Federal Register / Vol. 65, No. 213 / Thursday, November 2, 2000 / Rules and Regulations 65731

third and fourth lines, ‘‘(14 CFR part 39)

to include an airworthiness directive

(AD)’’ is corrected to read ‘‘(14 CFR part

39) by superseding (AD) 99–08–14,

Amendment 39–11120 (64 FR 17949),

dated April 13, 1999’’.

§ 39.13 [Corrected]

3. On page 63543, in the second

column, in the AD heading, in the

second line, ‘‘39–11941. Docket No. 98–

ANE–61–AD.’’ is corrected to read ‘‘39–

11941 Docket No. 98–ANE–61–AD.

Supersedes AD 99–08–14, Amendment

39–11120.’’.

Issued in Burlington, MA, on October 25,

2000.

David A. Downey,

Assistant Manager, Engine and Propeller

Directorate, Aircraft Certification Service.

[FR Doc. 00–27945 Filed 11–1–00; 8:45 am]

BILLING CODE 4910–13–P

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 98–ANE–48–AD; Amendment

39–11940; AD 2000–21–08]

RIN 2120–AA64

Airworthiness Directives; Pratt &

Whitney JT8D Series Turbofan

Engines; Correction

AGENCY: Federal Aviation

Administration, DOT.

ACTION: Final rule; correction.

SUMMARY: This document makes a

correction to Airworthiness Directive

(AD) 2000–21–08 applicable to Pratt &

Whitney JT8D series turbofan engines

that was published in the Federal

Register on October 24, 2000 (65 FR

63537). The statement identifying AD

2000–21–08 as superseding AD 99–12–

03, Amendment 39–11187 (64 FR

30379, dated June 8, 1999), was

inadvertently omitted from the AD. This

document corrects that statement. In all

other respects, the original document

remains the same.

EFFECTIVE DATE: April 23, 2001.

FOR FURTHER INFORMATION CONTACT:

Christopher Spinney, Aerospace

Engineer, Engine Certification Office,

FAA, Engine and Propeller Directorate,

12 New England Executive Park,

Burlington, MA 01803; telephone 781–

238–7175, fax 781–238–7199.

SUPPLEMENTARY INFORMATION: A final

rule airworthiness directive (FR Doc.

00–26971) applicable to Pratt & Whitney

JT8D series turbofan engines was

published in the Federal Register on

October 24, 2000 (65 FR 63537). The

following correction is needed:

§ 39.13 [Corrected]

On page 63539, in the first column,

the AD heading is corrected to read ‘‘AD

2000–21–08 Pratt & Whitney:

Amendment 39–11940. Docket 98–

ANE–48–AD. Supersedes AD 99–12–03,

Amendment 39–11187.’’.

Issued in Burlington, MA, on October 26,

2000.

David A. Downey,

Assistant Manager, Engine and Propeller

Directorate, Aircraft Certification Service.

[FR Doc. 00–28091 Filed 11–1–00; 8:45 am]

BILLING CODE 4910–13–P

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 98–ANE–43–AD; Amendment

39–11939; AD 2000–21–07]

RIN 2120–AA64

Airworthiness Directives; Pratt &

Whitney JT8D–200 Series Turbofan

Engines; Correction

AGENCY: Federal Aviation

Administration, DOT.

ACTION: Final rule; correction.

SUMMARY: This document makes a

correction to Airworthiness Directive

(AD) 2000–21–07 applicable to Pratt &

Whitney JT8D–200 series turbofan

engines that was published in the

Federal Register on October 24, 2000

(65 FR 63540). The statement

identifying AD 2000–21–07 as

superseding AD 99–12–04, Amendment

39–11188 (64 FR 30382, dated June 8,

1999), was inadvertently omitted from

the AD. This document corrects that

statement. In all other respects, the

original document remains the same.

EFFECTIVE DATE: April 23, 2001.

FOR FURTHER INFORMATION CONTACT:

Christopher Spinney, Aerospace

Engineer, Engine Certification Office,

FAA, Engine and Propeller Directorate,

12 New England Executive Park,

Burlington, MA 01803; telephone 781–

238–7175, fax 781–238–7199.

SUPPLEMENTARY INFORMATION: A final

rule airworthiness directive (FR Doc.

00–26970) applicable to Pratt & Whitney

JT8D–200 series turbofan engines was

published in the Federal Register on

October 24, 2000 (65 FR 63540). The

following correction is needed:

§ 39.13 [Corrected]

On page 63541, in the first column,

the AD heading is corrected to read ‘‘AD

2000–21–07 Pratt & Whitney:

Amendment 39–11939. Docket 98–

ANE–43–AD. Supersedes AD 99–12–04,

Amendment 39–11188.’’

Issued in Burlington, MA, on October 26,

2000.

David A. Downey,

Assistant Manager, Engine and Propeller

Directorate, Aircraft Certification Service.

[FR Doc. 00–28090 Filed 11–1–00; 8:45 am]

BILLING CODE 4910–13–P

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 71

[Airspace Docket No. 00–AWP–8]

Modification of Class E Airspace;

Willits, CA

AGENCY: Federal Aviation

Administration (FAA), DOT.

ACTION: Final rule.

SUMMARY: This action modifies the Class

E airspace area at Willits, CA. A revision

to the Area Navigation (RNAV) Standard

Instrument Approach Procedure (SIAP)

to Runway (RWY) 16 and RWY 34 at

Ells Field-Willits Municipal Airport has

made action necessary. Additional

controlled airspace extending upward

from 1200 feet above the surface of the

earth is needed to contain aircraft

executing the RNAV RWY 16 and RWY

34 SIAP with a Terminal Arrival Area

design to Ells Field-Willits Municipal

Airport. The intended effects of this

action is to provide adequate controlled

airspace for Instrument Flight Rules

operations at Ells Field-Willits

Municipal Airport, Willits, CA.

EFFECTIVE DATE: 0901 UTC January 25,

2001.

FOR FURTHER INFORMATION CONTACT: Jeri

Carson, Airspace Specialist, Airspace

Branch, AWP–520, Air Traffic Division,

Western-Pacific Region, Federal

Aviation Administration, 15000

Aviation Boulevard, Lawndale,

California 90261, telephone (310) 725–

6611.

SUPPLEMENTARY INFORMATION:

History

On August 23, 2000, the FAA

proposed to amend 14 CFR part 71 by

modifying the Class E airspace area at

Willits, CA (65 FR 38227). Additional

controlled airspace extending upward

from 1200 feet above the surface is

needed to contain aircraft executing the