This section of the FEDERAL REGISTER

contains regulatory documents having general

applicability and legal effect, most of which

are keyed to and codified in the Code of

Federal Regulations, which is published under

50 titles pursuant to 44 U.S.C. 1510.

The Code of Federal Regulations is sold by

the Superintendent of Documents. Prices of

new books are listed in the first FEDERAL

REGISTER issue of each week.

Rules and Regulations Federal Register

19343

Vol. 60, No. 74

Tuesday, April 18, 1995

DEPARTMENT OF ENERGY

Office of Energy Efficiency and

Renewable Energy

10 CFR Part 436

[Docket No. EE–RM–94–201]

RIN 1904–AA62

Federal Energy Management and

Planning Programs; Energy Savings

Performance Contract Procedures and

Methods

AGENCY: Department of Energy.

ACTION: Correction to final regulations.

SUMMARY: This document contains

corrections to the Final Regulations

which were published on Monday,

April 10, 1995 (60 FR 18326). The

regulations establish a five-year pilot

program of energy savings performance

contracts designed to accelerate

investment in cost effective energy

conservation measures in existing

Federal buildings and thereby save

taxpayer dollars.

EFFECTIVE DATE: April 10, 1995.

FOR FURTHER INFORMATION CONTACT: Joan

G. Stone (202) 586–5772.

SUPPLEMENTARY INFORMATION:

Need for Correction

As published, the rules become

effective 30 days after date of

publication. The Department intended

for the rule to become effective upon

publication in order to relieve

substantive restrictions that apply to

procurements under other regulations.

Correction of Publication

Accordingly, the final rule published

on April 10, 1995, which was the

subject of FR Doc No. 95–8750, is

corrected as follows:

On page 18326, 1st column, the

EFFECTIVE DATE caption is corrected to

read:

EFFECTIVE DATES: These rules become

effective April 10, 1995.

On page 18334, 2nd column, the

following paragraph is added as

paragraph G in section III. Procedural

Requirements:

G. Effective Date

DOE is making today’s final rule

effective upon publication because it

will relieve substantive restrictions that

apply to procurements under other

regulations. No member of the public

will be prejudiced by this action

because of a lack of timely notice.

§ 436.30 [Corrected]

On page 18334, 3rd column, in

§ 436.30, paragraph (a), first sentence,

the date ‘‘May 10, 1995’’ is corrected to

read ‘‘April 10, 1995’’.

Issued in Washington, DC on April 11,

1995.

Brian T. Castelli,

Chief of Staff for Energy Efficiency and

Renewable Energy.

[FR Doc. 95–9420 Filed 4–17–95; 8:45 am]

BILLING CODE 6450–01–P

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 94–ANE–42; Amendment 39–

9181; AD 95–07–02]

Airworthiness Directives; AlliedSignal

Inc. TFE731–3 Series Turbofan

Engines

AGENCY: Federal Aviation

Administration, DOT.

ACTION: Final rule.

SUMMARY: This amendment adopts a

new airworthiness directive (AD),

applicable to AlliedSignal Inc. (formerly

Garrett Turbine Engine Company)

TFE731–3 series turbofan engines, that

requires the removal of suspect low

pressure turbine (LPT) disks due to their

susceptibility to creep fatigue. This

amendment is prompted by reports of

LPT disks that have separated through

the disk web due to creep fatigue. The

actions specified by this AD are

intended to prevent an LPT disk web

separation, which may result in an

uncontained engine failure and damage

to the aircraft.

DATES: Effective on June 19, 1995.

The incorporation by reference of

certain publications listed in the

regulations is approved by the Director

of the Federal Register as of June 19,

1995.

ADDRESSES: The service information

referenced in this AD may be obtained

from AlliedSignal Inc., Aviation

Services Division, Data Distribution,

Dept. 6403/2102–201, P.O. Box 29003,

Phoenix, AZ 85038–9003; telephone

(602) 365–2548, fax (602) 365–2210.

This information may be examined at

the Federal Aviation Administration

(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.

FOR FURTHER INFORMATION CONTACT:

Joseph Costa, Aerospace Engineer, Los

Angeles Aircraft Certification Office,

FAA, Transport Airplane Directorate,

3960 Paramount Blvd., Lakewood, CA

90712–4137; telephone (310) 627–5246;

fax (310) 627–5210.

SUPPLEMENTARY INFORMATION: A

proposal to amend part 39 of the Federal

Aviation Regulations (14 CFR part 39) to

include an airworthiness directive (AD)

that is applicable to AlliedSignal Inc.

(formerly Garrett Turbine Engine

Company) TFE731–3 series turbofan

engines was published in the Federal

Register on November 29, 1994 (59 FR

60922). That action proposed to require

removal of suspect specific serial

numbered first and second stage low

pressure turbine (LPT) disks in

accordance with AlliedSignal Aerospace

Alert Service Bulletin (ASB) No.

TFE731–A72–3544, dated October 8,

1993, and ASB No. TFE731–A72–3557,

dated May 12, 1994.

Interested persons have been afforded

an opportunity to participate in the

making of this amendment. No

comments were received on the

proposal. The Federal Aviation

Administration’s (FAA) has determined

that the average labor rate has increased

since publication of the NPRM to $60

per work hour. The economic analysis

of this final rule has been changed

accordingly. The FAA has determined

that air safety and the public interest

require the adoption of the rule with the

changes described previously. The FAA

has determined that these changes will

not increase the scope of the AD.
19344 Federal Register / Vol. 60, No. 74 / Tuesday, April 18, 1995 / Rules and Regulations

There are approximately 350 engines

with the affected serial numbered disks

in the worldwide fleet. The FAA

estimates that 175 engines installed on

aircraft of U.S. registry will be affected

by this AD, that it will take

approximately 10 work hours per engine

to accomplish the required actions, and

that the average labor rate is $60 per

work hour. Required parts will cost

approximately $18,000 per engine.

Based on these figures, the total cost

impact of the AD on U.S. operators is

estimated to be $3,255,000.

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 final evaluation has

been prepared for this action and it is

contained in the Rules Docket. A copy

of it may be obtained from 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. App. 1354(a), 1421

and 1423; 49 U.S.C. 106(g); and 14 CFR

11.89.

§ 39.13 [Amended]

2. Section 39.13 is amended by

adding the following new airworthiness

directive:

95–07–02 AlliedSignal Inc.: Amendment

39–9181. Docket 94–ANE–42.

Applicability: AlliedSignal Inc. (formerly

Garrett Turbine Engine Company) TFE731–3,

–3A, –3AR, –3B, –3BR, and –3R turbofan

engine models installed on but not limited to

Avions Marcel Dassault Falcon 50, Lockheed

1329–23, –25 series (731 Jetstar, Jetstar II),

Israel Aircraft Industries (IAI) Ltd. 1124

(Westwind), Raytheon Corporate Jets Inc.

(formerly British Aerospace) (BAe) DH/HS/

BH 125 series, Learjet 55 series, Cessna 650

Citation III, VI, Sabreliner NA–265 series

(Sabreliner 65). This airworthiness directive

(AD) is not applicable to TFE731–3A–300G

and TFE731–3AR–200G engines installed on

IAI 1125 Westwind Astra aircraft.

Compliance: Required as indicated, unless

accomplished previously.

To prevent a low pressure turbine (LPT)

disk web separation, which may result in an

uncontained engine failure and damage to

the aircraft, accomplish the following:

(a) Remove from service first and second

stage LPT disks, with Part Numbers (P/N)

3072351–(), 3072542–(), 3073113–(), and

3073114–(), where () denotes any dash

number, identified by serial number in the

Compliance Sections of AlliedSignal

Aerospace Alert Service Bulletin (ASB) No.

TFE731–A72–3544, dated October 8, 1993,

and AlliedSignal Aerospace ASB No.

TFE731–A72–3557, dated May 12, 1994,

within 1,500 hours time in service (TIS) after

the effective date of this AD, or at the next

removal of the LPT assembly, whichever

occurs first, in accordance with the

Accomplishment Instructions of AlliedSignal

Aerospace ASB No. TFE731–A72–3544,

dated October 8, 1993, and AlliedSignal

Aerospace ASB No. TFE731–A72–3557,

dated May 12, 1994, and replace with

serviceable disks.

(b) An alternative method of compliance or

adjustment of the compliance time that

provides an acceptable level of safety may be

used if approved by the Manager, Los

Angeles Aircraft Certification Office. The

request should be forwarded through an

appropriate FAA Principal Maintenance

Inspector, who may add comments and then

send it to the Manager, Los Angeles Aircraft

Certification Office.

Note: Information concerning the existence

of approved alternative methods of

compliance with this airworthiness directive,

if any, may be obtained from the Los Angeles

Aircraft Certification Office.

(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 aircraft to

a location where the requirements of this AD

can be accomplished.

(d) The removal and replacement of the

affected disks shall be done in accordance

with the following AlliedSignal Aerospace

ASB’s:

Document No. Pages Date

ASB No. TFE731–A72–

3544.

1–10 Oct. 8,

1993.

Total Pages: 10.

ASB No. TFE731–A72–

3557.

1–12 May 12,

1994.

Total Pages: 12.

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 AlliedSignal Inc., Aviation Services

Division, Data Distribution, Dept. 6403/2102–

201, P.O. Box 29003, Phoenix, AZ 85038–

9003; telephone (602) 365–2548, fax (602)

365–2210. 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

June 19, 1995.

Issued in Burlington, Massachusetts, on

March 22, 1995.

James C. Jones,

Acting Manager, Engine and Propeller

Directorate, Aircraft Certification Service.

[FR Doc. 95–8827 Filed 4–17–95; 8:45 am]

BILLING CODE 4910–13–P

14 CFR Part 39

[Docket No. 94–NM–152–AD; Amendment

39–9194; AD 95–08–05]

Airworthiness Directives; British

Aerospace Model BAe 146–100A,

–200A, and –300A, and Model Avro

146–RJ70A, –RJ85A, and –RJ100A

Series Airplanes

AGENCY: Federal Aviation

Administration, DOT.

ACTION: Final rule.

SUMMARY: This amendment supersedes

an existing airworthiness directive (AD),

applicable to certain British Aerospace

Model BAe 146–100A, –200A, and

–300A series airplanes, that currently

requires repetitive inspections of the

attachment bolts and nuts in the rear

spar root joint attachment fittings at

wing rib 2 for integrity of nuts, tightness

of bolts, and/or fuel leaks; and repair, if

necessary. That AD was prompted by

fuel leaks from bolt positions on the rear

spar attachment fitting at wing rib 2.

This amendment provides for an

optional terminating modification for

the repetitive inspections, and expands

the applicability of the existing AD to

include additional airplanes. The

actions specified by this AD are

intended to prevent fuel leaks and a

subsequent fire.

DATES: Effective on May 18, 1995.