21976 Federal Register / Vol. 60, No. 86 / Thursday, May 4, 1995 / Rules and Regulations

The employment authorization

document will be given to the applicant

after an interview has been completed

by an immigration officer unless a

formal denial is issued by the

appropriate INS office. * * *

* * * * *

20. Section 245a.4 is amended by:

a. Removing in paragraph (b)(10), in

the first sentence the phrase ‘‘Forms I–

688A and I–688’’ and adding in its place

the phrase ‘‘an employment

authorization document and Form I–

688’’;

b. Removing in paragraph

(b)(14)(ii)(b), in the third sentence the

phrase ‘‘Form I–688A, Employment

Authorization,’’ and adding in its place

the phrase ‘‘An employment

authorization document’’; and

c. Revising in paragraph (b)(14)(iii)

the second sentence to read as follows:

§ 245a.4 Adjustment to lawful resident

status of certain nationals of countries for

which extended voluntary departure has

been made available.

* * * * *

(b) * * *

(14) * * *

(iii) * * * The alien will be required

to return to the appropriate INS office,

surrender the I–688A or employment

authorization document previously

issued, and obtain Form I–688,

Temporary Resident Card, authorizing

employment and travel abroad.

* * * * *

PART 274a—CONTROL OF

EMPLOYMENT OF ALIENS

21. The authority citation for part

274a continues to read as follows:

Authority: 8 U.S.C. 1101, 1103, 1324a; 8

CFR part 2.

§ 274a.12 [Amended]

22. In § 274a.12 paragraph (c)(10), in

the first sentence is amended by

removing the phrase ‘‘, if the alien

establishes the economic need to work’’.

23. In § 274a.13, paragraph (a) is

revised to read as follows:

274a.13 Application for employment

authorization.

(a) General. Aliens authorized to be

employed under § 274a.12(a)(3)–(8) and

(10)–(13) must file an Application for

Employment Authorization (Form I–

765) in order to obtain documentation

evidencing this fact.

(1) Aliens who may apply for

employment authorization under

§ 274a.12(c) of this part, except for those

who may apply under § 274a.12(c)(8),

shall file a Form I–765 with the director

having jurisdiction over applicant’s

residence, or the director having

jurisdiction over the port of entry at

which the alien applies, or with such

other Service office as the

Commissioner may designate. The

approval of applications filed under

§ 274a.12(c) of this part, except for

§ 274a.12(c)(8), shall be within the

discretion of the director or such other

officer as the Commissioner may

designate. Where economic necessity

has been identified as a factor, the alien

must provide information regarding his

or her assets, income, and expenses in

accordance with instructions on Form I–

765.

(2) An initial Application for

Employment Authorization (Form I–

765) for asylum applicants under

274a.12(c)(8) of this part shall be filed

in accordance with instructions on or

attached to Form I–765 with the

appropriate Service Center or with such

other Service office as the

Commissioner may designate. The

applicant also must submit a copy of the

underlying application for asylum or

withholding of deportation, together

with evidence that the application has

been filed in accordance with §§ 208.3

and 208.4 of this chapter. An

application for an initial employment

authorization or for a renewal of

employment authorization filed in

relation to a pending claim for asylum

shall be adjudicated in accordance with

§ 208.7 of this chapter. An application

for renewal or replacement of

employment authorization submitted in

relation to a pending claim for asylum,

as provided in § 208.7 of this chapter,

shall be filed, with fee or application for

waiver of such fee, in accordance with

the instructions on or attached to Form

I–765 with the appropriate Service

Center or with such other Service office

as the Commissioner may designate.

* * * * *

Dated: May 1, 1995.

Doris Meissner,

Commissioner, Immigration and

Naturalization Service.

[FR Doc. 95–11058 Filed 5–2–95; 8:45 am]

BILLING CODE 4410–10–M

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 91–ASW–28; Amendment 39–

9209; AD 95–09–06]

Airworthiness Directives; Bell

Helicopter Textron, Inc. Model 206A,

206B, 206L, 206L–1, and 206L–3

Helicopters

AGENCY: Federal Aviation

Administration, DOT.

ACTION: Final rule.

SUMMARY: This amendment adopts a

new airworthiness directive (AD),

applicable to Bell Helicopter Textron,

Inc. (BHTI) Model 206A, 206B, 206L,

206L–1, and 206L–3 helicopters, that

requires installing a protective

mechanical fuel valve switch guard on

the fuel valve switch. This amendment

is prompted by reports of airmen

inadvertently placing the fuel valve

switch to the ‘‘OFF’’ position. The

actions specified by this AD are

intended to prevent the fuel valve

switch from being inadvertently placed

in the ‘‘OFF’’ position, which could

result in an engine failure and a

subsequent power-off landing.

DATES: Effective June 8, 1995.

The incorporation by reference of

certain publications listed in the

regulations is approved by the Director

of the Federal Register as of June 8,

1995.

ADDRESSES: The service information

referenced in this AD may be obtained

from Bell Helicopter Textron, Inc.,

Attention: Customer Support, P.O. Box

482, Fort Worth, Texas 76101. This

information may be examined at the

FAA, Office of the Assistant Chief

Counsel, 2601 Meacham Blvd., Room

663, Fort Worth, Texas; or at the Office

of the Federal Register, 800 North

Capitol Street, NW., suite 700,

Washington, DC.

FOR FURTHER INFORMATION CONTACT: Mr.

Lance Gant, Aerospace Engineer,

Rotorcraft Certification Office,

Rotorcraft Directorate, FAA, 2601

Meacham Blvd., Fort Worth, Texas

76137, telephone (817) 222–5141, fax

(817) 222–5959.

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 Bell Helicopter

Textron, Inc. (BHTI) Model 206A, 206B,

206L, 206L–1, and 206L–3 helicopters

was published in the Federal Register

on November 14, 1994 (59 FR 56436).
Federal Register / Vol. 60, No. 86 / Thursday, May 4, 1995 / Rules and Regulations 21977

That action proposed to require

installing a protective mechanical fuel

valve switch guard on the fuel valve

switch.

Interested persons have been afforded

an opportunity to participate in the

making of this amendment. No

comments were received on the

proposal or the FAA’s determination of

the cost to the public. The FAA has

determined that air safety and the

public interest require the adoption of

the rule as proposed, except for editorial

changes.

The FAA estimates that 5,192

helicopters of U.S. registry will be

affected by this AD, that it will take

approximately 1 work hour per

helicopter to accomplish the required

actions, and that the average labor rate

is $60 per work hour. Required parts

will cost nothing for these helicopters

since the manufacturer is providing full

warranty compensation for the parts.

Based on these figures, the total cost

impact of the AD on U.S. operators is

estimated to be $311,520.

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 a new airworthiness directive to

read as follows:

95–09–06 Bell Helicopter Textron, Inc.:

Amendment 39–9209. Docket No. 91–

ASW–28.

Applicability: Model 206A, 206B, 206L,

206L–1, and 206L–3 helicopters, certificated

in any category.

Note 1: This AD applies to each helicopter

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

helicopters 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 (b) 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 helicopter

from the applicability of this AD.

Compliance: Required as indicated, unless

accomplished previously.

To prevent the fuel valve switch from

being inadvertently placed in the ‘‘OFF’’

position, which could result in an engine

failure and a subsequent power-off landing,

accomplish the following:

(a) Within the next 50 hours time-inservice after the effective date of this

airworthiness directive (AD), modify the fuel

valve switch to add a protective mechanical

fuel valve switch guard as follows:

(1) For the Model 206A, serial numbers (S/

N) 1 through 153, modify in accordance with

Part I of the Accomplishment Instructions in

BHTI Alert Service Bulletin (ASB) No. 206–

90–54, dated May 31, 1990.

(2) For the Model 206A, S/N 154 through

660 and 672 through 715, and Model 206B,

S/N 661 through 671 and 716 through 913,

modify in accordance with Part II of the

Accomplishment Instructions in ASB No.

206–90–54, dated May 31, 1990.

(3) For the Model 206B, S/N 914 through

4069 and 4071 through 4074, modify in

accordance with Part III of the

Accomplishment Instructions in ASB No.

206–90–54, dated May 31, 1990.

(4) For the visual flight rule-equipped

Model 206L, S/N 45001 through 45153 and

46601 through 46617, Model 206L–1, S/N

45154 through 45790, and Model 206L–3, S/

N 51001 through 51319, modify in

accordance with Part I of the

Accomplishment Instructions in BHTI ASB

No. 206L–90–67, Revision A, dated August 5,

1991.

(5) For the Model 206L–1, S/N 45154

through 45790, and Model 206L–3, S/N

51001 through 51319, equipped with

instrument flight rule kit, part number 206–

705–001–101, installed per BHTI Service

Instructions No. 206–2030, modify in

accordance with Part II of the

Accomplishment Instructions in ASB No.

206L–90–67, Revision A, dated August 5,

1991.

(b) An alternative method of compliance or

adjustment of the compliance time that

provides an acceptable level of safety may be

used when approved by the Manager,

Rotorcraft Certification Office, FAA,

Rotorcraft Directorate. Operators shall submit

their requests through an FAA Principal

Maintenance Inspector, who may concur or

comment and then send it to the Manager,

Rotorcraft Certification Office.

Note 2: Information concerning the

existence of approved alternative methods of

compliance with this AD, if any, may be

obtained from the Rotorcraft 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 helicopter

to a location where the requirements of this

AD can be accomplished.

(d) The modification shall be done in

accordance with Bell Helicopter Textron, Inc.

ASB 206–90–54, dated May 31, 1990, and

ASB 206L–90–67, Revision A, dated August

5, 1991. 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 Bell Helicopter Textron, Inc., Attention:

Customer Support, P.O. Box 482, Fort Worth,

Texas 76101. Copies may be inspected at the

FAA, Office of the Assistant Chief Counsel,

2601 Meacham Blvd., Room 663, Fort Worth,

Texas; or at the Office of the Federal Register,

800 North Capitol Street, NW., suite 700,

Washington, DC.

(e) This amendment becomes effective on

June 8, 1995.

Issued in Fort Worth, Texas, on April 24,

1995.

Eric Bries,

Acting Manager, Rotorcraft Directorate,

Aircraft Certification Service.

[FR Doc. 95–10589 Filed 5–3–95; 8:45 am]

BILLING CODE 4910–13–P

14 CFR Part 39

[Docket No. 95–NM–68–AD; Amendment

39–9213; AD 95–09–10]

Airworthiness Directives; McDonnell

Douglas Model DC–9–80 Series

Airplanes and Model MD–88 Airplanes

AGENCY: Federal Aviation

Administration, DOT.

ACTION: Final rule; request for

comments.