Federal Register / Vol. 60, No. 244 / Wednesday, December 20, 1995 / Rules and Regulations 65523

PART 39—AIRWORTHINESS

DIRECTIVES

1. The authority citation for part 39

continues to read as follows:

Authority: 49 USC 106(g), 40101, 40113,

44701.

§ 39.13 [Amended]

2. Section 39.13 is amended by

adding the following new airworthiness

directive:

95–26–07 Bombardier, Inc. (Formerly

Canadair): Amendment 39–9465. Docket

95–NM–238–AD.

Applicability: Model CL–600–2B19

(Regional Jet Series 100) series airplanes,

serial numbers 7003 through 7079 inclusive;

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 (e) of this AD 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 damage to the aileron hinge

fittings due to failure of the shear pins, which

could cause subsequent reduced

controllability of the airplane; accomplish

the following:

(a) Within 7 days after the effective date of

this AD, revise the Limitations Section of the

FAA-approved Airplane Flight Manual

(AFM) to include the following. This may be

accomplished by inserting a copy of this AD

in the AFM.

‘‘Before engine start, prior to the first flight

of each day, the flight crew or certificated

maintenance personnel shall perform a check

of the travel range of the aileron as follows:

Aileron—Check travel range (to approx 1⁄2

travel) using each hydraulic system in turn,

with the other hydraulic systems

depressurized.’’

Note 2: This AFM revision may also be

accomplished by inserting a copy of

Temporary Revision RJ/45, dated September

7, 1995, in the AFM. When this temporary

revision has been incorporated into general

revisions of the AFM, the general revisions

may be inserted in the AFM, provided the

information contained in the general

revisions is identical to that specified in

Temporary Revision RJ/45.

Note 3: Operators should note that

operation of the aircraft remains restricted to

the altitude and airspeed limits currently

specified in the FAA-approved AFM,

Revision 34, Chapter 5, Abnormal

Procedures, Section 13, Hydraulic Power,

Paragraphs ‘‘A’’ through ‘‘C’’ and ‘‘M’’

through ‘‘O.’’

(b) Perform a visual inspection to detect

damage of the shear link, the shear pin, and

the aileron attachment fitting, in accordance

with Canadair Regional Jet Alert Service

Bulletin S.B. A601R–27–058, Revision ‘A,’

dated September 8, 1995, and at the time

specified in paragraph (b)(1) or (b)(2) of this

AD, as applicable.

(1) For airplanes having serial numbers

7003 through 7054 inclusive: Inspect at the

next scheduled shear pin replacement, but no

later than 30 days after the effective date of

the AD.

(2) For airplanes having serial numbers

7055 through 7079 inclusive: Inspect at the

next scheduled shear pin replacement, but no

later than 400 flight hours after the effective

date of the AD.

(c) If no shear pin is found to be damaged

during the inspection required by paragraph

(b) of this AD, accomplish the requirements

of either paragraph (c)(1) or (c)(2), as

applicable, at the times specified:

(1) For airplanes having serial numbers

7003 through 7054 inclusive: At the next

scheduled shear pin replacement, but no

later than 400 flight hours after

accomplishing the inspection specified in

paragraph (b) of this AD, remove the aileron

flutter dampers, shear link, and pivot, in

accordance with Canadair Regional Jet Alert

Service Bulletin S.B. A601R–27–058,

Revision ‘A,’ dated September 8, 1995.

Following removal of the flutter dampers, the

shear pin replacement in accordance with the

FAA-approved maintenance program is not

required.

(2) For airplanes having serial numbers

7055 through 7079 inclusive: Repeat the

inspection required by paragraph (b) of this

AD at intervals not to exceed 400 flight

hours. At the next scheduled shear pin

replacement, but no later than 1,500 landings

after accomplishing the initial inspection

specified in paragraph (b) of this AD, remove

the aileron flutter dampers, shear link, and

pivot, in accordance with Canadair Regional

Jet Alert Service Bulletin S.B. A601R–27–

058, Revision ‘A,’ dated September 8, 1995.

Following removal of the flutter dampers, the

shear pin replacement in accordance with the

FAA-approved maintenance program is not

required.

(d) If any shear pin is found to be damaged

during the inspection required by paragraph

(b) of this AD, prior to further flight, remove

the aileron flutter dampers, shear link, and

pivot, in accordance with Canadair Regional

Jet Alert Service Bulletin S.B. A601R–27–

058, Revision ‘A,’ dated September 8, 1995.

Following removal of the flutter dampers,

shear pin replacement in accordance with the

FAA-approved maintenance program is not

required.

(e) If any aileron hinge fitting is found to

be damaged during the inspection required

by paragraph (b) of this AD, prior to further

flight, repair in accordance with Canadair

Regional Jet Alert Service Bulletin S.B.

A601R–27–058, Revision ‘A,’ dated

September 8, 1995.

(f) 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, New York

Aircraft Certification Office (ACO), FAA,

Engine and Propeller Directorate. Operators

shall submit their requests through an

appropriate FAA Principal Maintenance

Inspector, who may add comments and then

send it to the Manager, New York ACO.

Note 4: Information concerning the

existence of approved alternative methods of

compliance with this AD, if any, may be

obtained from the New York ACO.

(g) 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.

(h) The inspections, removal, and repair

shall be done in accordance with Canadair

Regional Jet Alert Service Bulletin S.B.

A601R–27–058, Revision ‘A,’ dated

September 8, 1995. 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 Bombardier, Inc., Canadair,

Aerospace Group, P.O. Box 6087, Station

Centreville, Quebec H3C 3G9, Canada.

Copies may be inspected at the FAA,

Transport Airplane Directorate, 1601 Lind

Avenue, SW., Renton, Washington; or at the

FAA, New York Aircraft Certification Office,

Engine and Propeller Directorate, 10 Fifth

Street, Third Floor, Valley Stream, New York;

or at the Office of the Federal Register, 800

North Capitol Street NW., suite 700,

Washington, DC.

(i) This amendment becomes effective on

January 4, 1996.

Issued in Renton, Washington, on

December 13, 1995.

Darrell M. Pederson,

Acting Manager, Transport Airplane

Directorate, Aircraft Certification Service.

[FR Doc. 95–30961 Filed 12–19–95; 8:45 am]

BILLING CODE 4910–13–U

14 CFR Part 39

[Docket No. 95–NM–245–AD; Amendment

39–9464; AD 95–26–06]

Airworthiness Directives; McDonnell

Douglas Model MD–11 Series

Airplanes

AGENCY: Federal Aviation

Administration, DOT.

ACTION: Final rule; request for

comments.

SUMMARY: This amendment adopts a

new airworthiness directive (AD) that is

applicable to certain McDonnell

Douglas Model MD–11 series airplanes.

This AD requires either that the control

circuit breaker of the left fuel pump

valve be opened and collared, or that

the Airplane Flight Manual (AFM) be

revised to prohibit autoland operation
65524 Federal Register / Vol. 60, No. 244 / Wednesday, December 20, 1995 / Rules and Regulations

below 100 feet above ground level

(AGL). Additionally, this action requires

an inspection of the fuel system control

panel (FSCP) to detect any mis-wiring,

and modification or replacement of the

FSCP. This AD also provides for an

optional terminating modification for

the requirements of the AD. This

amendment is prompted by a report of

improper wiring of the FSCP during

production of these airplanes. The

actions specified in this AD are

intended to prevent degradation of the

automatic landing system during flight

due to improper wiring of the FSCP.

DATES: Effective January 4, 1996.

The incorporation by reference of

certain publications listed in the

regulations is approved by the Director

of the Federal Register as of January 4,

1996.

Comments for inclusion in the Rules

Docket must be received on or before

February 20, 1996.

ADDRESSES: Submit comments in

triplicate to the Federal Aviation

Administration (FAA), Transport

Airplane Directorate, ANM–103,

Attention: Rules Docket No. 95–NM–

245–AD, 1601 Lind Avenue, SW.,

Renton, Washington 98055–4056.

The service information referenced in

this AD may be obtained from

McDonnell Douglas Corporation, 3855

Lakewood Boulevard, Long Beach,

California 90846, Attention: Technical

Publications Business Administration,

Department C1–L51 (2–60). This

information may be examined at the

FAA, Transport Airplane Directorate,

1601 Lind Avenue, SW., Renton,

Washington; or at the FAA, Los Angeles

Aircraft Certification Office, Transport

Airplane Directorate, 3960 Paramount

Boulevard, Lakewood, California; or at

the Office of the Federal Register, 800

North Capitol Street, NW., suite 700,

Washington, DC.

FOR FURTHER INFORMATION CONTACT:

Raymond Vakili, Aerospace Engineer,

Propulsion Branch, ANM–140L, FAA,

Los Angeles Aircraft Certification

Office, 3960 Paramount Boulevard,

Lakewood, California 90712; telephone

(310) 627–5262; fax (310) 627–5210.

SUPPLEMENTARY INFORMATION: The FAA

has received a report from McDonnell

Douglas indicating that improper wiring

of the fuel system control panel (FSCP)

on Model MD–11 airplanes was

detected during functional checks

performed during production.

Investigation revealed that the direct

current (DC) electrical busses, numbers

1 and 3, had been tied together; this

could lead to a single short of one bus,

which could adversely affect the

operation of the remaining bus. This

condition, if not corrected, could result

in degradation of the automatic landing

system during flight.

The FAA has reviewed and approved

McDonnell Douglas Alert Service

Bulletin MD11–28A081, dated

November 30, 1995, which describes

procedures to open and collar the

control circuit breaker, B1–458, of the

left fuel dump valve. This will reduce

the redundancy of the fuel dump system

and the fuel dump rate so that autoland

(dual land) operations can be

maintained. This alert service bulletin

also provides procedures for a

conducting a one-time visual inspection

of the FSCP to detect any mis-wiring,

and various necessary follow-on actions,

depending upon the result of the

inspection. Necessary follow-on actions

include re-identification, modification,

or replacement of the FSCP, if

necessary. (The McDonnell Douglas

alert service bulletin references

Honeywell Service Bulletin 4059024–

28–2, dated November 22, 1995, as an

additional source of service information

for inspection, re-identification, and

modification of the FSCP.)

Since an unsafe condition has been

identified that is likely to exist or

develop on other McDonnell Douglas

Model MD–11 series airplanes of the

same type design, this AD is being

issued to prevent degradation of the

automatic landing system during flight

due to improper wiring of the FSCP.

This AD first requires either (1) That the

control circuit breaker of the left fuel

pump valve be opened and collared, in

accordance with the McDonnell Douglas

alert service bulletin described

previously; or (2) that the FAAapproved Airplane Flight Manual

(AFM) be revised to prohibit autoland

operation below 100 feet above ground

level (AGL).

Second, this AD also requires a onetime visual inspection of the FSCP to

detect any mis-wiring, and reidentification, modification, or

replacement of the FSCP, if necessary.

These actions are required to be

accomplished in accordance with the

McDonnell Douglas alert service

bulletin described previously.

Additionally, operators must submit a

report of the results of the inspection to

the FAA.

This AD also provides for an optional

terminating action for the requirements

of the AD, which consists of replacing

the FSCP with a modified unit.

This is considered to be interim

action. The FAA may consider further

rulemaking action to require the

accomplishment of the optional

terminating action currently specified in

this AD. However, the proposed

compliance time for accomplishment of

that action is sufficiently long so that

prior notice and time for public

comment will be practicable.

Since a situation exists that requires

the immediate adoption of this

regulation, it is found that notice and

opportunity for prior public comment

hereon are impracticable, and that good

cause exists for making this amendment

effective in less than 30 days.

Comments Invited

Although this action is in the form of

a final rule that involves requirements

affecting flight safety and, thus, was not

preceded by notice and an opportunity

for public comment, comments are

invited on this rule. Interested persons

are invited to comment on this rule by

submitting such written data, views, or

arguments as they may desire.

Communications shall identify the

Rules Docket number and be submitted

in triplicate to the address specified

under the caption ADDRESSES. All

communications received on or before

the closing date for comments will be

considered, and this rule may be

amended in light of the comments

received. Factual information that

supports the commenter’s ideas and

suggestions is extremely helpful in

evaluating the effectiveness of the AD

action and determining whether

additional rulemaking action would be

needed.

Comments are specifically invited on

the overall regulatory, economic,

environmental, and energy aspects of

the rule that might suggest a need to

modify the rule. All comments

submitted will be available, both before

and after the closing date for comments,

in the Rules Docket for examination by

interested persons. A report that

summarizes each FAA-public contact

concerned with the substance of this AD

will be filed in the Rules Docket.

Commenters wishing the FAA to

acknowledge receipt of their comments

submitted in response to this rule must

submit a self-addressed, stamped

postcard on which the following

statement is made: ‘‘Comments to

Docket Number 95–NM–245–AD.’’ The

postcard will be date stamped and

returned to the commenter.

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
Federal Register / Vol. 60, No. 244 / Wednesday, December 20, 1995 / Rules and Regulations 65525

implications to warrant the preparation

of a Federalism Assessment.

The FAA has determined that this

regulation is an emergency regulation

that must be issued immediately to

correct an unsafe condition in aircraft,

and that it is not a ‘‘significant

regulatory action’’ under Executive

Order 12866. It has been determined

further that this action involves an

emergency regulation under DOT

Regulatory Policies and Procedures (44

FR 11034, February 26, 1979). If it is

determined that this emergency

regulation otherwise would be

significant under DOT Regulatory

Policies and Procedures, a final

regulatory evaluation will be prepared

and placed in the Rules Docket. A copy

of it, if filed, 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 USC 106(g), 40101, 40113,

44701.

§ 39.13 [Amended]

2. Section 39.13 is amended by

adding the following new airworthiness

directive:

95–26–06 McDonnell Douglas: Amendment

39–9464. Docket 95–NM–245–AD.

Applicability: Model MD–11 series

airplanes, manufacturer’s fuselage numbers

0447 through 0593 inclusive, 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 (e) of this AD 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 degradation of the automatic

landing system during flight due to improper

wiring of the fuel system control panel

(FSCP), accomplish the following:

(a) Within 15 days after the effective date

of this AD, accomplish the requirements of

either paragraph (a)(1) or (a)(2) of this AD.

(1) Revise the Limitations Section of the

FAA-approved Airplane Flight Manual

(AFM), page 5–4, Flight Guidance, Automatic

Landing Section, to include the following

statement. This may be accomplished by

inserting a copy of this AD in the AFM.

‘‘Autoland operation below 100 feet above

ground level (AGL) is prohibited. The

autopilot must be disconnected prior to

descent below 100 feet AGL.’’

(2) Open and collar the control circuit

breaker, B1–458, of the left fuel dump valve,

in accordance with Phase 1 of the

Accomplishment Instructions of McDonnell

Douglas Service Bulletin MD11–28A081,

dated November 30, 1995.

Note 2: McDonnell Douglas Alert Service

Bulletin MD11–28A081, dated November 30,

1995, references Honeywell Service Bulletin

4059024–28–2, dated November 22, 1995, for

specific service instructions.

(b) Within 60 days after the effective date

of this AD, perform a visual inspection to

determine if the wiring is mis-wired in the

fuel system control panel (FSCP), part

number 4059024–901, in accordance with

McDonnell Douglas Alert Service Bulletin

MD11–28A081, dated November 30, 1995.

(1) If the FSCP wiring is not mis-wired (the

measured resistance between connector pins

J1–T and J3–K is more than 100 ohms),

accomplish the requirements of either

paragraph (b)(1)(i) or (b)(1)(ii) of this AD:

(i) Continue to operate the airplane

provided that the actions specified in either

paragraph (a)(1) or (a)(2) have been

accomplished; or

(ii) Prior to further flight, re-identify the

FSCP, part number 4059024–901, to

incorporate modification letter ‘‘A’’ in the

FSCP identification plate, in accordance with

McDonnell Douglas Service Bulletin MD11–

28A081, dated November 30, 1995. This reidentification constitutes terminating action

for the requirements of this AD. [The AFM

revision as specified in paragraph (a)(1) of

this AD, if previously accomplished, may be

removed following this re-identification

action.]

(2) If the FSCP wiring is mis-wired (the

measured resistance between connectors J1–

T and J3–K is less than 100 ohms),

accomplish the requirements of either

paragraph (b)(2)(i) or (b)(2)(ii) of this AD.

(i) Continue to operate the airplane

provided that the actions specified in either

paragraph (a)(1) or (a)(2) have been

accomplished; or

(ii) Prior to further flight, either modify the

FSCP, part number 4059024–901; or replace

the FSCP, part number 4059024–901, with an

FSCP having part number 4059024–901 and

modification letter ‘‘A’’ in the FSCP

identification plate; in accordance with

McDonnell Douglas Service Bulletin MD11–

28A081, dated November 30, 1995. This

modification or replacement constitutes

terminating action for the requirements of

this AD. [The AFM revision as specified in

paragraph (a)(1) of this AD, if accomplished

previously, may be removed following this

modification/replacement.]

(c) Within 10 days after accomplishing the

visual inspection required by paragraph (b) of

this AD, submit a report of the inspection

results (both positive and negative findings)

to the Manager, FAA, Transport Airplane

Directorate, Los Angeles Aircraft Certification

Office (ACO), 3690 Paramount Boulevard,

Lakewood, California 90712; telephone (310)

627–5262; fax (310) 627–5210, Attention: Ray

Vakili, ANM–140L. Information collection

requirements contained in this regulation

have been approved by the Office of

Management and Budget (OMB) under the

provisions of the Paperwork Reduction Act of

1980 (44 U.S.C. 3501 et seq.) and have been

assigned OMB Control Number 2120–0056.

(d) Installation of an FSCP having part

number 4059024–901 and modification letter

‘‘A’’ in the FSCP identification plate, in

accordance with McDonnell Douglas Service

Bulletin MD11–28A081, dated November 30,

1995, constitutes terminating action for the

requirements of this AD.

(e) 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, Los

Angeles ACO, 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, Los Angeles ACO.

Note 3: Information concerning the

existence of approved alternative methods of

compliance with this AD, if any, may be

obtained from the Los Angeles ACO.

(f) 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.

(g) The actions shall be done in accordance

with McDonnell Douglas Alert Service

Bulletin MD11–28A081, dated November 30,

1995. 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 McDonnel Douglas Corporation, 3855

Lakewood Boulevard, Long Beach, California

90846. Attention: Technical Publications

Business Administration, Department C1–

L51 (2–60). Copies may be inspected at the

FAA, Transport Airplane Directorate, 1601

Lind Avenue, SW., Renton, Washington; or at

the FAA, Los Angeles Aircraft Certification

Office, Transport Airplane Directorate, 3960

Paramount Boulevard, Lakewood, California;

or at the Office of the Federal Register, 800

North Capitol Street, NW., suite 700,

Washington, DC.

(h) This amendment becomes effective on

January 4, 1996.
65526 Federal Register / Vol. 60, No. 244 / Wednesday, December 20, 1995 / Rules and Regulations

Issued in Renton, Washington, on

December 13, 1995.

Darrell M. Pederson,

Acting Manager, Transport Airplane

Directorate, Aircraft Certification Service.

[FR Doc. 95–30962 Filed 12–19–95; 8:45 am]

BILLING CODE 4910–13–U

14 CFR Part 71

[Airspace Docket No. 95–ASO–23]

Removal of Class E Airspace; Marietta,

GA

AGENCY: Federal Aviation

Administration (FAA), DOT.

ACTION: Final rule.

SUMMARY: This amendment removes

Class E airspace at Marietta, GA. The

required weather observations are not

available to Atlanta Tower, the ATC

facility having jurisdiction over the

Class E2 surface area airspace at the

Cobb County-McCollum Field Airport,

when the Cobb County-McCollum Field

Airport Traffic Control Tower is closed.

Therefore, the Class E2 surface area

airspace for the airport must be revoked.

EFFECTIVE DATE: 9091 UTC, February 29,

1996.

FOR FURTHER INFORMATION CONTACT:

Benny L. McGlamery, System

Management Branch, Air Traffic

Division, Federal Aviation

Administration, P.O. Box 20636,

Atlanta, Georgia 30320; telephone (404)

305–5570.

SUPPLEMENTARY INFORMATION:

History

It is a requirement that weather

observations shall be taken at the

surface area’s primary airport during the

times and dates a surface area is

designated, and further that the required

weather observation shall be transmitted

expeditiously to the ATC facility having

jurisdiction over the surface area. When

the Cobb County-McCollum Field

Airport Traffic Control Tower is closed

this requirement is not being met. This

action will eliminate the impact Class

E2 surface area airspace has placed on

users of the airspace in the vicinity of

the Cobb County-McCollum Field

Airport. This rule will become effective

on the date specified in the DATES

section. Since this action removes the

Class E2 surface area airspace, which

eliminates the impact of Class E2

surface area airspace on users of the

airspace in the vicinity of the Cobb

County-McCollum Field Airport, notice

and public procedure under 5 U.S.C.

553(b) are unnecessary.

The Rule

The amendment to part 71 of the

Federal Aviation Regulations (14 CFR

part 71) removes Class E airspace at

Marietta, GA. The required weather

observations are not available to Atlanta

Tower, the ATC facility having

jurisdiction over the Class E2 surface

area airspace at the Cobb CountyMcCollum Field Airport, when the Cobb

County-McCollum Field Airport Traffic

Control Tower is closed. Therefore, the

Class E2 surface area airspace for the

airport must be revoked.

The FAA has determined that this

regulation only involves an established

body of technical regulations for which

frequent and routine amendments are

necessary to keep them operationally

current. It, therefore, (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)

does not warrant preparation of a

regulatory evaluation as the anticipated

impact is so minimal. Since this is a

routine matter that will only affect air

traffic procedures and air navigation, it

is certified that this rule will not have

a significant economic impact on a

substantial number of small entities

under the criteria of the Regulatory

Flexibility Act.

List of Subjects in 14 CFR Part 71

Airspace, Incorporation by reference,

Navigation (air).

Adoption of the Amendment

In consideration of the foregoing, the

Federal Aviation Administration

amends 14 CFR part 71 as follows:

PART 71—[AMENDED]

1. The authority citation for 14 CFR

part 71 continues to read as follows:

Authority: 49 U.S.C. 106(g); 40103, 40113,

40120; EO 10854, 24 FR 9565, 3 CFR, 1959–

1963 Comp., p. 389; 14 CFR 11.69.

§ 71.1 [Amended]

2. The incorporation by reference in

14 CFR 71.1 of Federal Aviation

Administration Order 7400.9C, Airspace

Designations and Reporting Points,

dated August 17, 1995, and effective

September 16, 1995, is amended as

follows:

* * * * *

Paragraph 6002 Class E airspace areas

designated as a surface area for an airport.

* * * * *

ASO GA E2 Marietta, GA [Removed]

* * * * *

Issued in College Park, Georgia, on October

20, 1995.

Benny L. McGlamery,

Acting Manager, Air Traffic Division,

Southern Region.

[FR Doc. 95–30919 Filed 12–19–95; 8:45 am]

BILLING CODE 4910–13–M

DEPARTMENT OF COMMERCE

Bureau of Export Administration

15 CFR Parts 771, 779 and 799

[Docket No. 951211296–5296–01]

RIN 0694–AB30

Expansion of General License GLX and

GTDR

AGENCY: Bureau of Export

Administration.

ACTION: Final rule.

SUMMARY: This final rule revises the

Export Administration Regulations

(EAR) by expanding General License

GLX eligibility to include:

microprocessors with a composite

theoretical performance not exceeding

500 million theoretical operations per

second; memory integrated circuits;

certain digital integrated circuits; field

programmable gate arrays and logic

arrays; portable (personal) or mobile

radiotelephones not capable of end-toend encryption; and software to protect

against computer viruses.

In addition, revisions have been made

to expand eligibility for General License

GTDR with written assurance to include

virus protection software controlled

under ECCN 5D13A.c.

This rule also revises the list of

‘‘Additional Items Eligible for General

License GLX’’ included in a supplement

to the General License section of the

EAR to reflect the expansion of General

License GLX, and makes editorial

corrections to the permissive reexport

provisions for technical data.

The expansion of General License

GLX and GTDR to include additional

items will reduce paperwork and

licensing delays for exporters, and will

focus controls on exports that are of

direct strategic concern.

EFFECTIVE DATE: This rule is effective

December 20, 1995.

FOR FURTHER INFORMATION CONTACT:

For questions of a general nature, call

Nancy Crowe, Bureau of Export

Administration, Telephone: (202) 482–

2440.

For questions of a technical nature on

digital mobile telephones call Joseph

Young, Bureau of Export

Administration, Telephone: (202) 482–

4197.