44888 Federal Register / Vol. 62, No. 164 / Monday, August 25, 1997 / Rules and Regulations

21.197 and 21.199) to operate the aircraft to

a location where the requirements of this AD

can be accomplished.

(d) The actions required by this AD shall

be performed in accordance with the

following PWC SIL:

Document No. Pages Date

PW100–003 .... 1 June 18, 1997

Total pages: 1.

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 Pratt & Whitney Canada, 1000 MarieVictorin, Longueuil, Quebec, Canada J4G1A1;

telephone (514) 647–2866, fax (514) 647–

2888. Copies may be inspected at the FAA,

New England Region, Office of the Assistant

Chief Counsel, 12 New England Executive

Park, Burlington, MA; or at the Office of the

Federal Register, 800 North Capitol Street,

NW., suite 700, Washington, DC.

(e) This amendment becomes effective on

September 9, 1997.

Issued in Burlington, Massachusetts, on

August 12, 1997.

Jay J. Pardee,

Manager, Engine and Propeller Directorate,

Aircraft Certification Service.

[FR Doc. 97–22308 Filed 8–22–97; 8:45 am]

BILLING CODE 4910–13–U

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 95–NM–228–AD; Amendment

39–10097; AD 97–16–06]

RIN 2120–AA64

Airworthiness Directives; Airbus Model

A300–600 Series Airplanes; Correction

AGENCY: Federal Aviation

Administration, DOT.

ACTION: Final rule; correction.

SUMMARY: This document corrects the

compliance time information in

airworthiness directive (AD) 97–16–06

that was published in the Federal

Register on August 1, 1997 (62 FR

41257). A portion of the specified

compliance times was inadvertently

omitted in the AD. This AD is

applicable to all Airbus Model A300–

600 series airplanes, and requires an

inspection to detect cracks of certain

attachment holes; and installation of a

new fastener and follow-on inspections

or repair, if necessary.

DATES: Effective September 5, 1997.

The incorporation by reference of

certain publications listed in the

regulations was previously approved by

the Director of the Federal Register as of

September 5, 1997 (62 FR 41257, August

1, 1997).

FOR FURTHER INFORMATION CONTACT: Tim

Backman, Aerospace Engineer,

Standardization Branch, ANM–113,

FAA, Transport Airplane Directorate,

1601 Lind Avenue, SW., Renton,

Washington 98055–4056; telephone

(425) 227–2797; fax (425) 227–1149.

SUPPLEMENTARY INFORMATION:

Airworthiness Directive (AD) 97–16–06,

amendment 39–10097, applicable to all

Airbus Model A300–600 series

airplanes, was published in the Federal

Register on August 1, 1997 (62 FR

41257). That AD requires an inspection

to detect cracks of certain attachment

holes; and installation of a new fastener

and follow-on inspections or repair, if

necessary.

As published, the phrase ‘‘whichever

occurs later’’ after the compliance times

specified in paragraphs (a)(1) and (a)(2)

of the AD was inadvertently omitted.

Since no other part of the regulatory

information has been changed, the final

rule is not being republished.

The effective date of the AD remains

September 5, 1997.

In rule FR Doc. 97–20131 published

on August 1, 1997 (62 FR 41257), make

the following corrections:

§39.13 [Corrected]

1. On page 41258, in the third

column, paragraph (a)(1) of AD 97–16–

06 is corrected to read as follows:

* * * * *

(a) * * *

(1) For airplanes on which Airbus

Modification 10454 (reference Airbus

Service Bulletin A300–57–6050) has not

been installed: Inspect prior to the

accumulation of 13,800 total landings,

or within 750 landings after the effective

date of this AD, whichever occurs later.

* * * * *

2. On page 41258, in the third

column, paragraph (a)(2) of AD 97–16–

06 is corrected to read as follows:

* * * * *

(a) * * *

(2) For airplanes on which Airbus

Modification 10454 (reference Airbus

Service Bulletin A300–57–6050) or

Airbus Modification 10155 has been

installed: Inspect prior to the

accumulation of 18,700 total landings,

or within 750 landings after the effective

date of this AD, whichever occurs later.

* * * * *

Issued in Renton, Washington, on August

19, 1997.

S. R. Miller,

Acting Manager, Transport Airplane

Directorate, Aircraft Certification Service.

[FR Doc. 97–22488 Filed 8–22–97; 8:45 am]

BILLING CODE 4910–13–U

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 71

[Airspace Docket No. 97–AGL–23]

Modification of Class E Airspace;

Grafton, ND

AGENCY: Federal Aviation

Administration (FAA), DOT.

ACTION: Final rule.

SUMMARY: This action modifies Class E

airspace at Grafton, ND. A Global

Positioning System (GPS) Standard

Instrument Approach Procedure (SIAP)

to Runway 17 and Amendment 1 to the

GPS SIAP to Runway 35 have been

developed for Grafton Municipal

Airport. Controlled airspace extending

upward from 700 to 1200 feet above

ground level (AGL) is needed to contain

aircraft executing the approaches. This

proposal increases the radius, and adds

an extension to the north and an

extension to the south, of the existing

Class E airspace. The intended effect of

this action is to provide segregation of

aircraft using instrument approach

procedures in instrument conditions

from other aircraft operating in visual

weather conditions.

EFFECTIVE DATE: 0901 UTC, November 6,

1997.

FOR FURTHER INFORMATION CONTACT:

Michelle M. Behm, Air Traffic Division,

Airspace Branch, AGL–520, Federal

Aviation Administration, 2300 East

Devon Avenue, Des Plaines, Illinois

60018, telephone (847) 294–7568.

SUPPLEMENTARY INFORMATION:

History

On Wednesday, May 28, 1997, the

FAA proposed to amend part 71 of the

Federal Aviation Regulations (14 CFR

part 71) by modifying the Class E

airspace at Grafton, ND (62 FR 28814).

The proposal would add controlled

airspace extending upward from 700 to

1200 feet AGL to contain Instrument

Flight Rules (IFR) operations in

controlled airspace during portions of

the terminal operation and while

transiting between the enroute and

terminal environments.

Interested parties were invited to

participate in this rulemaking

proceeding by submitting written

comments on the proposal to the FAA.

No comments objecting to the proposal

were received. Class E airspace

designations for airspace areas

extending upward from 700 feet or more

above the surface of the earth are

published in paragraph 6005 of FAA