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