Federal Register / Vol. 62, No. 205 / Thursday, October 23, 1997 / Rules and Regulations 55157

‘‘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 copy of the final

evaluation prepared for this action is

contained in the Rules Docket. A copy

of it may be obtained by contacting 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

removing Airworthiness Directive (AD)

84–23–06, Amendment 39–4942, (49 FR

43621, October 31, 1984), and adding a

new AD to read as follows:

84–23–06 R1. Pilatus Britten-Norman LTD.:

Amendment 39–10172; Docket No. 84–

CE–18–AD; Revises AD 84–23–06,

Amendment 39–4942.

Applicability: BN–2A MK. 111 Series

Airplanes (all serial numbers), certificated in

any category.

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 (d) 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.

Note 2: The paragraph structure of this AD

is as follows:

Level 1: (a), (b), (c), etc.

Level 2: (1), (2), (3), etc.

Level 3: (i), (ii), (iii), etc.

Level 2 and Level 3 structures are

designations of the Level 1 paragraph they

immediately follow.

Compliance: Required initially upon the

accumulation of 500 hours time-in-service

(TIS) or within the next 50 hours TIS after

the effective date of this AD, whichever

occurs later, unless already accomplished

(compliance with AD 84–23–06), and

thereafter at intervals not to exceed 500 hours

TIS.

To prevent failure of the upper mounting

brackets on both wing mounted engines,

which could possibly cause structural failure

of the airplane, accomplish the following:

(a) Visually inspect the following areas in

accordance with paragraphs 1 through 6 of

the ‘‘Inspection’’ section of the Pilatus

Britten-Norman (Pilatus) Service Bulletin

(SB) No. BN–2/SB.61, Issue 5, dated

December 9, 1981:

(1) The upper engine to wing mounting

brackets for:

(i) Minimum lug bolt hole-to-edge distance,

elongation of the bolt holes, distortion,

delamination, cracks, flaking, and corrosion;

(ii) The bolts for correct bearing length; and

(iii) Loose and fretted bushings.

(2) Prior to further flight, correct defects in

accordance with the following:

(i) If the lug bolt hole-to-edge distance is

less than the specified minimum (0.2625-

inches), correct in accordance with paragraph

3 of the ‘‘Rectification/Modification’’ section

of Pilatus SB No. BN–2/SB.61, Issue 5, dated

December 9, 1981;

(ii) If the bolt holes are elongated, or if any

bushings are loose or fretted, modify and

correct in accordance with paragraph 4 of the

‘‘Rectification/Modification’’ section of

Pilatus SB No. BN–2/SB.61, Issue 5, dated

December 9, 1981;

(iii) If any mounting bracket is cracked,

modify both brackets on the same engine

installation (left side engine or right side

engine) concurrently (even if only one

bracket is defective) in accordance with

paragraph 1 of the ‘‘Rectification/

Modification’’ section of Pilatus SB No. BN–

2/SB.61, Issue 5, dated December 9, 1981;

(iv) If any lug is distorted or delaminated,

replace the deficient part in accordance with

paragraphs 1 and 2 of the ‘‘Rectification/

Modification’’ section of Pilatus SB No. BN–

2/SB.61, Issue 5, dated December 9, 1981;

(v) If any inspected part is corroded or

flaking, replace the part in accordance

paragraph 1 with the ‘‘Rectification/

Modification’’ section of Pilatus SB No. BN–

2/SB.61, Issue 5, dated December 9, 1981;

and

(vi) If any of the bolts are of incorrect

length or damaged, replace with new units of

the correct length in accordance with

paragraphs 1 and 2 of the ‘‘Rectification/

Modification’’ section of Pilatus SB No. BN–

2/SB.61, Issue 5, dated December 9, 1981.

(b) The intervals between the repetitive

inspections required by this AD may be

adjusted up to 10 percent of the specified

interval to allow for accomplishing these

inspections concurrent with the other

scheduled maintenance of the airplane.

(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.

(d) An alternative method of compliance or

adjustment of the initial or repetitive

compliance times that provides an equivalent

level of safety may be approved by the

Manager, Small Airplane Directorate, Aircraft

Certification Service, FAA, 1201 Walnut,

suite 900, Kansas City, Missouri 64106. The

request shall be forwarded through an

appropriate FAA Maintenance Inspector,

who may add comments and then send it to

the Manager, Small Airplane Directorate.

Note 3: Information concerning the

existence of approved alternative methods of

compliance with this AD, if any, may be

obtained from the Small Airplane

Directorate.

(e) The inspections, modifications, and

replacements, required by this AD shall be

done in accordance with Pilatus BrittenNorman Service Bulletin No. BN–2/SB.61,

Issue: 5, Date: December 9, 1981. 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 Pilatus

Britten-Norman Limited, Bembridge, Isle of

Wight, United Kingdom PO35 5PR. Copies

may be inspected at the FAA, Central Region,

Office of the Regional Counsel, Room 1558,

601 E. 12th Street, Kansas City, Missouri, or

at the Office of the Federal Register, 800

North Capitol Street, NW., suite 700,

Washington, DC.

(f) This amendment (39–10172) becomes

effective on November 24, 1997.

Issued in Kansas City, Missouri, on

October 16, 1997.

Mary Ellen A. Schutt,

Acting Manger, Small Airplane Directorate,

Aircraft Certification Service.

[FR Doc. 97–27931 Filed 10–22–97; 8:45 am]

BILLING CODE 4910–13–P

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 71

[Airspace Docket No. 97–AWP–23]

Amendment of Class E Airspace;

Flagstaff, AZ

AGENCY: Federal Aviation

Administration (FAA), DOT.

ACTION: Final rule.

SUMMARY: This action amends the Class

E airspace areas at Flagstaff, AZ. The

development of a Global Positioning

System (GPS) Standard Instrument

Approach Procedure (SIAP) to Runway

(RWY) 3 has made this action necessary.

The intended effect of this action is to

provide adequate additional controlled

airspace extending upward from 700

feet or more above the surface for

Instrument Flight Rules (IFR) operations

at Flagstaff Pulliam Airport, Flagstaff,

AZ.
55158 Federal Register / Vol. 62, No. 205 / Thursday, October 23, 1997 / Rules and Regulations

EFFECTIVE DATE: 0901 UTC January 01,

1998.

FOR FURTHER INFORMATION CONTACT:

Larry Tonish, Airspace Specialist,

Airspace Branch, AWP–520, Air Traffic

Division, Western-Pacific Region,

Federal Aviation Administration, 15000

Aviation Boulevard, Lawndale,

California, 90261, telephone (310) 725–

6531.

SUPPLEMENTARY INFORMATION:

History

On August 11, 1997, the FAA

proposed to amend part 71 of the

Federal Aviation Regulations (14 CFR

part 71) by amending the Class E

airspace areas at Flagstaff, AZ (62 FR

42955). The development of a GPS SIAP

at Flagstaff Pulliam Airport has made

this action necessary. The intended

effect of this action is to provide

additional controlled airspace extending

700 feet or more above the surface for

aircraft executing the GPS RWY 3 SIAP

to Flagstaff Pulliam Airport, Flagstaff,

AZ.

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 are published in

paragraphs 6004 and 6005 of FAA Order

7400.9E, dated September 10, 1997, and

effective September 16, 1997, which is

incorporated by reference in 14 CFR

71.1. Class E airspace designations

listed in this document will be

published subsequently in the Order.

The Rule

This amendment to part 71 of the

Federal Aviation Regulations (14 CFR

part 71) amends the Class E airspace

areas at Flagstaff, AZ. The development

of a GPS SIAP at Flagstaff Pulliam

Airport has made this action necessary.

The intended effect of this action is to

provide additional controlled airspace

extending 700 feet or more above the

surface for aircraft executing the GPS

RWY 3 SIAP at Flagstaff Pulliam

Airport, Flagstaff, AZ.

The FAA has determined that this

regulation only involves an established

body of technical regulations for which

frequent and routine amendments are

necessary to keep them operationally

current. Therefore, this regulation—(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)

does not warrant preparation of a

Regulatory Evaluation as the anticipated

impact is so minimal. Since this is a

routine matter that will only affect air

traffic procedures and air navigation, it

is certified that this rule will not have

a significant economic impact on a

substantial number of small entities

under the criteria of the Regulatory

Flexibility Act.

List of Subjects in 14 CFR Part 71

Airspace, Incorporation by reference,

Navigation (air).

Adoption of the Amendment

In consideration of the foregoing, the

Federal Aviation Administration

amends 14 CFR part 71 as follows:

PART 71—[AMENDED]

1. The authority citation for 14 CFR

part 71 continues to read as follows:

Authority: 49 U.S.C. 106(g), 40103, 40113,

40120; E.O. 10854, 24 FR 9565, 3 CFR, 1959–

1963 Comp., p. 389.

§ 71.1 [Amended]

2. The incorporation by reference in

14 CFR 71.1 of the Federal Aviation

Administration Order 7400.9E, Airspace

Designations and Reporting Points,

dated September 10, 1997, and effective

September 16, 1997, is amended as

follows:

Paragraph 6004 Class E airspace areas

designated as an extension to a Class D or

Class E surface area.

* * * * *

AWP AZ E4 Flagstaff, AZ [Revised]

Flagstaff Pulliam Airport, AZ.

(Lat. 35°08′18′′ N, long. 111°40′16′′ W)

Flagstaff VOR/DME

(Lat. 35°08′50′′ N, long. 111°40′27′′ W)

That airspace extending upward from the

surface beginning where a line 1.8 miles

northwest of and parallel to the Flagstaff

VOR/DME 057° radial intercepts the 6.1-mile

radius of the Flagstaff Pulliam Airport,

thence clockwise to intercept a line 1.8 miles

northwest of and parallel to the Flagstaff

VOR/DME 218° radial, thence

northeastbound on a line 1.8 miles west of

and parallel to the Flagstaff VOR/DME 218°

radial to intercept the 3-mile arc of the

Flagstaff Pulliam Airport clockwise to

intercept the line 1.8 miles northwest of and

parallel to the Flagstaff VOR/DME 057° radial

and thence to the point of beginning and

within 1.8 miles each side of the Flagstaff

VOR/DME 127° radial, extending from the

6.1-mile radius to 8.6 miles southeast of the

VOR/DME. This Class E airspace area is

effective during the specific dates and times

established in advance by a Notice to

Airmen. The effective date and time will

thereafter be continuously published in the

Airport/Facility Directory.

* * * * *

Paragraph 6005 Class E airspace areas

extending upward from 700 feet or more

above the surface of the earth.

* * * * *

AWP AZ E5 Flagstaff, AZ [Revised]

Flagstaff Pulliam Airport, AZ

(Lat. 35°08′18′′ N, long. 111°40′16′′ W)

Flagstaff VOR/DME

(Lat. 35°08′50′′ N, long. 111°40′27′′ W)

That airspace extending upward from 700

feet above the surface within a 3.6-mile

radius of the Flagstaff Pulliam Airport and

within a 10-mile radius of the Flagstaff VOR

beginning at a line 1.8-miles northwest of

parallel to the Flagstaff VOR 043° radial

extending clockwise to a point beginning at

lat. 34°59′20′′ N, long. 111°36′35′′ W; to lat.

34°44′00′′ N, long. 111°50′00′′ W; to lat.

34°45′00′′ N, long. 112°01′00′′ W; to lat.

34°54′00′′ N, long. 112°05′00′′ W; to lat.

35°08′00′′ N, long. 111°52′00′′ W, thence

eastbound along the Flagstaff VOR 265°

radial to intercept the 3.6-mile radius of the

Flagstaff Pulliam Airport, thence clockwise

to the point of beginning. That airspace

extending upward from 1,200 feet above the

surface within 8.3 miles each side of the

Flagstaff VOR 127° and 307° radials,

extending from 7 miles northwest to 16.5

miles southeast of the Flagstaff VOR and that

airspace bounded by a line beginning at lat.

35°13′32′′ N, long. 111°04′31′′ W; to lat.

35°17′17′′ N, long. 111°02′35′′ W; to lat.

35°22′00′′ N, long. 111°16′43′′ W; to lat.

35°24′00′′ N, long. 111°26′16′′ W; to lat.

35°18′00′′ N, long. 111°25′33′′ W, thence

clockwise via a 10-mile radius of the Flagstaff

VOR to lat. 35°16′34′′ N, long. 111°32′42′′ W;

to lat. 35°19′58′′ N, long. 111°24′10′′ W,

thence to the point of beginning and that

airspace bounded by a line beginning at lat.

35°02′56′′ N, long. 111°20′38′′ W; to lat.

35°02′00′′ N, long. 111°15′00′′ W; to lat.

35°00′56′′ N, long. 111°22′28′′ W, thence to

the point of beginning, excluding the Sedona,

AZ, Class E airspace area.

* * * * *

Issued in Los Angeles, California, on

October 16, 1997.

Thomas L. Parks,

Acting Manager, Air Traffic Division WesternPacific Region.

[FR Doc. 97–28103 Filed 10–22–97; 8:45 am]

BILLING CODE 4910–13–M

DEPARTMENT OF HEALTH AND

HUMAN SERVICES

Food and Drug Administration

21 CFR Parts 510 and 520

Animal Drugs, Feeds, and Related

Products; Selegiline Hydrochloride

Tablets; Correction

AGENCY: Food and Drug Administration,

HHS.

ACTION: Final rule; correction.

SUMMARY: The Food and Drug

Administration (FDA) is correcting a