10808 Federal Register / Vol. 60, No. 39 / Tuesday, February 28, 1995 / Rules and Regulations

§ 39.13 [Amended]

2. Section 39.13 is amended by

adding the following new airworthiness

directive:

95–03–07 Aerospatiale: Amendment 39–

9144. Docket 94–NM–83–AD.

Applicability: Model ATR72–101, –102,

–201, and –202 series airplanes; as listed in

Aerospatiale Service Bulletin ATR72–27–

1033, dated February 23, 1994; 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 use the authority

provided in paragraph (d) to request approval

from the FAA. This approval may address

either no action, if the current configuration

eliminates the unsafe condition; or different

actions necessary to address the unsafe

condition described in this AD. Such a

request should include an assessment of the

effect of the changed configuration on the

unsafe condition addressed by this AD. In no

case does the presence of any modification,

alteration, or repair remove any airplane from

the applicability of this AD.

Compliance: Required as indicated, unless

accomplished previously.

To prevent problems associated with

corrosion of the flight control rods, which

could compromise the required strength of

these items, accomplish the following:

Note 2: Rods replaced and installed in

accordance with the instructions of any

version of Aerospatiale Service Bulletin

ATR72–27–1010 prior to the effective date of

this AD are not affected by the requirements

of this AD.

(a) For airplanes having Manufacturer’s

Serial Numbers (MSN) 126 through 183,

inclusive: Within 18 months after the

effective date of this AD, visually inspect the

elevator trim fail-safe rods to determine the

model and the orientation of the open end of

the rod, in accordance with Part A of

Aerospatiale Service Bulletin ATR72–27–

1033, dated February 23, 1994.

(1) If a SARMA-type rod is installed, prior

to further flight, replace that rod with a

modified rod, in accordance with

Aerospatiale Service Bulletin ATR72–27–

1012, Revision 3, dated October 7, 1991.

(2) If a TAC-type rod is installed, and if the

open end of the rod is oriented in any

direction other than downwards, prior to

further flight, accomplish the reverse

installation procedures specified in

Aerospatiale Service Bulletin ATR72–27–

1010, Revision 4, dated February 23, 1994.

(b) For airplanes having MSN’s 126

through 198 inclusive, 204, and 207: Within

18 months after the effective date of this AD,

visually inspect the rudder trim fail-safe rods

to determine the model and the orientation

of the open end of the rod, in accordance

with Part B of Aerospatiale Service Bulletin

ATR72–27–1033, dated February 23, 1994.

(1) If a SARMA-type rod is installed, prior

to further flight, replace that rod with a

modified rod, in accordance with

Aerospatiale Service Bulletin ATR72–27–

1012, Revision 3, dated October 7, 1991.

(2) If a TAC-type rod is installed, and if the

open end of the rod is oriented in any

direction other than downwards, prior to

further flight, accomplish the reverse

installation procedures specified in

Aerospatiale Service Bulletin ATR72–27–

1010, Revision 4, dated February 23, 1994.

(c) For airplanes having MSN’s 198, and

126 through 237 inclusive: Within 18 months

after the effective date of this AD, visually

inspect the rudder travel limitation unit failsafe rods to determine the model and the

orientation of the open end of the rod, in

accordance with Part C of Aerospatiale

Service Bulletin ATR72–27–1033, dated

February 23, 1994.

(1) If a SARMA-type rod is installed, prior

to further flight, replace that rod with a new

rod in accordance with Aerospatiale Service

Bulletin ATR72–27–1027, dated July 28,

1993.

(2) If a TAC-type rod is installed at the

rudder travel limitation rod location, and if

the open end of the rod is oriented in any

direction other than downwards, prior to

further flight, inspect that rod in accordance

with Aerospatiale Service Bulletin ATR72–

27–1027, dated July 28, 1993.

(i) If no crack(s), deformation, or corrosion

of the rod is found, prior to further flight,

reinstall the rod so that the open end is

oriented downwards, in accordance with the

service bulletin.

(ii) If any crack(s), deformation, or

corrosion of the rod is found, prior to further

flight, replace the rod with a modified rod in

accordance with the service bulletin.

(d) 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,

Standardization Branch, ANM–113, FAA,

Transport Airplane Directorate. Operators

shall submit their requests through an

appropriate FAA Principal Maintenance

Inspector, who may add comments and then

send it to the Manager, Standardization

Branch, ANM–113.

Note 3: Information concerning the

existence of approved alternative methods of

compliance with this AD, if any, may be

obtained from the Standardization Branch,

ANM–113.

(e) Special flight permits may be issued in

accordance with §§ 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.

(f) The inspections, replacements, reverse

installations, and reinstallation shall be done

in accordance with the following

Aerospatiale service bulletins, as applicable,

which contain the specified effective pages:

Service bulletin referenced and date Page No.

Revision

level shown

on page

Date shown on

page

ATR72–27–1012, Revision 3, October 7, 1991 ................................................................ 1 ............................. 3 .................. Oct. 7, 1991.

2, 4, 6, 9 ................. Original ........ Oct. 29, 1990.

5, 7, 8 ..................... 1 .................. Nov. 21, 1990.

3 ............................. 2 .................. May 16, 1991.

ATR72–27–1033 Original Issue, February 23, 1994 ........................................................ 1–10 ....................... Original ........ Feb. 23, 1994.

ATR72–27–1027, Original Issue, July 28, 1993 ............................................................... 1–11 ....................... Original ........ July 28, 1993.

ATR72–27–1010, Revision 4, February 23, 1994 ............................................................. 1, 3 ......................... 4 .................. Feb. 23, 1994.

2, 7 ......................... Original ........ June 22, 1990.

4 ............................. 2 .................. Jan. 10, 1991.

5, 6 ......................... 1 .................. Nov. 21, 1990.

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 Aerospatiale, 316 Route de Bayonne,

31060 Toulouse, Cedex 03, France. Copies

may be inspected at the FAA, Transport

Airplane Directorate, 1601 Lind Avenue,

SW., Renton, Washington; or at the Office of

the Federal Register, 800 North Capitol

Street, NW., suite 700, Washington, DC.

(g) This amendment becomes effective on

March 30, 1995.

Issued in Renton, Washington, on February

6, 1995.

S.R. Miller,

Acting Manager, Transport Airplane

Directorate, Aircraft Certification Service.

[FR Doc. 95–3356 Filed 2–27–95; 8:45 am]

BILLING CODE 4910–13–U
Federal Register / Vol. 60, No. 39 / Tuesday, February 28, 1995 / Rules and Regulations 10809

LEGAL SERVICES CORPORATION

45 CFR Part 1611

Eligibility: Income Level for Individuals

Eligible for Assistance

AGENCY: Legal Services Corporation.

ACTION: Final rule.

SUMMARY: The Legal Services

Corporation (‘‘Corporation’’) is required

by law to establish maximum income

levels for individuals eligible for legal

assistance. This document updates the

specified income levels to reflect the

annual amendments to the Federal

Poverty Guidelines as issued by the

Department of Health and Human

Services.

EFFECTIVE DATE: February 28, 1995.

FOR FURTHER INFORMATION CONTACT:

Victor M. Fortuno, General Counsel,

Legal Services Corporation, 750 First

Street NE, Washington, D.C. 20002–

4250; 202–336–8810.

SUPPLEMENTARY INFORMATION: Section

1007(a)(2) of the Legal Services

Corporation Act (‘‘Act’’), 42 U.S.C.

2996f(a)(2), requires the Corporation to

establish maximum income levels for

individuals eligible for legal assistance,

and the Act provides that other

specified factors shall be taken into

account along with income.

Section 1611.3(b) of the Corporation’s

regulations establishes a maximum

income level equivalent to one hundred

and twenty-five percent (125%) of the

official Federal Poverty Income

Guidelines.

Responsibility for revision of the

official Federal Poverty Income

Guidelines was shifted in 1982 from the

Community Services Administration to

the Department of Health and Human

Services. The revised figures for 1995

set out below are equivalent to 125% of

the current official Poverty Guidelines

as set out at 60 FR 7772 (Feb. 9, 1995).

List of Subjects in 45 CFR Part 1611

Legal services.

PART 1611—ELIGIBILITY

1. The authority citation for Part 1611

continues to read as follows:

Authority: Secs. 1006(b)(1), 1007(a)(1)

Legal Services Corporation Act of 1974, 42

U.S.C. 2996e(b)(1), 2996f(a)(1), 2996f(a)(2).

2. Appendix A of Part 1611.is revised

to read as follows:

APPENDIX A OF PART 1611.—LEGAL

SERVICES CORPORATION 1995 POVERTY GUIDELINES*

Size of

family

unit

All states

but Alaska and

Hawaii 1

Alaska 2 Hawaii 3

1 ............ $9,338 $11,675 $10,763

2 ............ 12,538 15,675 14,438

3 ............ 15,738 19,675 18,113

4 ............ 18,938 23,675 21,788

5 ............ 22,138 27,675 25,463

6 ............ 25,338 31,675 29,138

7 ............ 28,538 35,675 32,813

8 ............ 31,738 39,675 36,488

*The figures in this table represent 125% of

the poverty guidelines by family size as determined by the Department of Health and

Human Services. 1For family units with more than eight members, add $3,200 for each additional member

in a family. 2For family units with more than eight members, add $4,000 for each additional member

in a family. 3For family units with more than eight members, add $3,675 for each additional member

in a family.

Victor M. Fortuno,

General Counsel.

[FR Doc. 95–4837 Filed 2–27–95; 8:45 am]

BILLING CODE 7050–01–P