Federal Register / Vol. 67, No. 144 / Friday, July 26, 2002 / Rules and Regulations 48753

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. 98–ANE–43–AD; Amendment 

39–12797; AD 2002–13–09] 

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 

corrections to Airworthiness Directive 

(AD) 2002–13–09 applicable to Pratt & 

Whitney JT8D–200 engines that was 

published in the Federal Register on 

July 3, 2002 (67 FR 44527). In the 

regulatory information, Table part B., 

Parts Requiring Inspection, one item 

under Description and one item under 

Engine Manual are incorrect. This 

document corrects these items. In all 

other respects, the original document 

remains the same.

EFFECTIVE DATE: July 3, 2002.

FOR FURTHER INFORMATION CONTACT:

Christopher Spinney, Aerospace 

Engineer, Engine Certification Office, 

FAA, Engine and Propeller Directorate, 

12 New England Executive Park, 

Burlington, MA; telephone (781) 238–

7175; fax (781) 238–7199.

SUPPLEMENTARY INFORMATION: A final 

rule airworthiness directive FR Doc, 02–

16535 applicable to Pratt & Whitney 

JT8D–200 series turbofan engines, was 

published in the Federal Register on 

July 3, 2002 (67 FR 44527). The 

following correction is needed:

§ 39.13 [Corrected] 

On page 44528, in the third column, 

in the regulatory information, Table part 

B., Parts Requiring Inspection, first 

column, the last Description ‘‘Disk, 4th 

Stage Turbine—’’ is corrected to read 

‘‘Disk, 4th Stage Turbine—All P/N’s’. 

On page 44528, in the third column, 

in the regulatory information, Table part 

B., Parts Requiring Inspection, second 

column, the sixth Engine Manual 

Section ‘‘2–53–16’’ is corrected to read 

‘‘72–53–16’.

Issued in Burlington, MA, on July 22, 2002. 

Peter A. White, 

Acting Manager, Engine and Propeller 

Directorate, Aircraft Certification Service.

[FR Doc. 02–19034 Filed 7–25–02; 8:45 am] 

BILLING CODE 4910–13–U

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. 2000–NE–19–AD; Amendment 

39–12792; AD 2002–13–04] 

RIN 2120–AA64 

Airworthiness Directives; Teledyne 

Continental Motors; Correction

AGENCY: Federal Aviation 

Administration, DOT.

ACTION: Final rule; correction.

SUMMARY: This document makes a 

correction to Airworthiness Directive 

(AD) 2000–NE–19 applicable to 

Teledyne Continental Motors O–300, 

IO–360, TSIO–360, and LTSIO–520–AE 

series reciprocating engines that was 

published in the Federal Register on 

June 27, 2002 (67 FR 43230). The 

superseded AD number was 

inadvertently omitted from the 

regulatory information, paragraph 2. of 

§ 39.13 [Amended]. This document 

corrects that omission. In all other 

respects, the original document remains 

the same.

EFFECTIVE DATE: July 12, 2002.

FOR FURTHER INFORMATION CONTACT:

Michael Downs, Aerospace Engineer, 

Chicago Aircraft Certification Office, 

FAA, 2300 East Devon Avenue, Des 

Plaines, IL 60018; telephone (847) 294–

7870, fax (847) 294–7834.

SUPPLEMENTARY INFORMATION: A final 

rule; request for comments 

airworthiness directive FR Doc. 02–

16174 applicable to Teledyne 

Continental Motors O–300, IO–360, 

TSIO–360, and LTSIO–520–AE series 

reciprocating engines, was published in 

the Federal Register on June 27, 2002 

(67 FR 43230). The following correction 

is needed:

§ 39.13 [Corrected] 

On page 43231, in the second column, 

§ 39.13 Amended, paragraph 2. in the 

seventh line, ‘‘2000–NE–19–AD.’’ is 

corrected to read ‘‘2000–NE–19–AD. 

Supersedes AD 2000–11–51’’.

Issued in Burlington, MA, on July 22, 2002. 

Peter A. White, 

Acting Manager, Engine and Propeller 

Directorate, Aircraft Certification Service.

[FR Doc. 02–19035 Filed 7–25–02; 8:45 am] 

BILLING CODE 4910–13–U

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration 

14 CFR Part 71

[Airspace Docket No. 02–ACE–4] 

Amendment to Class E Airspace; 

Norton, KS

AGENCY: Federal Aviation 

Administration, DOT.

ACTION: Direct final rule; confirmation of 

effective date. 

SUMMARY: This document confirms the 

effective date of a direct final rule which 

revises Class E airspace at Norton, KS.

EFFECTIVE DATE: 0901 UTC, October 3, 

2002.

FOR FURTHER INFORMATION CONTACT:

Kathy Randolph, Air Traffic Division, 

Airspace Branch, ACE–520C, DOT 

Regional Headquarters Building, Federal 

aviation Administration, 901 Locust, 

Kansas City, MO 64106; telephone: 

(816) 329–2525.

SUPPLEMENTARY INFORMATION: The FAA 

published this direct final rule with a 

request for comments in the Federal 

Register on May 20, 2002 (67 FR 35426). 

The FAA uses the direct final 

rulemaking procedure for a noncontroversial rule where the FAA 

believes that there will be no adverse 

public comment. This direct final rule 

advised the public that no adverse 

comments were anticipated, and that 

unless a written adverse comment, or a 

written notice of intent to submit such 

an adverse comment, were received 

within the comment period, the 

regulation would become effective on 

October 3, 2002. No adverse comments 

were received, and thus this notice 

confirms that this direct final rule will 

become effective on that date.

Issued in Kansas City, MO on July 17, 

2002. 

Herman J. Lyons, Jr. 

Manager, Air Traffic Division, Central Region.

[FR Doc. 02–19000 Filed 7–25–02; 8:45 am] 

BILLING CODE 4910–13–M