third column, in Footnote

3, the 21st line, insert the word ‘‘or’’

after ‘‘application’’.

Dated at Rockville, Maryland, this 14th day

of June 2001.

For the Nuclear Regulatory Commission.

Alzonia W. Shepard,

Acting Chief, Rules and Directives Branch,

Division of Administrative Services, Office

of Administration.

[FR Doc. 01–15473 Filed 6–19–01; 8:45 am]

BILLING CODE 7590–01–P

NUCLEAR REGULATORY

COMMISSION

10 CFR Part 72

RIN 3150–AF94

Changes, Tests, and Experiments;

Correction

AGENCY: Nuclear Regulatory

Commission.

ACTION: Final rule; correction.

SUMMARY: This document is necessary to

correct three erroneous Federal Register

citations appearing in a document

published on February 26, 2001 (66 FR

11527).

FOR FURTHER INFORMATION CONTACT:

Jayne McCausland, Office of Nuclear

Material Safety and Safeguards, Nuclear

Regulatory Commission, telephone 301–

415–6219, e-mail: jmm@nrc.gov.

SUPPLEMENTARY INFORMATION:

On page 11527, in the first column, in

the SUMMARY paragraph, in the third

line, ‘‘65’’ is corrected to read ‘‘64.’’

On page 11527, in the first column, in

the Background paragraph, in both the

first and last lines of the paragraph,

‘‘64’’ is corrected to read ‘‘63’’.

Dated at Rockville, Maryland, this 14th day

of June 2001.

For the Nuclear Regulatory Commission.

Alzonia W. Shepard,

Acting Chief, Rules and Directives Branch,

Division of Administrative Services, Office

of Administration.

[FR Doc. 01–15472 Filed 6–19–01; 8:45 am]

BILLING CODE 7590–01–P

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2000–NM–176–AD, Amendment

39–12273; AD 2001–12–17]

RIN 2120–AA64

Airworthiness Directives; Raytheon

Model Hawker 800XP Series Airplanes

AGENCY: Federal Aviation

Administration, DOT.

ACTION: Final rule.

SUMMARY: This amendment adopts a

new airworthiness directive (AD),

applicable to certain Raytheon Model

Hawker 800XP series airplanes, that

requires an inspection to confirm the

installation of rivets at fuselage stations

251.975, 262.35, 272.725, and 283.10,

and installation of new rivets, if

necessary. The actions specified by this

AD are intended to detect and correct

fatigue cracking of the fuselage skin, and

consequent loss of cabin pressurization.

This action is intended to address the

identified unsafe condition.

DATES: Effective July 25, 2001.

The incorporation by reference of

certain publications listed in the

regulations is approved by the Director

of the Federal Register as of July 25,

2001.

ADDRESSES: The service information

referenced in this AD may be obtained

from Raytheon Aircraft Company,

Department 62, P.O. Box 85, Wichita,

Kansas 67201–0085. This information

may be examined at the Federal

Aviation Administration (FAA),

Transport Airplane Directorate, Rules

Docket, 1601 Lind Avenue, SW.,

Renton, Washington; or at the FAA,

Wichita Aircraft Certification Office,

1801 Airport Road, Room 100, Wichita,

Kansas; or at the Office of the Federal

Register, 800 North Capitol Street, NW.,

suite 700, Washington, DC.

FOR FURTHER INFORMATION CONTACT:

David Ostrodka, Aerospace Engineer,

Airframe Branch, ACE–118W, FAA,

Wichita Aircraft Certification Office,

1801 Airport Road, Room 100, Wichita,

Kansas 67209; telephone (316) 946–

4129; fax (316) 946–4407.

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 Raytheon

Model Hawker 800XP series airplanes

was published in the Federal Register

on March 29, 2001 (66 FR 17103). That

action proposed to require an inspection

to confirm the installation of rivets at

fuselage stations 251.975, 262.35,

272.725, and 283.10, and installation of

new rivets, if necessary.

Comments

Interested persons have been afforded

an opportunity to participate in the

making of this amendment. No

comments were submitted in response

to the proposal or the FAA’s

determination of the cost to the public.

33014 Federal Register / Vol. 66, No. 119 / Wednesday, June 20, 2001 / Rules and Regulations

Conclusion

The FAA has determined that air

safety and the public interest require the

adoption of the rule as proposed.

Cost Impact

There are approximately 124 Model

Hawker 800XP series airplanes of the

affected design in the worldwide fleet.

The FAA estimates that 87 airplanes of

U.S. registry will be affected by this AD,

that it will take approximately 2 work

hours per airplane to accomplish the

required actions, and that the average

labor rate is $60 per work hour. Based

on these figures, the cost impact of the

AD on U.S. operators is estimated to be

$10,440, or $120 per airplane.

The cost impact figure discussed

above is 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.

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.

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:

2001–12–17 Raytheon Aircraft Company:

Amendment 39–12273. Docket 2000–

NM–176–AD.

Applicability: Model Hawker 800XP series

airplanes, certificated in any category, having

the following serial numbers 258266, and

258277 through 258399 inclusive.

Note 1: This AD applies to each airplane

identified in the preceding applicability

provision, regardless of whether it has been

modified, altered, or repaired in the area

subject to the requirements of this AD. For

airplanes that have been modified, altered, or

repaired so that the performance of the

requirements of this AD is affected, the

owner/operator must request approval for an

alternative method of compliance in

accordance with paragraph (b) of this AD.

The request should include an assessment of

the effect of the modification, alteration, or

repair on the unsafe condition addressed by

this AD; and, if the unsafe condition has not

been eliminated, the request should include

specific proposed actions to address it.

Compliance: Required as indicated, unless

accomplished previously.

To detect and correct fatigue cracking of

the fuselage skin, and consequent loss of

cabin pressurization, accomplish the

following:

Inspection and Corrective Action

(a) Within 600 flight hours or 12 months

after the effective date of this AD, whichever

occurs first: Do a one-time detailed visual

inspection to confirm the installation of

rivets at fuselage stations 251.975, 262.35,

272.725, and 283.10. Do the inspection per

the Accomplishment Instructions of

Raytheon Service Bulletin 51–3336, Revision

1, dated January 2001. If any rivet is missing,

before further flight, install a new rivet per

the Accomplishment Instructions of the

service bulletin.

Note 2: Accomplishment of the actions in

accordance with Raytheon Service Bulletin

51–3336, dated May 2000, is acceptable for

compliance with the requirements of

paragraph (a) of this AD.

Alternative Methods of Compliance

(b) An alternative method of compliance or

adjustment of the compliance time that

provides an acceptable level of safety may be

used if approved by the Manager, Wichita

Aircraft Certification Office (ACO), FAA.

Operators shall submit their requests through

an appropriate FAA Principal Maintenance

Inspector, who may add comments and then

send it to the Manager, Wichita ACO.

Note 3: Information concerning the

existence of approved alternative methods of

compliance with this AD, if any, may be

obtained from the Wichita ACO.

Special Flight Permits

(c) Special flight permits may be issued in

accordance with sections 21.197 and 21.199

of the Federal Aviation Regulations (14 CFR

21.197 and 21.199) to operate the airplane to

a location where the requirements of this AD

can be accomplished.

Incorporation by Reference

(d) The actions shall be done in accordance

with Raytheon Service Bulletin 51–3336,

Revision 1, dated January 2001. 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. Copies may be obtained from

Raytheon Aircraft Company, Department 62,

P.O. Box 85, Wichita, Kansas 67201–0085.

Copies may be inspected at the FAA,

Transport Airplane Directorate, 1601 Lind

Avenue, SW., Renton, Washington; or at the

FAA, Wichita Aircraft Certification Office,

1801 Airport Road, Room 100, Wichita,

Kansas; or at the Office of the Federal

Register, 800 North Capitol Street, NW., suite

700, Washington, DC.

Effective Date

(e) This amendment becomes effective on

July 25, 2001.

Issued in Renton, Washington, on June 11,

2001.

Donald L. Riggin,

Acting Manager, Transport Airplane

Directorate, Aircraft Certification Service.

[FR Doc. 01–15211 Filed 6–19–01; 8:45 am]

BILLING CODE 4910–13–P

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2000–NM–262–AD; Amendment

39–12274; AD 2001–12–18]

RIN 2120–AA64

Airworthiness Directives;

Construcciones Aeronauticas, S.A.

(CASA), Model CN–235 Series

Airplanes

AGENCY: Federal Aviation

Administration, DOT.

ACTION: Final rule.

SUMMARY: This amendment adopts a

new airworthiness directive (AD),

applicable to certain CASA Model CN–