Federal Register / Vol. 60, No. 68 / Monday, April 10, 1995 / Rules and Regulations 17987

The OCC, in consultation with the

other banking agencies, will issue

further guidance specifying how the

modified capital standard will be

implemented for reporting purposes.

Following issuance of this additional

guidance, the OCC intends to amend the

rule to include a specific description of

the reporting treatment.

Regulatory Flexibility Act

It is hereby certified that this final

rule will not have a significant

economic impact on a substantial

number of small entities. This final rule

will increase somewhat the measured

risk-based capital ratios of banks of all

sizes that sell assets with low levels of

recourse and will have a beneficial, but

not material, effect on those banks.

Executive Order 12866

The OCC has determined that this

final rule is not a significant regulatory

action under Executive Order 12866.

List of Subjects in 12 CFR Part 3

Administrative practice and

procedure, Capital risk, National banks,

Reporting and recordkeeping

requirements.

Authority and Issuance

For the reasons set out in the

preamble, part 3 of chapter I of title 12

of the Code of Federal Regulations is

amended as follows:

PART 3—MINIMUM CAPITAL RATIOS;

ISSUANCE OF DIRECTIVES

1. The authority citation for part 3 is

revised to read as follows:

Authority: 12 U.S.C. 93a, 161, 1818,

1828(n), 1828 note, 1831n note, 1835, 3907,

and 3909.

2. In appendix A to part 3, section 3

is amended by adding a new paragraph

(c) to read as follows:

Appendix A to Part 3—Risk-Based

Capital Guidelines

* * * * *

Section 3. Risk Categories/Weights for OnBalance Sheet Assets and Off-Balance Sheet

Items

* * * * *

(c) Recourse Obligations. Where the

amount of recourse liability retained by a

bank is less than the capital requirement for

credit-risk exposure, the bank shall maintain

capital for the recourse liability equal to the

amount of credit-risk exposure retained. Any

recourse liability that is subject to this

section 3(c) is not subject to any additional

capital treatment under sections 3(a) or 3(b)

of this appendix A.

* * * * *

Dated: March 17, 1995.

Eugene A. Ludwig,

Comptroller of the Currency.

[FR Doc. 95–8719 Filed 4–7–95; 8:45 am]

BILLING CODE 4810–33–P

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 94–NM–170–AD; Amendment

39–9191; AD 95–08–02]

Airworthiness Directives; Jetstream

Model 4101 Airplanes

AGENCY: Federal Aviation

Administration, DOT.

ACTION: Final rule.

SUMMARY: This amendment adopts a

new airworthiness directive (AD),

applicable to certain Jetstream Model

4101 airplanes, that requires installation

of new case drain pipes and an

additional fairlead support for the

hydraulics case drain line in the rear

spar area of the engine/nacelle. This

amendment is prompted by reports of

fatigue failure of the case drain line in

the hydraulics system. The actions

specified by the proposed AD are

intended to prevent the loss of main

system hydraulics as a result of lack of

support against vibration and

subsequent fatigue failure of the case

drain line for the hydraulics system.

DATES: Effective May 10, 1995.

The incorporation by reference of

certain publications listed in the

regulations is approved by the Director

of the Federal Register as of May 10,

1995.

ADDRESSES: The service information

referenced in this AD may be obtained

from Jetstream Aircraft, Inc., P.O. Box

16029, Dulles International Airport,

Washington, DC 20041–6029. This

information may be examined at the

Federal Aviation Administration (FAA),

Transport Airplane Directorate, Rules

Docket, 1601 Lind Avenue, SW.,

Renton, Washington; or at the Office of

the Federal Register, 800 North Capitol

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

FOR FURTHER INFORMATION CONTACT: Sam

Grober, Aerospace Engineer,

Standardization Branch, ANM–113,

FAA, Transport Airplane Directorate,

1601 Lind Avenue, SW., Renton,

Washington 98055–4056; telephone

(206) 227–1187; fax (206) 227–1320.

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 certain Jetstream

Model 4101 airplanes series airplanes

was published in the Federal Register

on December 16, 1994 (59 FR 64875).

That action proposed to require

installation of new case drain pipes and

an additional fairlead support for the

hydraulics case drain line in the rear

spar area of the engine/nacelle. –

Interested persons have been afforded

an opportunity to participate in the

making of this amendment. Due

consideration has been given to the

single comment received. –

The commenter supports the

proposed rule. –

After careful review of the available

data, including the comment noted

above, the FAA has determined that air

safety and the public interest require the

adoption of the rule as proposed. –

The FAA estimates that 9 airplanes of

U.S. registry will be affected by this AD,

that it will take approximately 10 work

hours per airplane to accomplish the

required actions, and that the average

labor rate is $60 per work hour.

Required parts will be supplied by the

manufacturer at no cost to operators.

Based on these figures, the total cost

impact of the AD on U.S. operators is

estimated to be $5,400, or $600 per

airplane. –

The total cost impact figure discussed

above is based on assumptions that no

operator has yet accomplished any of

the requirements of this AD action, and

that no operator would accomplish

those actions in the future if this AD

were not adopted. –

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.
17988 Federal Register / Vol. 60, No. 68 / Monday, April 10, 1995 / Rules and Regulations

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:

95–08–02 Jetstream Aircraft Limited:

Amendment 39–9191. Docket 94–NM–

170–AD.

Applicability: Model 4101 airplanes;

constructors numbers 41005 through 41015

inclusive, 41019 through 41024 inclusive,

41028, and 41029; 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 (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 airplane from

the applicability of this AD.

Compliance: Required as indicated, unless

accomplished previously.

To prevent the loss of the main system

hydraulics, accomplish the following:

(a) Within 4 months after the effective date

of this AD, install new case drain pipes and

an additional fairlead support for the

hydraulics case drain line in the rear spar

area of the engine/nacelle in accordance with

Jetstream Service Bulletin J41–29–005,

Revision 1, dated August 12, 1994; or

Revision 2, dated August 30, 1994.

(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,

Standardization Branch, FAA, Transport

Airplane Directorate, ANM–113. 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 2: Information concerning the

existence of approved alternative methods of

compliance with this AD, if any, may be

obtained from the Standardization Branch,

ANM–113.

(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 airplane to

a location where the requirements of this AD

can be accomplished.

(d) The installation shall be done in

accordance with the following Jetstream

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

J41–29–005– .................................................................................................................................. 1, 4– 2 .................. Aug. 30, 1994.

Revision 2

August 30, 1994 ............................................................................................................................. 2, 3, 5–12– 1 .................. Aug. 12, 1994.

J41–29–005– .................................................................................................................................. 1–12– 1– ................ Aug. 12, 1994.

Revision 1

August 12, 1994

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 Jetstream Aircraft, Inc., P.O. Box 16029,

Dulles International Airport, Washington, DC

20041–6029. 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.

(e) This amendment becomes effective on

May 10, 1995.

Issued in Renton, Washington, on March

31, 1995.

Darrell M. Pederson,

Acting Manager, Transport Airplane

Directorate, Aircraft Certification Service.

[FR Doc. 95–8445 Filed 4–7–95; 8:45 am]

BILLING CODE 4910–13–U

14 CFR Part 39

[Docket No. 94–NM–169–AD; Amendment

39–9190; AD 95–08–01]

Airworthiness Directives; Jetstream

Model 4101 Airplanes

AGENCY: Federal Aviation

Administration, DOT.

ACTION: Final rule.

SUMMARY: This amendment adopts a

new airworthiness directive (AD),

applicable to certain Jetstream Model

4101 airplanes, that requires

modification of the spoiler system. This

amendment is prompted by reports of

fatigue failures of the tee fittings of the

spoiler bleed nipples. The actions

specified by this AD are intended to

ensure that the tee fittings do not fail,

and subsequently lead to loss of the

main system hydraulics.

DATES: Effective May 10, 1995.

The incorporation by reference of

certain publications listed in the

regulations is approved by the Director

of the Federal Register as of May 10,

1995.

ADDRESSES: The service information

referenced in this AD may be obtained

from Jetstream Aircraft, Inc., P.O. Box

16029, Dulles International Airport,

Washington, DC 20041–6029. This

information may be examined at the

Federal Aviation Administration (FAA),

Transport Airplane Directorate, Rules

Docket, 1601 Lind Avenue, SW.,

Renton, Washington; or at the Office of

the Federal Register, 800 North Capitol

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

FOR FURTHER INFORMATION CONTACT: Sam

Grober, Aerospace Engineer,

Standardization Branch, ANM–113,

FAA, Transport Airplane Directorate,

1601 Lind Avenue, SW., Renton,

Washington 98055–4056; telephone

(206) 227–1187; fax (206) 227–1320.