Federal Register / Vol. 71, No. 21 / Wednesday, February 1, 2006 / Rules and Regulations 5159 

carton of assessable oranges, grapefruit, 

tangerines, and tangelos was then 

determined by dividing the total 

recommended budget by the quantity of 

assessable Florida citrus, estimated at 24 

million 4⁄5 bushel cartons for the 2005–

06 season taking into consideration the 

availability of reserve funds and interest 

income. This assessment rate will yield 

approximately $17,000 under 

anticipated budgeted expenses with the 

deficit funds to be drawn from reserves 

and interest income. 

A review of historical information and 

preliminary information pertaining to 

the upcoming 2005–06 fiscal period 

indicates that the grower price for the 

2005–06 season could range between 

$1.23 and $7.18 per 4⁄5 bushel of 

oranges, grapefruit, tangerines, and 

tangelos. Therefore, the estimated 

assessment revenue for the 2005–06 

fiscal period as a percentage of total 

grower revenue could range between .11 

and .65 percent. 

This action increases the assessment 

obligation imposed on handlers. While 

assessments impose some additional 

costs on handlers, the costs are minimal 

and uniform on all handlers. Some of 

the additional costs may be passed on 

to producers. However, these costs 

would be offset by the benefits derived 

by the operation of the marketing order. 

In addition, the Committee’s meeting 

was widely publicized throughout the 

Florida citrus industry and all interested 

persons were invited to attend the 

meeting and participate in Committee 

deliberations on all issues. Like all 

Committee meetings, the December 16, 

2005 meeting was a public meeting and 

all entities, both large and small, were 

able to express views on this issue. 

Finally, interested persons are invited to 

submit information on the regulatory 

and informational impacts of this action 

on small businesses. 

This action imposes no additional 

reporting or recordkeeping requirements 

on either small or large Florida citrus 

handlers. As with all Federal marketing 

order programs, reports and forms are 

periodically reviewed to reduce 

information requirements and 

duplication by industry and public 

sector agencies. 

USDA has not identified any relevant 

Federal rules that duplicate, overlap, or 

conflict with this rule. 

A small business guide on complying 

with fruit, vegetable, and specialty crop 

marketing agreements and orders may 

be viewed at: http://www.ams.usda.gov/ 

fv/moab.html. Any questions about the 

compliance guide should be sent to Jay 

Guerber at the previously mentioned 

address in the FOR FURTHER INFORMATION

CONTACT section. 

After consideration of all relevant 

material presented, including the 

information and recommendation 

submitted by the Committee and other 

available information, it is hereby found 

that this rule, as hereinafter set forth, 

will tend to effectuate the declared 

policy of the Act. 

Pursuant to 5 U.S.C. 553, it is also 

found and determined upon good cause 

that it is impracticable, unnecessary, 

and contrary to the public interest to 

give preliminary notice prior to putting 

this rule into effect, and that good cause 

exists for not postponing the effective 

date of this rule until 30 days after 

publication in the Federal Register 

because: (1) The 2005–06 fiscal period 

began August 1, 2005, and the 

marketing order requires that the rate of 

assessment for each fiscal period apply 

to all assessable Florida citrus handled 

during such fiscal period; (2) the 

Committee needs to have sufficient 

funds to pay its expenses which are 

incurred on a continuous basis; (3) 

handlers are aware of this action which 

was unanimously recommended by the 

Committee at a public meeting and is 

similar to other assessment rate actions 

issued in past years; and (4) this interim 

final rule provides a 60-day comment 

period, and all comments timely 

received will be considered prior to 

finalization of this rule. 

List of Subjects in 7 CFR Part 905 

Grapefruit, Oranges, Tangelos, 

Tangerines, Marketing agreements, 

Reporting and recordkeeping 

requirements. 

■ For the reasons set forth in the 

preamble, 7 CFR part 905 is amended as 

follows: 

PART 905—ORANGES, GRAPEFRUIT, 

TANGERINES, AND TANGELOS 

GROWN IN FLORIDA 

■ 1. The authority citation for 7 CFR 

part 905 continues to read as follows: 

Authority: 7 U.S.C. 601–674. 

■ 2. Section 905.235 is revised to read 

as follows: 

§ 905.235 Assessment rate. 

On and after August 1, 2005, an 

assessment rate of $0.008 per 4⁄5 bushel 

carton or equivalent is established for 

Florida citrus covered under the order. 

Dated: January 27, 2006. 

Lloyd C. Day, 

Administrator, Agricultural Marketing 

Service. 

[FR Doc. 06–947 Filed 1–30–06; 9:06 am] 

BILLING CODE 3410–02–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2006–23716; Directorate 

Identifier 2006–NM–008–AD; Amendment 

39–14466; AD 2006–03–02] 

RIN 2120–AA64 

Airworthiness Directives; Dassault 

Model Falcon 2000 and Falcon 2000EX 

Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule; request for 

comments. 

SUMMARY: The FAA is adopting a new 

airworthiness directive (AD) for certain 

Dassault Model Falcon 2000 and Falcon 

2000EX airplanes. For all airplanes, this 

AD requires, among other actions, doing 

an inspection for damage of the feeder 

cables, and corrective actions if 

necessary; and installing a protective 

plate on the feeder cables. For certain 

airplanes, this AD also requires rerouting the wiring on the cockpit 

protector; drilling holes in the cockpit 

protector; and clamping the feeder 

cables; as applicable. This AD results 

from a drawing review and further 

associated inspections that highlighted a 

potential chafing risk between the third 

crew member’s oxygen mask box and 

feeder cables routed in the area. We are 

issuing this AD to prevent chafing 

between the subject oxygen mask box 

and the adjacent feeder cables, which 

could generate smoke or fire in the 

cockpit that could be fanned by oxygen 

leakage from the oxygen mask box. 

DATES: This AD becomes effective 

February 16, 2006. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in the AD 

as of February 16, 2006. 

We must receive comments on this 

AD by April 3, 2006. 

ADDRESSES: Use one of the following 

addresses to submit comments on this 

AD. 

• DOT Docket Web site: Go to 

http://dms.dot.gov and follow the 

instructions for sending your comments 

electronically. 

• Government-wide rulemaking Web 

site: Go to http://www.regulations.gov 

and follow the instructions for sending 

your comments electronically. 

• Mail: Docket Management Facility; 

U.S. Department of Transportation, 400 

Seventh Street, SW., Nassif Building, 

Room PL–401, Washington, DC 20590. 


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5160 Federal Register / Vol. 71, No. 21 / Wednesday, February 1, 2006 / Rules and Regulations 

• Fax: (202) 493–2251. 

• Hand Delivery: Room PL–401 on 

the plaza level of the Nassif Building, 

400 Seventh Street, SW., Washington, 

DC, between 9 a.m. and 5 p.m., Monday 

through Friday, except Federal holidays. 

Contact Dassault Falcon Jet, P.O. Box 

2000, South Hackensack, New Jersey 

07606, for service information identified 

in this AD. 

FOR FURTHER INFORMATION CONTACT: Tom 

Rodriguez, Aerospace Engineer, 

International Branch, ANM–116, 

Transport Airplane Directorate, FAA, 

1601 Lind Avenue, SW., Renton, 

Washington 98055–4056; telephone 

(425) 227–1137; fax (425) 227–1149. 

SUPPLEMENTARY INFORMATION: 

Discussion 

The European Aviation Safety Agency 

(EASA) notified us that an unsafe 

condition may exist on certain Dassault 

Model Falcon 2000 and Falcon 2000EX 

airplanes. The EASA advises that a 

drawing review and further associated 

inspections have highlighted a potential 

chafing risk between the third crew 

member’s oxygen mask box, which is 

optional, installed in the cockpit ceiling, 

and feeder cables routed in the area. 

This condition, if not corrected, could 

generate smoke or fire in the cockpit 

that could be fanned by oxygen leakage 

from the oxygen mask box. 

Relevant Service Information 

Dassault has issued the service 

bulletins in the following table: 

TABLE.—SERVICE BULLETINS

Dassault service bulletin— Dated— For model— 

F2000EX–92 ...................................................................... December 22, 2005 .......................................................... Falcon 2000EX airplanes. 

F2000–332 ........................................................................ December 22, 2005 .......................................................... Falcon 2000 airplanes. 

Both service bulletins describe the 

following procedures for both airplane 

models, except as indicated: 

• Coating nuts and rivets with epoxy 

resin if necessary. 

• Doing a general visual inspection 

for damage of the feeder cables coming 

from the essential and A1 buses, and 

applicable corrective actions if 

necessary. The corrective actions 

include repairing any damaged feeder 

cable having a damaged conductor, and 

wrapping with Roundit sheath any 

damaged feeder cable that does not 

affect the conductor; as applicable. 

• Re-routing the wiring on the cockpit 

protector, and bonding the applicable 

supports with epoxy resin (for all Model 

Falcon 2000 airplanes and for certain 

Model Falcon 2000EX airplanes). 

• Installing a protective plate on the 

feeder cables. 

For certain airplanes, Dassault Service 

Bulletin F2000EX–92 also describes 

procedures for drilling holes in the 

cockpit protector located between the 

headline and the skin, and clamping the 

feeder cables coming from the essential, 

A1, and A2 buses. 

Accomplishing the actions specified 

in the service information is intended to 

adequately address the unsafe 

condition. The EASA mandated the 

service bulletins and issued emergency 

airworthiness directive 2006–0003, 

dated January 5, 2006, to ensure the 

continued airworthiness of these 

airplanes in the European Union. 

FAA’s Determination and Requirements 

of This AD 

These airplane models are 

manufactured in France and are type 

certificated for operation in the United 

States under the provisions of § 21.29 of 

the Federal Aviation Regulations (14 

CFR 21.29) and the applicable bilateral 

airworthiness agreement. Pursuant to 

FAA Order 8100.14A, ‘‘Interim 

Procedures for Working with the 

European Community on Airworthiness 

Certification and Continued 

Airworthiness,’’ dated August 12, 2005, 

the EASA has kept the FAA informed of 

the situation described above. We have 

examined the EASA’s findings, 

evaluated all pertinent information, and 

determined that we need to issue an AD 

for products of this type design that are 

certificated for operation in the United 

States. 

Therefore, we are issuing this AD to 

prevent chafing between the third crew 

member’s oxygen mask box and feeder 

cables routed in the area, which could 

generate smoke or fire in the cockpit 

that could be fanned by oxygen leakage 

from the oxygen mask box. This AD 

requires accomplishing the actions 

specified in the service information 

described previously. 

Difference Between the EASA’s 

Emergency Airworthiness Directive and 

This AD 

The applicability of the EASA’s 

emergency airworthiness directive 

2006–0003 excludes airplanes on which 

Dassault Modification M2738 (reference 

Dassault Service Bulletins F2000EX–92 

and F2000–332) was done. However, we 

have not excluded those airplanes in the 

applicability of this AD; rather, this AD 

includes a requirement to accomplish 

the actions specified in those service 

bulletins, as applicable. This 

requirement will ensure that the actions 

specified in the applicable service 

bulletin and required by this AD are 

done on all affected airplanes. Operators 

must continue to operate the airplane in 

the configuration required by this AD 

unless an alternative method of 

compliance is approved. This difference 

has been coordinated with the EASA. 

FAA’s Determination of the Effective 

Date 

An unsafe condition exists that 

requires the immediate adoption of this 

AD; therefore, providing notice and 

opportunity for public comment before 

the AD is issued, is impracticable, and 

good cause exists to make this AD 

effective in less than 30 days. 

Comments Invited 

This AD is a final rule that involves 

requirements that affect flight safety and 

was not preceded by notice and an 

opportunity for public comment; 

however, we invite you to submit any 

relevant written data, views, or 

arguments regarding this AD. Send your 

comments to an address listed in the 

ADDRESSES section. Include ‘‘Docket No. 

FAA–2006–23716; Directorate Identifier 

2006–NM–008–AD’’ at the beginning of 

your comments. We specifically invite 

comments on the overall regulatory, 

economic, environmental, and energy 

aspects of the AD that might suggest a 

need to modify it. 

We will post all comments we 

receive, without change, to http:// 

dms.dot.gov, including any personal 

information you provide. We will also 

post a report summarizing each 

substantive verbal contact with FAA 

personnel concerning this AD. Using the 

search function of that Web site, anyone 

can find and read the comments in any 

of our dockets, including the name of 

the individual who sent the comment 

(or signed the comment on behalf of an 

association, business, labor union, etc.). 

You may review the DOT’s complete 

Privacy Act Statement in the Federal 

Register published on April 11, 2000 


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Federal Register / Vol. 71, No. 21 / Wednesday, February 1, 2006 / Rules and Regulations 5161 

(65 FR 19477–78), or you may visit 

http://dms.dot.gov. 

Examining the Docket 

You may examine the AD docket on 

the Internet at http://dms.dot.gov, or in 

person at the Docket Management 

Facility office between 9 a.m. and 5 

p.m., Monday through Friday, except 

Federal holidays. The Docket 

Management Facility office (telephone 

(800) 647–5227) is located on the plaza 

level of the Nassif Building at the DOT 

street address stated in the ADDRESSES

section. Comments will be available in 

the AD docket shortly after the Docket 

Management System receives them. 

Authority for This Rulemaking 

Title 49 of the United States Code 

specifies the FAA’s authority to issue 

rules on aviation safety. Subtitle I, 

Section 106, describes the authority of 

the FAA Administrator. Subtitle VII, 

Aviation Programs, describes in more 

detail the scope of the Agency’s 

authority. 

We are issuing this rulemaking under 

the authority described in subtitle VII, 

part A, subpart III, section 44701, 

‘‘General requirements.’’ Under that 

section, Congress charges the FAA with 

promoting safe flight of civil aircraft in 

air commerce by prescribing regulations 

for practices, methods, and procedures 

the Administrator finds necessary for 

safety in air commerce. This regulation 

is within the scope of that authority 

because it addresses an unsafe condition 

that is likely to exist or develop on 

products identified in this rulemaking 

action. 

Regulatory Findings 

We have determined that this AD will 

not have federalism implications under 

Executive Order 13132. This AD will 

not have a substantial direct effect 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. 

For the reasons discussed above, I 

certify that the regulation: 

1. Is not a ‘‘significant regulatory 

action’’ under Executive Order 12866; 

2. Is not a ‘‘significant rule’’ under the 

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. 

We prepared a regulatory evaluation 

of the estimated costs to comply with 

this AD and placed it in the AD docket. 

See the ADDRESSES section for a location 

to examine the regulatory evaluation. 

List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation 

safety, Incorporation by reference, 

Safety. 

Adoption of the Amendment 

■ Accordingly, under the authority 

delegated to me by the Administrator, 

the FAA amends 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. The Federal Aviation 

Administration (FAA) amends § 39.13 

by adding the following new 

airworthiness directive (AD): 

2006–03–02 Dassault Aviation: 

Amendment 39–14466. Docket No. 

FAA–2006–23716; Directorate Identifier 

2006–NM–008–AD. 

Effective Date 

(a) This AD becomes effective February 16, 

2006. 

Affected ADs 

(b) None. 

Applicability 

(c) This AD applies to the Dassault 

airplanes in Table 1 of this AD, certificated 

in any category; equipped with a third crew 

member passenger-type oxygen mask on the 

cockpit ceiling; excluding those airplanes on 

which Dassault Modification M2739 has been 

done in production. 

TABLE 1.—APPLICABILITY

Model Serial numbers 

(1) Falcon 2000 airplanes.1 through 226 inclusive. 

(2) Falcon 2000EX 

airplanes.

1 through 64 inclusive 

Unsafe Condition 

(d) This AD results from a drawing review 

and further associated inspections that 

highlighted a potential chafing risk between 

the third crew member’s oxygen mask box 

and feeder cables routed in the area. We are 

issuing this AD to prevent chafing between 

the subject oxygen mask box and the adjacent 

feeder cables, which could generate smoke or 

fire in the cockpit that could be fanned by 

oxygen leakage from the oxygen mask box. 

Compliance 

(e) You are responsible for having the 

actions required by this AD performed within 

the compliance times specified, unless the 

actions have already been done. 

Service Bulletins 

(f) The term ‘‘service bulletin,’’ as used in 

this AD, means the Accomplishment 

Instructions of the applicable service bulletin 

in Table 2 of this AD. 

TABLE 2.— SERVICE BULLETINS

Dassault service bulletin— Dated— For model—

(1) F2000–332 ................................................................... December 22, 2005 .......................................................... Falcon 2000 airplanes. 

(2) F2000EX–92 ................................................................ December 22, 2005 .......................................................... Falcon 2000EX airplanes. 

Apply Epoxy Resin, Inspect for Damaged 

Feeder Cables, Re-Route Wiring, and Install 

of a Protective Plate 

(g) Within 30 days or 30 flight cycles after 

the effective date of this AD, whichever 

occurs first, do the applicable actions in 

Table 3 of this AD in accordance with the 

service bulletin. 

TABLE 3.—REQUIRED ACTIONS

For— Required actions 

(1) All airplanes ........................................................................................ Coat nuts and rivets with epoxy resin. 

(2) All airplanes ........................................................................................ Do a general visual inspection for damage of the feeder cables coming 

from the essential and A1 buses. 


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5162 Federal Register / Vol. 71, No. 21 / Wednesday, February 1, 2006 / Rules and Regulations 

TABLE 3.—REQUIRED ACTIONS—Continued 

For— Required actions 

(3) Model Falcon 2000EX airplanes, serial number 6 and 28 through 64 

inclusive.

Drill holes in the cockpit protector located between the headline and 

the skin, and clamp the feeder cables coming from the essential, A1, 

and A2 buses. 

(4) All Model Falcon 2000 airplanes and for Model Falcon 2000EX airplanes, serial numbers 1 through 5 inclusive and 7 through 27 inclusive.Re-route the wiring on the cockpit protector, and bond the applicable 

supports with epoxy resin. 

(5) All airplanes ........................................................................................ Install a protective plate on the feeder cables. 

Note 1: For the purposes of this AD, a 

general visual inspection is: ‘‘A visual 

examination of an interior or exterior area, 

installation, or assembly to detect obvious 

damage, failure, or irregularity. This level of 

inspection is made from within touching 

distance unless otherwise specified. A mirror 

may be necessary to ensure visual access to 

all surfaces in the inspection area. This level 

of inspection is made under normally 

available lighting conditions such as 

daylight, hangar lighting, flashlight, or 

droplight and may require removal or 

opening of access panels or doors. Stands, 

ladders, or platforms may be required to gain 

proximity to the area being checked.’’

Corrective Actions 

(h) If any damaged feeder cable is detected 

during the inspection required by paragraph 

(g)(2) of this AD, before further flight, do the 

applicable corrective actions in accordance 

with the service bulletin. 

No Reporting 

(i) Although the service bulletins 

referenced in this AD specifies to submit 

certain information to the manufacturer, this 

AD does not include that requirement. 

Alternative Methods of Compliance 

(AMOCs) 

(j)(1) The Manager, International Branch, 

ANM–116, Transport Airplane Directorate, 

FAA, has the authority to approve AMOCs 

for this AD, if requested in accordance with 

the procedures found in 14 CFR 39.19. 

(2) Before using any AMOC approved in 

accordance with § 39.19 on any airplane to 

which the AMOC applies, notify the 

appropriate principal inspector in the FAA 

Flight Standards Certificate Holding District 

Office. 

Related Information 

(k) The European Aviation Safety Agency’s 

emergency airworthiness directive 2006–

0003, dated January 5, 2006, also addresses 

the subject of this AD. 

Material Incorporated by Reference 

(l) You must use the applicable service 

bulletin in Table 4 of this AD to perform the 

actions that are required by this AD, unless 

the AD specifies otherwise. The Director of 

the Federal Register approved the 

incorporation by reference of these 

documents in accordance with 5 U.S.C. 

552(a) and 1 CFR part 51. Contact Dassault 

Falcon Jet, P.O. Box 2000, South Hackensack, 

New Jersey 07606, for a copy of this service 

information. You may review copies at the 

Docket Management Facility, U.S. 

Department of Transportation, 400 Seventh 

Street SW., Room PL–401, Nassif Building, 

Washington, DC; on the Internet at http:// 

dms.dot.gov; or at the National Archives and 

Records Administration (NARA). For 

information on the availability of this 

material at the NARA, call (202) 741–6030, 

or go to http://www.archives.gov/ 

federal_register/code_of_federal_regulations/

ibr_locations.html. 

TABLE 4.—MATERIAL INCORPORATED

BY REFERENCE

Dassault service bulletin— Dated—

(1) F2000–332 .......... December 22, 2005. 

(2) F2000EX–92 ........ December 22, 2005. 

Issued in Renton, Washington, on January 

23, 2006. 

Ali Bahrami, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 06–824 Filed 1–31–06; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2005–23031; Directorate 

Identifier 2005–NE–41–AD; Amendment 39–

14467; AD 2006–03–03] 

RIN 2120–AA64 

Airworthiness Directives; Rolls-Royce 

plc RB211 Trent 553–61, 553A2–61, 

556–61, 556A2–61, 556B–61, 556B2–61, 

560–61, and 560A2–61 Turbofan 

Engines 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule; request for 

comments. 

SUMMARY: The FAA is adopting a new 

airworthiness directive (AD) for certain 

Rolls-Royce plc (RR) RB211 Trent 553–

61, 553A2–61, 556–61, 556A2–61, 

556B–61, 556B2–61, 560–61, and 

560A2–61 turbofan engines. This AD 

requires initial and repetitive borescope 

inspections for missing HPT rear seal 

plate locking plugs and damaged 

locking plug retaining wires, and 

removal of the engine from service if 

necessary, based on inspection results. 

This AD results from two reports of 

missing HPT rear seal plate locking 

plugs, damage to the HPT disc, and 

damage to the remaining locking plug 

retaining wires. We are issuing this AD 

to prevent uncontained release of the 

HPT rear side plate and HPT disc, 

resulting in damage to the airplane. 

DATES: Effective February 16, 2006. The 

Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in the 

regulations as of February 16, 2006. 

We must receive any comments on 

this AD by April 3, 2006. 

ADDRESSES: Use one of the following 

addresses to comment on this AD: 

• DOT Docket Web site: Go to 

http://dms.dot.gov and follow the 

instructions for sending your comments 

electronically. 

• Government-wide rulemaking Web 

site: Go to http://www.regulations.gov 

and follow the instructions for sending 

your comments electronically. 

• Mail: Docket Management Facility; 

U.S. Department of Transportation, 400 

Seventh Street, SW., Nassif Building, 

Room PL–401, Washington, DC 20590–

0001. 

• Fax: (202) 493–2251. 

• Hand Delivery: Room PL–401 on 

the plaza level of the Nassif Building, 

400 Seventh Street, SW., Washington, 

DC, between 9 a.m. and 5 p.m., Monday 

through Friday, except Federal holidays. 

Contact Rolls-Royce plc, P.O. Box 31, 

Derby, DE248BJ; UK, telephone: 011–

44–1332–242424; fax: 011–44–1332–

249936, for the service information 

identified in this AD. 

FOR FURTHER INFORMATION CONTACT: 

Christopher Spinney, Aerospace 

Engineer, Engine Certification Office, 

FAA, Engine and Propeller Directorate, 

12 New England Executive Park; 

telephone (781) 238–7175; fax (781) 

238–7199. 

SUPPLEMENTARY INFORMATION: The Civil 

Aviation Authority (CAA), which is the 


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