23200 Federal Register / Vol. 63, No. 81 /Tuesday, April 28, 1998 /Rules and Regulations

Common registered, par Greek

IONIAN & POPULAR BANK OF GREECE,

Common registered, par Greek

MICHANIKI, S.A.

Common registered, par Greek

MICHANIKI, S.A.

Preference registered, par Greek

MYTILINEOS HOLDINGS, S.A.

Common bearer, par Greek drachmas

N.I.B.I.D. (NATIONAL INVESTMENT BANK

Common registered, par Greek

N.I.B.I.D. (NATIONAL INVESTMENT BANK

Preference registered, par Greek

NATIONAL BANK OF GREECE

Common registered, par Greek

NATIONAL MORTGAGE BANK, S.A.

Common registered, par Greek

PAPASTRATOS CIGARETTE CO., S.A.

Common, par Greek drachmas 200

SILVER & BARYTE ORES MINING CO.,

Common bearer, par Greek drachmas

TITAN CEMENT CO.

Preference registered, par Greek

TITAN CEMENT CO.

Common registered, par Greek

Italy

BANCA DI ROMA, SPA

Ordinary shares, par 500 lira

Mexico

GRUPO MODELO S.A.

Class C, no par common

TELEVISION AZTECA S.A. (CPO)

No par common

TUBOS DE ACERO MEXICO S.A.

No par common

Norway

ODFJELL ASA

B Ordinary shares, par 10 Norwegian

ODFJELL ASA

A Ordinary shares, par 10 Norwegian

Portugal

BANCO ESPINTO SANTO E COMERCIAL

DE

Registered, par ESC 1,000

BANCO MELLO, S.A.

Registered, par ESC 1,000

BANCO TOTTA & ACORES, S.A.

Registered, par ESC 1,000

BCP (BANCO COMERCIAL PORTUGUES)

Registered, par ESC 1,000

BPI–SGPS (BANCO PORTUGEUES DE)

Registered, par ESC 1,000

BRISA (AUTO-ESTRADAS DE PORTUGAL)

Registered, par ESC 1,000

CIMPOR (CIMENTOS DE PORTUGAL)

Registered, par ESC 1,000

COMPANHIA DE SEGUROS

TRANQUILIDADE

Registered, par ESC 1,000

CREDITO PREDIAL PORTUGUESE, S.A.

Registered, par ESC 1,000

EDP (ELECTRICIDADE DE PORTUGAL),

Registered, par ESC 1,000

INPARSA (Industrial Participacoes)

Ordinary, par ESC 1,000

JERONIMO MARTINS

(ESTABELECIMENTOS)

Ordinary, par ESC 1,000

PORTUCEI INDUSTRIAL, S.A.

Registered, par ESC 1,000

PORTUGAL TELECOM, S.A.

Registered, par ESC 1,000

SEMAPA, S.A.

Ordinary, par ESC 1,000

SONAE INDUSTRIA, S.A.

Ordinary, par ESC 1,000

SONAE INVESTIMENTOS (SOCIETE)

Ordinary, par ESC 1,000

TELECEL COMMUNICACOES PESSOAIS

Ordinary, par ESC 1,000

Singapore

INCHCAPE MOTORS, LTD.

Ordinary shares, par S$.50

South Africa

GOLD FIELDS, LIMITED

Ordinary shares, par .01 South

United Kingdom

DEBENHAMS PLC

Ordinary shares, par 10 p

REUTERS GROUP PLC

Ordinary shares, par 25 p

By order of the Board of Governors of the

Federal Reserve System, acting by its Director

of the Division of Banking Supervision and

Regulation pursuant to delegated authority

(12 CFR 265.7(f)(10)), April 22, 1998.

William W. Wiles,

Secretary of the Board.

[FR Doc. 98–11221 Filed 4–27–98; 8:45 am]

BILLING CODE 6210–01–P

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 97–CE–132–AD; Amendment

39–10495; AD 98–09–14]

RIN 2120–AA64

Airworthiness Directives; Diamond

Aircraft Industries Models HK 36 TTS

and HK 36 TTC Sailplanes

AGENCY: Federal Aviation

Administration, DOT.

ACTION: Final rule.

SUMMARY: This amendment adopts a

new airworthiness directive (AD) that

applies to certain Diamond Aircraft

Industries (Diamond) Models HK 36

TTS and HK 36 TTC sailplanes. This AD

requires inspecting the engine

turbocharger oil-pressure line for the

correct banjo bolt. The correct banjo bolt

will have a valve seat, instead of a builtin orifice. If the banjo bolt does not have

a valve seat, then this action will require

replacing the banjo bolt with one that

has a valve seat, and repairing or

replacing the turbocharger. This AD is

the result of mandatory continuing

airworthiness information (MCAI)

issued by the airworthiness authority for

Austria. The actions specified by this

AD are intended to prevent possible loss

of engine power, which could result in

possible loss of control of the sailplane.

DATES: Effective June 14, 1998.

The incorporation by reference of

certain publications listed in the

regulations is approved by the Director

of the Federal Register as of June 14,

1998.

ADDRESSES: Service information that

applies to this AD may be obtained from

Diamond Aircraft Industries, G.m.b.H.,

N.A. Otto-Strabe 5, A–2700, Wiener

Neustadt, Austria. This information may

also be examined at the Federal

Aviation Administration (FAA), Central

Region, Office of the Regional Counsel,

Attention: Rules Docket No. 97–CE–

132–AD, Room 1558, 601 E. 12th Street,

Kansas City, Missouri 64106; or at the

Office of the Federal Register, 800 North

Capitol Street, NW, suite 700,

Washington, DC.

FOR FURTHER INFORMATION CONTACT: Mr.

Mike Kiesov, Aerospace Engineer, Small

Airplane Directorate, Aircraft

Certification Service, FAA, 1201

Walnut, suite 900, Kansas City, Missouri

64106; telephone: (816) 426–6934;

facsimile: (816) 426–2169.

SUPPLEMENTARY INFORMATION:

Events Leading to the Issuance of This

AD

A proposal to amend part 39 of the

Federal Aviation Regulations (14 CFR

part 39) to include an AD that would

apply to certain Diamond Models HK 36

TTS and HK 36 TTC sailplanes that are

equipped with Bombardier ROTAX

(ROTAX) 914 F series engines, serial

numbers 4,420.011 through 4,420.058,

was published in the Federal Register

as a notice of proposed rulemaking

(NPRM) on February 11, 1998 (63 FR

6882). The NPRM proposed to require

inspecting the banjo bolt for a valve

seat. If the banjo bolt does not have a

valve seat, this AD will require

replacing the banjo bolt, and repairing

or replacing the turbocharger.

Accomplishment of the proposed

installation will be in accordance with

Bombardier ROTAX Technical Bulletin

No. 914–04, dated August, 1997.

The NPRM was the result of

mandatory continuing airworthiness

information (MCAI) issued by the

airworthiness authority for Austria.

Interested persons have been afforded

an opportunity to participate in the

making of this amendment. No

comments were received on the

proposed rule or the FAA’s

determination of the cost to the public.

The FAA’s Determination

After careful review of all available

information related to the subject

presented above, the FAA has

determined that air safety and the

public interest require the adoption of
Federal Register / Vol. 63, No. 81 /Tuesday, April 28, 1998 /Rules and Regulations 23201

the rule as proposed except for minor

editorial corrections. The FAA has

determined that these minor corrections

will not change the meaning of the AD

and will not add any additional burden

upon the public than was already

proposed.

Cost Impact

The FAA estimates that 4 sailplanes

in the U.S. registry will be affected by

this AD, that it will take approximately

1 workhour per sailplane to accomplish

this inspection, and that the average

labor rate is approximately $60 an hour.

Based on these figures, the total cost

impact of this AD on U.S. operators is

estimated to be $240 or $60 per

sailplane.

Regulatory Impact

The regulations adopted herein will

not have substantial direct effects on the

States, on the relationship between the

national government and the States, or

on the distribution of power and

responsibilities among the various

levels of government. Therefore, in

accordance with Executive Order 12612,

it is determined that this final rule does

not have sufficient federalism

implications to warrant the preparation

of a Federalism Assessment.

For the reasons discussed above, I

certify that this action (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)

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

adding a new airworthiness directive

(AD) to read as follows:

98–09–14 Diamond Aircraft Industries:

Amendment 39–10495; Docket No. 97–

CE–132–AD.

Applicability: Model HK 36 TTS and HK

36 TTC sailplanes, all serial numbers,

certificated in any category, that are

equipped with Bombardier ROTAX 914 F

series engines, serial numbers 4,420.011

through 4,420.058.

Note 1: This AD applies to each sailplane

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

sailplanes 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.

Compliance: Required within the next 10

hours time-in-service (TIS) after the effective

date of this AD, unless already accomplished.

To prevent possible loss of engine power,

which could result in possible loss of control

of the sailplane, accomplish the following:

(a) Inspect the Bombardier ROTAX

engine’s turbocharger oil-pressure line for a

banjo bolt with a valve seat, part number

(P/N) 941 782 (or an FAA-approved

equivalent part number), in accordance with

the Instructions section of Bombardier

ROTAX Technical Bulletin No. 914–04,

dated August, 1997.

Note 2: An incorrect banjo bolt would have

a built-in orifice, instead of a valve seat.

(b) If an incorrect banjo bolt is installed,

prior to further flight, replace the banjo bolt

with one that has P/N 941 782 (or an FAAapproved equivalent part number), and repair

or replace the turbocharger in accordance

with the Instructions section of Bombardier

ROTAX Technical Bulletin No. 914–04,

dated August, 1997.

(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 sailplane

to a location where the requirements of this

AD can be accomplished.

(d) An alternative method of compliance or

adjustment of the compliance time that

provides an equivalent level of safety may be

approved by the Manager, Small Airplane

Directorate, 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) Questions or technical information

related to Bombardier ROTAX Technical

Bulletin No. 914–04, dated August 1997,

should be directed to Diamond Aircraft

Industries, G.m.b.H., N.A. Otto-Strabe 5, A–

2700, Wiener Neustadt, Austria. This service

information may be examined at the FAA,

Central Region, Office of the Regional

Counsel, Room 1558, 601 E. 12th Street,

Kansas City, Missouri 64106.

(f) The inspection and replacement

required by this AD shall be done in

accordance with Bombardier ROTAX

Technical Bulletin No. 914–04, dated August,

1997. 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 Diamond Aircraft Industries, G.m.b.H.,

N.A. Otto-Strabe 5, A–2700, Wiener

Neustadt, Austria. 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.

Note 4: The subject of this AD is addressed

in Austrian AD No. 90, undated.

(g) This amendment becomes effective on

June 14, 1998.

Issued in Kansas City, Missouri, on April

17, 1998.

James A. Jackson,

Acting Manager, Small Airplane Directorate,

Aircraft Certification Service.

[FR Doc. 98–11008 Filed 4–27–98; 8:45 am]

BILLING CODE 4910–13–U

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 97–CE–104–AD; Amendment

39–10494; AD 98–09–13]

RIN 2120–AA64

Airworthiness Directives; Alexander

Schleicher Segelflugzeugbau Model

ASK 21 Sailplanes

AGENCY: Federal Aviation

Administration, DOT.

ACTION: Final rule.

SUMMARY: This amendment adopts a

new airworthiness directive (AD) that

applies to certain Alexander Schleicher

Segelflugzeugbau (Alexander

Schleicher) Model ASK 21 sailplanes.

This AD requires inspecting the Sshaped rudder pedal tube for

displacement, and correcting any

displacement of the plastic tube. This

AD is the result of mandatory

continuing airworthiness information

(MCAI) issued by the airworthiness

authority for Germany. The actions

specified by this AD are intended to

prevent rudder control jamming, which