Federal Register / Vol. 63, No. 95 / Monday, May 18, 1998 /Rules and Regulations 27195

Sponsor’s household size 100% of poverty line 125% of poverty line

4 ..................................................................................................................................... 18,920 ................................ 23,650

5 ..................................................................................................................................... 22,140 ................................ 27,675

6 ..................................................................................................................................... 25,360 ................................ 31,700

7 ..................................................................................................................................... 28,580 ................................ 35,725

8 ..................................................................................................................................... 31,800 ................................ 39,750

Add $3,220 for each additional person.Add $4,025 for each additional person.

Dated: April 30, 1998.

Doris Meissner,

Commissioner, Immigration and

Naturalization Service.

[FR Doc. 98–12952 Filed 5–15–98; 8:45 am]

BILLING CODE 4410–10–M

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 98–NM–21–AD; Amendment

39–10425; AD 97–25–11R1]

RIN 2120–AA64

Airworthiness Directives; Bombardier

Model CL–600–2B16 Series Airplanes

AGENCY: Federal Aviation

Administration, DOT.

ACTION: Direct final rule; confirmation of

effective date.

SUMMARY: This document confirms the

effective date of a direct final rule

published on March 27, 1998 which

revised an existing airworthiness

directive (AD), applicable to certain

Bombardier Model CL–600–2B16 series

airplanes, that currently requires

disabling the remote fuel/defuel panel

in the cockpit; and provides for an

optional modification of the remote

fuel/defuel panel, which would

terminate the requirement to disable the

panel. The direct final rule amendment

reduces the applicability of the existing

AD. The direct final rule amendment

was prompted by reports of in-flight

failure of the panel that resulted when

a circuit breaker on a battery bus opened

due to insufficient current flow

capacity. The actions specified in this

AD are intended to prevent the circuit

breakers from opening during flight,

which could result in irreversible loss of

engine indicating and fuel quantity

systems in the cockpit.

DATES: The direct final rule published at

63 FR 14804 is effective on June 25,

1998.

FOR FURTHER INFORMATION CONTACT:

Brett Portwood, Aerospace Engineer,

Systems and Equipment Branch, ANM–

130L, FAA, Transport Airplane

Directorate, Los Angeles Aircraft

Certification Office, 3960 Paramount

Boulevard, Lakewood, California 90712;

telephone (562) 627–5350; fax (562)

627–5210.

SUPPLEMENTARY INFORMATION: The FAA

published the direct final rule with

request for comments in the Federal

Register on March 27, 1998 (63 FR

14804). The FAA uses the direct final

rulemaking procedure for a noncontroversial rule where the FAA

anticipates that there will be no adverse

public comment. The direct final rule

advised the public that no adverse

comments were anticipated, and that

unless a written adverse comment, or a

written notice of intent to submit such

an adverse comment, was received

within the comment period, the

regulation would become effective on

June 25, 1998. No adverse comments

were received, and thus this document

confirms that this final rule will become

effective on that date, with the

airworthiness directive (AD) number

shown at the beginning of this

document.

Issued in Renton, Washington, on May 5,

1998.

John J. Hickey,

Acting Manager, Transport Airplane

Directorate, Aircraft Certification Service.

[FR Doc. 98–12513 Filed 5–15–98; 8:45 am]

BILLING CODE 4910–13–P

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 98–CE–40–AD; Amendment 39–

10528; AD 98–11–01]

RIN 2120–AA64

Airworthiness Directives; Pilatus

Aircraft Ltd. Models PC–12 and PC–12/

45 Airplanes

AGENCY: Federal Aviation

Administration, DOT.

ACTION: Final rule; request for

comments.

SUMMARY: This amendment supersedes

Airworthiness Directive (AD) 97–23–04,

which currently requires replacing the

fuel tank vent valves with modified fuel

tank vent valves on certain Pilatus

Aircraft Ltd. (Pilatus) Models PC–12 and

PC–12/45 airplanes. This AD retains the

fuel tank vent valves replacement

required by AD 97–23–04, and requires

drilling a 4.8 millimeter (0.1875 inch)

hole in each fuel filler cap. This AD also

requires inserting a temporary revision

in the Pilot’s Operating Handbook

(POH) that specifies checking to assure

that the fuel filler cap hole is clear of ice

and foreign objects. This AD is the

result of mandatory continued

airworthiness information (MCAI)

issued by the airworthiness authority for

Switzerland. The actions specified by

this AD are intended to prevent the fuel

tank inward vent valve from freezing,

which, if followed by a cold soak at

altitude, could result in wing airfoil

distortion and structural damage with

consequent degradation of the airplane’s

handling qualities.

DATES: Effective June 7, 1998.

The incorporation by reference of

Pilatus Service Bulletin No. 28–003,

Revision 1, dated September 30, 1997,

as listed in the regulations, was

previously approved by the Director of

the Federal Register as of December 1,

1997 (62 FR 59993, November 6, 1997).

The incorporation by reference of

Pilatus Service Bulletin No. 28–004,

dated March 27, 1998, is approved by

the Director of the Federal Register as of

June 7, 1998.

Comments for inclusion in the Rules

Docket must be received on or before

July 13, 1998.

ADDRESSES: Submit comments in

triplicate to the Federal Aviation

Administration (FAA), Central Region,

Office of the Regional Counsel,

Attention: Rules Docket No. 98–CE–40–

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

Kansas City, Missouri 64106.

Service information that applies to

this AD may be obtained from Pilatus

Aircraft Ltd., CH–6370 Stans,

Switzerland. This information may also

be examined at the Federal Aviation

Administration (FAA), Central Region,

Office of the Regional Counsel,

Attention: Rules Docket No. 98–CE–40–

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

Kansas City, Missouri 64106; or at the