61910 Federal Register / Vol. 62, No. 224 / Thursday, November 20, 1997 / Rules and Regulations

Compliance: Required within the next 200

hours time-in-service (TIS) after the effective

date of this AD, unless already accomplished.

To prevent a loss of vacuum to

depressurize the airplane cabin, which could

result in personal injury to the door operator;

and to prevent malfunction of the de-ice

indicator system which could cause the pilot

to unnecessarily exit icing conditions,

accomplish the following:

(a) Inspect for collapse, deformation, and

proper routing of the gray, blue, or clear

pneumatic pressurization control system

tubes and the de-ice indicator pneumatic

tubing located forward of the co-pilot’s right

outboard rudder pedal in accordance with

the ACCOMPLISHMENT INSTRUCTIONS

section and Figure 1 of the Raytheon Aircraft

Company (Raytheon) Mandatory Service

Bulletin (SB) No. 2676, Issued: January 1997.

(b) If any of this tubing is deformed or

collapsed, prior to further flight, replace the

damaged section of tube with new nylon

tubing, then use aluminum tubing and hose

clamps to secure and re-route the tubing at

least 8 inches away from the discharge

opening of the co-pilot’s foot warmer outlet

in accordance with the ACCOMPLISHMENT

INSTRUCTIONS section and Figure 2 of the

Raytheon Mandatory SB No. 2676, Issued:

January 1997.

(c) If there is no evidence of damage to the

tubing, prior to further flight, re-route and

secure the tubing as specified in paragraph

(b) of this AD in accordance with the

ACCOMPLISHMENT INSTRUCTIONS

section of the Raytheon Mandatory SB No.

2676, Issued: January 1997.

(d) 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.

(e) An alternative method of compliance or

adjustment of the compliance time that

provides an equivalent level of safety may be

approved by the Manager, Wichita Aircraft

Certification Office, 1801 Airport Road,

Room 100, Mid-Continent Airport, Wichita,

Kansas 67209. The request shall be

forwarded through an appropriate FAA

Maintenance Inspector, who may add

comments and then send it to the Manager,

Wichita Aircraft Certification Office.

Note 2: Information concerning the

existence of approved alternative methods of

compliance with this AD, if any, may be

obtained from Wichita Aircraft Certification

Office.

(f) The inspections, modifications, and

replacements required by this AD shall be

done in accordance Raytheon Aircraft

Company Mandatory Service Bulletin No.

2676, Issued: January 1997. 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

Raytheon Aircraft Company, P.O. Box 85,

Wichita, Kansas 67201–0085. Copies may be

inspected at the FAA, Central Region, Office

of the Regional Counsel, Room 1558, 601 E.

12th Street, Kansas City, Missouri, or at the

Office of the Federal Register, 800 North

Capitol Street, NW., suite 700, Washington,

DC.

(g) This amendment (39–10207) becomes

effective on December 29, 1997.

Issued in Kansas City, Missouri, on

November 7, 1997.

Larry D. Malir,

Acting Manager, Small Airplane Directorate,

Aircraft Certification Service.

[FR Doc. 97–30057 Filed 11–19–97; 8:45 am]

BILLING CODE 4910–13–U

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 97–NM–198–AD; Amendment

39–10210; AD 97–24–03]

RIN 2120–AA64

Airworthiness Directives; Dassault

Model Falcon 2000 Series Airplanes

AGENCY: Federal Aviation

Administration, DOT.

ACTION: Final rule.

SUMMARY: This amendment adopts a

new airworthiness directive (AD),

applicable to certain Dassault Model

Falcon 2000 series airplanes, that

requires a revision to the Limitations

section of the FAA-approved Airplane

Flight Manual (AFM) to limit the

allowed loads in the baggage

compartment aft of the center baggage

net. This AD also requires replacement

of the center baggage net in the baggage

compartment with a net having

reinforced straps, which terminates the

requirement for the AFM revision. This

amendment is prompted by a report

indicating that the center baggage net

cannot sustain design loads in the event

of an accident. The actions specified by

this AD are intended to prevent injury

to passengers, as a result of inadequate

breaking strength of the baggage net, in

the event of an accident.

DATES: Effective December 26, 1997.

The incorporation by reference of

certain publications listed in the

regulations is approved by the Director

of the Federal Register as of December

26, 1997.

ADDRESSES: The service information

referenced in this AD may be obtained

from Dassault Falcon Jet Corporation,

Teterboro Airport, P.O. Box 2000, South

Hackensack, New Jersey 07606.

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:

International Branch, ANM–116, FAA,

Transport Airplane Directorate, 1601

Lind Avenue, SW., Renton, Washington

98055–4056; telephone (425) 227–2110;

fax (425) 227–1149.

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 Dassault

Model Falcon 2000 series airplanes was

published in the Federal Register on

September 15, 1997 (62 FR 48187). That

action proposed to require a revision to

the Limitations section of the FAAapproved Airplane Flight Manual

(AFM) to limit the allowed loads in the

baggage compartment aft of the center

baggage net. The AD also proposed to

require replacement of the center

baggage net in the baggage compartment

with a net having reinforced straps,

which would terminate the requirement

for the AFM revision.

Comments

Interested persons have been afforded

an opportunity to participate in the

making of this amendment. No

comments were submitted in response

to the proposal or the FAA’s

determination of the cost to the public.

Conclusion

The FAA has determined that air

safety and the public interest require the

adoption of the rule as proposed.

Cost Impact

The FAA estimates that 20 Model

Falcon 2000 series airplanes of U.S.

registry will be affected by this AD, that

it will take approximately 1 work hour

per airplane to accomplish the

replacement, and that the average labor

rate is $60 per work hour. Required

parts will cost approximately $520 per

airplane. Based on these figures, the cost

impact of the AD on U.S. operators is

estimated to be $11,600, or $580 per

airplane.

It will take approximately 1 work

hour per airplane to accomplish the

AFM revision, at an average labor rate

of $60 per work hour. Based on these

figures, the cost impact on U.S.

operators of the AFM revision required

by this AD is estimated to be $1,200, or

$60 per airplane.

Based on the above figures, the total

cost impact on U.S. operators of the

replacement and AFM revision is

estimated to be $12,800, or $640 per

airplane.

The cost impact figures discussed

above are based on assumptions that no

operator has yet accomplished any of

the requirements of this AD action, and

that no operator would accomplish
Federal Register / Vol. 62, No. 224 / Thursday, November 20, 1997 / Rules and Regulations 61911

those actions in the future if this AD

were not adopted.

Regulatory Impact

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. 106(g), 40113, 44701.

§ 39.13 [Amended]

2. Section 39.13 is amended by

adding the following new airworthiness

directive:

97–24–03 Dassault Aviation: Amendment

39–10210. Docket 97–NM–198–AD.

Applicability: Model Falcon 2000

airplanes, serial numbers 2 through 31

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

otherwise 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 request approval for an

alternative method of compliance in

accordance with paragraph (c) of this AD.

The request should include an assessment of

the effect of the modification, alteration, or

repair on the unsafe condition addressed by

this AD; and, if the unsafe condition has not

been eliminated, the request should include

specific proposed actions to address it.

Compliance: Required as indicated, unless

accomplished previously.

To prevent injury to passengers as a result

of inadequate breaking strength of the

baggage net, accomplish the following:

(a) Within 60 days after the effective date

of this AD, revise the Limitations section of

the FAA-approved Airplane Flight Manual

(AFM) by inserting into the AFM a copy of

Falcon 2000 AFM Temporary Change No. 31

(undated).

Note 2: The revision of the AFM required

by this paragraph may be accomplished by

inserting a copy of Falcon 2000 AFM

Temporary Change No. 31 in the AFM. When

this temporary change has been incorporated

into general revisions of the AFM, the general

revisions may be inserted in the AFM,

provided that the information contained in

the general revisions is identical to that

specified in Falcon 2000 AFM Temporary

Change No. 31.

(b) Within 6 months after the effective date

of this AD, replace the center baggage net in

the baggage compartment with a net having

reinforced straps, in accordance with

Dassault Service Bulletin F2000–76 (F2000–

25–2), dated December 11, 1996. After this

replacement is accomplished, the AFM

revision required by paragraph (a) of this AD

may be removed from the AFM.

(c) 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,

International Branch, ANM–116, 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, International Branch,

ANM–116.

Note 3: Information concerning the

existence of approved alternative methods of

compliance with this AD, if any, may be

obtained from the International Branch,

ANM–116.

(d) 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.

(e) The actions shall be done in accordance

with Falcon 2000 Airplane Flight Manual

Temporary Change No. 31 (undated), and

Dassault Service Bulletin F2000–76 (F2000–

25–2), dated December 11, 1996. 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

Dassault Falcon Jet Corporation, Teterboro

Airport, P.O. Box 2000, South Hackensack,

New Jersey 07606. 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.

Note 4: The subject of this AD is addressed

French airworthiness directive 96–291–

002(B), dated December 4, 1996.

(f) This amendment becomes effective on

December 26, 1997.

Issued in Renton, Washington, on

November 10, 1997.

Darrell M. Pederson,

Acting Manager, Transport Airplane

Directorate, Aircraft Certification Service.

[FR Doc. 97–30301 Filed 11–19–97; 8:45 am]

BILLING CODE 4910–13–U

DEPARTMENT OF HEALTH AND

HUMAN SERVICES

Food and Drug Administration

21 CFR Part 558

New Animal Drugs for Use in Animal

Feeds; Clopidol and Bacitracin Zinc

AGENCY: Food and Drug Administration,

HHS.

ACTION: Final rule.

SUMMARY: The Food and Drug

Administration (FDA) is amending the

animal drug regulations to reflect

approval of an abbreviated new animal

drug application (ANADA) filed by

Alpharma Inc. The ANADA provides for

using approved clopidol and bacitracin

zinc Type A medicated articles to make

Type C medicated broiler chicken feeds

used for prevention of coccidiosis,

improved feed efficiency, and increased

rate of weight gain.

EFFECTIVE DATE: November 20, 1997.

FOR FURTHER INFORMATION CONTACT:

Jeffrey M. Gilbert, Center for Veterinary

Medicine (HFV–128), Food and Drug

Administration, 7500 Standish Pl.,

Rockville, MD 20855, 301–594–1602.

SUPPLEMENTARY INFORMATION: Alpharma

Inc., One Executive Dr., P.O. Box 1399,

Fort Lee, NJ 07024, is sponsor of

ANADA 200–218 that provides for

combining approved clopidol and

bacitracin zinc Type A medicated

articles to make Type C medicated feeds

for broilers containing clopidol 113.5

grams per ton (g/t) and bacitracin zinc

5 to 25 g/t. The Type C medicated feed

is used as an aid in the prevention of

coccidiosis caused by Eimeria tenella, E.

necatrix, E. acervulina, E. brunetti, E.

mivati, and E. maxima, and for

increased rate of weight gain and

improved feed efficiency.

Alpharma Inc.’s ANADA 200–218 is

approved as a generic copy of Rhone-