Federal Register / Vol. 66, No. 161 / Monday, August 20, 2001 / Rules and Regulations 43463

26 U.S.C. 403(a). An eligible retirement

plan must be maintained in the United

States, which means one of the 50 states

or the District of Columbia.

[FR Doc. 01–20862 Filed 8–17–01; 8:45 am]

BILLING CODE 6760–01–P

FEDERAL RESERVE SYSTEM

12 CFR Part 226

Open-end Model Forms and Clauses

CFR Correction

In Title 12 of the Code of Federal

Regulations, parts 220 to 299, revised as

of January 1, 2001, in Part 226,

Appendix G is corrected by adding

Table G–10(C) as follows:

PART 226—TRUTH IN LENDING

(REGULATION Z)

* * * * *

Appendix G to Part 226—Open-End

Model Forms and Clauses

* * * * *

* * * * *

[FR Doc. 01–55525 Filed 8–17–01; 8:45 am]

BILLING CODE 1505–01–D

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 99–NM–367–AD; Amendment

39–12374; AD 2001–16–06]

RIN 2120–AA64

Airworthiness Directives; Boeing

Model 737–100 and –200 Series

Airplanes

AGENCY: Federal Aviation

Administration, DOT.

ACTION: Final rule.

SUMMARY: This amendment adopts a

new airworthiness directive (AD),

applicable to certain Boeing Model 737

series airplanes, that requires initial and

repetitive inspections of certain areas of

the wing spars to detect cracking or

corrosion; and follow-on corrective

actions and repair, if necessary. This

amendment is prompted by reports of

cracks and corrosion in the upper chord

of the front and rear spars of the wing

and reports of cracks propagating from

previously repaired areas. The actions

specified by this AD are intended to

detect and correct such cracking or

corrosion of the upper and lower chords

of the wing spars, which could result in

reduced structural integrity of the wing.

DATES: Effective September 24, 2001.

The incorporation by reference of

certain publications listed in the

regulations is approved by the Director

of the Federal Register as of September

24, 2001.

ADDRESSES: The service information

referenced in this AD may be obtained

from Boeing Commercial Airplane

Group, P.O. Box 3707, Seattle,

Washington 98124–2207. 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:

James Blilie, Aerospace Engineer,

Airframe Branch, ANM–120S, FAA,

Seattle Aircraft Certification Office,

1601 Lind Avenue, SW., Renton,

Washington 98055–4056; telephone

(425) 227–2131; fax (425) 227–1181.

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 Boeing

Model 737–100 and –200 series

airplanes was published in the Federal

Register on May 1, 2001 (66 FR 21700).

That action proposed to require initial

and repetitive inspections of certain

areas of the wing spars to detect

cracking or corrosion; and follow-on

corrective actions and repair, if

necessary.

Comments

Interested persons have been afforded

an opportunity to participate in the

making of this amendment. Due

consideration has been given to the

comments received.

The manufacturer recommends

adding certain wording for clarification

to the section of the Notice of Proposed

Rulemaking (NPRM) which is entitled

‘‘Explanation of Relevant Service

Information.’’ The FAA acknowledges

that the suggested wording is more

precise. However, since that wording

does not reappear in the AD itself, no

change is necessary.

The manufacturer also suggests that

the ‘‘Applicability’’ section be changed

to read ‘‘Model 737–100 and –200 series

airplanes, line number 1 through 310

inclusive, and 323; certificated in any

category.’’ The effect of the suggested

wording would be to clarify that the

next generation of 737 models is

specifically excluded. The FAA agrees