53540 Federal Register / Vol. 70, No. 174 / Friday, September 9, 2005 / Rules and Regulations 

PART 966—TOMATOES GROWN IN 

FLORIDA 

■ 1. The authority citation for 7 CFR 

part 966 continues to read as follows: 

Authority: 7 U.S.C. 601–674. 

■ 2. In part 966, a new § 966.124 is 

added to read as follows: 

§ 966.124 Approved receiver. 

(a) Approved receiver. Any person 

who desires to acquire, as an approved 

receiver, tomatoes for purposes as set 

forth in § 966.120(a), shall annually, 

prior thereto, file an application with 

the committee on a form approved by it, 

which shall contain, but not be limited 

to, the following information: 

(1) Name, address, contact person, 

telephone number, and e-mail address 

of applicant; 

(2) Purpose of shipment; 

(3) Physical address of where 

manufacturing or other specified 

purpose is to occur; 

(4) Whether or not the receiver packs, 

repacks or sells fresh tomatoes; 

(5) A statement that the tomatoes 

obtained exempt from the fresh tomato 

regulations will not be resold or 

transferred for resale, directly or 

indirectly, but will be used only for the 

purpose specified in the corresponding 

certificate of privilege; 

(6) A statement agreeing to undergo 

random inspection by the committee; 

(7) A statement agreeing to submit 

such reports as is required by the 

committee. 

(b) The committee, or its duly 

authorized agents, shall give prompt 

consideration to each application for an 

approved receiver and shall determine 

whether the application is approved or 

disapproved and notify the applicant 

accordingly. 

(c) The committee, or its duly 

authorized agents, may rescind a 

person’s approved receiver status upon 

proof satisfactory that such a receiver 

has handled tomatoes contrary to the 

provisions established under the 

Certificate of Privilege. Such action 

rescinding approved receiver status 

shall apply to and not exceed a 

reasonable period of time as determined 

by the committee or its duly authorized 

agents. Any person who has been 

denied as an approved receiver or who 

has had their approved receiver status 

rescinded, may appeal to the committee 

for reconsideration. Such an appeal 

shall be made in writing. 

■ 3. In § 966.323, a new paragraph (5) is 

added to paragraph (c), and paragraph 

(g) is amended by revising the 

definitions of Processing and U.S. 

tomato Standards, and by adding a 

definition for Pickling to read as 

follows: 

§ 966.323 Handling regulations. 

* * * * * 

(c) * * * 

(5) Make shipments only to those who 

have qualified with the committee as 

approved receivers. 

* * * * * 

(g) * * *Processing as used in 

§§ 966.120 and 966.323 means the 

manufacture of any tomato product 

which has been converted into juice, or 

preserved by any commercial process, 

including canning, dehydrating, drying, 

and the addition of chemical 

substances. Further, all processing 

procedures must result in a product that 

does not require refrigeration until 

opened. Pickling as used in §§ 966.120 

and 966.323 means to preserve tomatoes 

in a brine or vinegar solution. U.S. 

tomato standards means the revised 

United States Standards for Fresh 

Tomatoes (7 CFR 51.1855 through 

51.1877), effective October 1, 1991, as 

amended, or variations thereof specified 

in this section. Other terms in this 

section shall have the same meaning as 

when used in Marketing Agreement No. 

125, as amended, and this part, and the 

U.S. tomato standards. 

Dated: September 2, 2005. 

Lloyd C. Day, 

Administrator, Agricultural Marketing 

Service. 

[FR Doc. 05–17860 Filed 9–8–05; 8:45 am] 

BILLING CODE 3410–02–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2005–22309; Directorate 

Identifier 2005–NM–159–AD; Amendment 

39–14254; AD 2005–18–14] 

RIN 2120–AA64 

Airworthiness Directives; Avions 

Marcel Dassault-Breguet Model Falcon 

10 Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule; request for 

comments. 

SUMMARY: The FAA is superseding an 

existing airworthiness directive (AD) 

that applies to all Dassault Model 

Falcon 10 series airplanes. The existing 

AD currently requires revising the 

airplane flight manual (AFM) and 

installing a placard in the flight deck to 

prohibit flight into known or forecasted 

icing conditions. In lieu of the AFM 

revision and placard installation, that 

AD allows identifying the part number 

of each flexible hose in the wing (slat) 

anti-icing system, performing repetitive 

inspections of each hose for 

delamination, and performing corrective 

actions if necessary. This AD adds the 

following actions (also in lieu of the 

AFM revision and placard installation): 

New repetitive inspections for 

delamination at reduced intervals, 

corrective actions if necessary, and an 

additional AFM revision to include a 

statement to track flight cycles when the 

slat anti-icing system is activated. This 

AD also provides an option to 

repetitively replace the existing flexible 

hoses with improved flexible hoses, 

which terminates the repetitive 

inspection requirements. This AD 

results from a report of in-service 

delamination of a flexible hose in the 

slat anti-icing system at a time earlier 

than previously reported. We are issuing 

this AD to prevent collapse of the 

flexible hoses in the slat anti-icing 

system, which could lead to insufficient 

anti-icing capability and, if icing is 

encountered in this situation, could 

result in reduced controllability of the 

airplane. 

DATES: This AD becomes effective 

September 26, 2005. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in the AD 

as of September 26, 2005. 

On April 26, 2005 (70 FR 18282, April 

11, 2005), the Director of the Federal 

Register approved the incorporation by 

reference of Dassault Alert Service 

Bulletin F10–A312, dated February 25, 

2005, including the Service Bulletins 

Compliance Card. 

We must receive any comments on 

this AD by November 8, 2005. 

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. 

• Fax: (202) 493–2251. 

• Hand Delivery: Room PL–401 on 

the plaza level of the Nassif Building, 

400 Seventh Street, SW., Washington, 

Federal Register / Vol. 70, No. 174 / Friday, September 9, 2005 / Rules and Regulations 53541 

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. 

You may examine the contents of the 

AD docket on the Internet at http:// 

dms.dot.gov, or in person at the Docket 

Management Facility, U.S. Department 

of Transportation, 400 Seventh Street, 

SW., Room PL–401, on the plaza level 

of the Nassif Building, Washington, DC. 

This docket number is FAA–2005–

22309; the directorate identifier for this 

docket is 2005–NM–159–AD. 

FOR FURTHER INFORMATION CONTACT: Tom 

Rodriguez, Aerospace Engineer, 

International Branch, ANM–116, FAA, 

Transport Airplane Directorate, 1601 

Lind Avenue, SW., Renton, Washington 

98055–4056; telephone (425) 227–1137; 

fax (425) 227–1149. 

SUPPLEMENTARY INFORMATION: 

Discussion 

On March 31, 2005, the FAA issued 

AD 2005–07–23, amendment 39–14048 

(70 FR 18282, April 11, 2005). That AD 

applies to all Dassault Model Falcon 10 

series airplanes. That AD requires 

revising the Limitations section of the 

airplane flight manual (AFM) to include 

a statement prohibiting flight into 

known or forecasted icing conditions, 

and installing a placard in the flight 

deck. In lieu of the AFM revision and 

placard installation, that AD allows 

identifying the part number of each 

flexible hose in the wing (slat) anti-icing 

system, performing repetitive detailed 

inspections of each hose for 

delamination, and performing corrective 

actions if necessary. That AD resulted 

from a report of delamination of the 

internal wall of a flexible hose in the 

slat anti-icing system. The actions 

specified in that AD are intended to 

prevent collapse of the flexible hoses in 

the slat anti-icing system, which could 

lead to insufficient anti-icing capability 

and, if icing is encountered in this 

situation, could result in reduced 

controllability of the airplane. 

Actions Since AD Was Issued 

Since we issued that AD the Direction 

Ge ́ne ́rale de l’Aviation Civile (DGAC), 

which is the airworthiness authority for 

France, informed us of an in-service 

delamination of a flexible hose in the 

slat anti-icing system at a time earlier 

than previously reported. 

In addition, the preamble to AD 2005–

07–23 explains that we consider the 

requirements ‘‘interim action’’ and were 

considering further rulemaking. We now 

have determined that further 

rulemaking is indeed necessary, and, 

although a final action has not yet been 

developed, this AD follows from that 

determination. 

Relevant Service Information 

Avions Marcel Dassault-Breguet has 

issued Dassault Alert Service Bulletin 

F10–A312, Revision 1, dated June 27, 

2005. The existing AD refers to Dassault 

Alert Service Bulletin F10–A312, dated 

February 25, 2005, as the appropriate 

source of service information for 

accomplishing the required actions of 

that AD. Dassault Alert Service Bulletin 

F10–A312, Revision 1, describes 

procedures for a visual check and an 

improved boroscope inspection of the 

internal walls of each flexible hose in 

the slat anti-icing system for blistering 

(delamination), and performing 

corrective actions if necessary. The 

corrective actions include replacing any 

hose that doesn’t have a certain part 

number with a hose having the part 

number specified in the service bulletin, 

and replacing any damaged hose with a 

new hose having the part number 

specified in the service bulletin. The 

DGAC mandated the service bulletin 

and issued French emergency 

airworthiness directive 

EASA.A.AD.01001, dated June 29, 2005, 

to ensure the continued airworthiness of 

these airplanes in France. 

Avions Marcel Dassault-Breguet has 

also issued Dassault Service Bulletin 

F10–313, dated August 10, 2005. This 

service bulletin describes procedures for 

replacing the existing flexible hoses 

with improved flexible hoses, having a 

new part number. These new flexible 

hoses have a temporary life limit of 90 

flight cycles during which the slat antiicing system is in use. 

Accomplishing the actions specified 

in the service information is intended to 

adequately address the unsafe 

condition. 

FAA’s Determination and Requirements 

of This AD 

This airplane model is manufactured 

in France and is type certificated for 

operation in the United States under the 

provisions of section 21.29 of the 

Federal Aviation Regulations (14 CFR 

21.29) and the applicable bilateral 

airworthiness agreement. Pursuant to 

this bilateral airworthiness agreement, 

the DGAC has kept the FAA informed 

of the situation described above. We 

have examined the DGAC’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 

supersede AD 2005–07–23. This new 

AD retains the requirements of the 

existing AD. This AD also: 

• Provides an improved inspection 

method and reduces the intervals for the 

inspections; 

• Provides an option to repetitively 

replace the existing flexible hoses with 

improved flexible hoses, which 

terminates the repetitive inspection 

requirements; 

• Requires revising the Limitations 

section of the AFM to provide a 

mechanism for tracking flight cycles in 

which the slat anti-icing system is 

activated; and 

• Requires sending the inspection 

results to the manufacturer. 

Differences Between the AD and the 

French Emergency Airworthiness 

Directive 

This AD differs from the French 

emergency airworthiness directive in 

that it includes the option to install 

improved flexible hoses. The airplane 

manufacturer is requesting that the 

DGAC approve this option as an 

alternative method of complying with 

French emergency airworthiness 

directive EASA.A.AD.01001. 

This AD also differs from the French 

emergency airworthiness directive by 

requiring an AFM revision to enable the 

tracking of flight cycles in which the 

slat anti-icing system is activated. The 

French emergency airworthiness 

directive contains instructions to the 

flightcrew to record in the flight log any 

time the anti-icing system switch is on 

during flight, but does not specify an 

AFM revision. 

These differences have been 

coordinated with the DGAC. 

Interim Action 

This AD is considered to be interim 

action. The inspection reports that are 

required by this AD will enable the 

manufacturer to obtain better insight 

into the nature, cause, and extent of the 

delamination of the internal walls of a 

flexible hose, and eventually to develop 

final action to address the unsafe 

condition. Once final action has been 

identified, we may consider further 

rulemaking. 

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. 

53542 Federal Register / Vol. 70, No. 174 / Friday, September 9, 2005 / Rules and Regulations 

Explanation of Change to Applicability 

We have revised the applicability of 

the AD to identify the model 

designation as published in the most 

recent type certificate data sheet for the 

affected model. 

Clarification of Inspection Terminology 

In this AD, the ‘‘visual check’’

specified in Dassault Alert Service 

Bulletin F10–A312, Revision 1, is 

referred to as a ‘‘detailed inspection.’’

We have included the definition for a 

detailed inspection in a note in this AD. 

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–2005–22309; Directorate Identifier 

2005–NM–159–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 can review the DOT’s complete 

Privacy Act Statement in the Federal 

Register published on April 11, 2000 

(65 FR 19477–78), or you can 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 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. The Federal Aviation 

Administration (FAA) amends § 39.13 

by removing amendment 39–14048 (70 

FR 18282, April 11, 2005) and adding 

the following new AD: 

2005–18–14 Avions Marcel DassaultBreguet Aviation (AMD/BA): Docket No. 

FAA–2005–22309; Directorate Identifier 

2005–NM–159–AD; Amendment 39–

14254. 

Effective Date 

(a) This AD becomes effective September 

26, 2005. 

Affected ADs 

(b) This AD supersedes AD 2005–07–23. 

Applicability 

(c) This AD applies to all Avions Marcel 

Dassault-Breguet Model Falcon 10 airplanes, 

certificated in any category. 

Unsafe Condition 

(d) This AD results from a report of inservice delamination of a flexible hose in the 

slat anti-icing system at a time earlier than 

previously reported. We are issuing this AD 

to prevent collapse of the flexible hoses in 

the slat anti-icing system, which could lead 

to insufficient anti-icing capability and, if 

icing is encountered in this situation, could 

result in reduced controllability of the 

airplane. 

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. 

Restatement of the Requirements of AD 

2005–07–23 

Repetitive Inspections, or Airplane Flight 

Manual (AFM) Revision and Placard 

Installation 

(f) Within 14 days after April 26, 2005 (the 

effective date of AD 2005–07–23), perform 

the actions specified in either paragraph (f)(1) 

or (f)(2) of this AD: 

(1) Revise the Limitations section of the 

Dassault Aviation Falcon 10 AFM, and install 

a placard in the flight deck, to include the 

following information. 

‘‘Flights into known or forecasted icing 

conditions are prohibited.’’

The AFM revision may be done by 

inserting a copy of this AD into the AFM. 

Install the placard on the pedestal in clear 

view of the pilot. 

(2) Determine the part number of each 

flexible hose installed in the slat anti-icing 

system, perform a detailed inspection of the 

internal walls of the hoses for delamination, 

and perform any applicable corrective action, 

by accomplishing all of the applicable 

actions specified in the Accomplishment 

Instructions of Dassault Alert Service 

Bulletin F10–A312, dated February 25, 2005. 

If the part number for any hose cannot be 

determined, before further flight, replace that 

hose with a hose having part number (P/N) 

FAL1005D. Any corrective action must be 

Federal Register / Vol. 70, No. 174 / Friday, September 9, 2005 / Rules and Regulations 53543 

done before further flight. Repeat the detailed 

inspection thereafter at intervals not to 

exceed 60 flight cycles or 3 months, 

whichever is first, until the actions required 

by paragraph (i) of this AD are accomplished. 

Note 1: When a statement identical to that 

in paragraph (f)(1) of this AD has been 

included in the general revision of the AFM, 

the general revision may be inserted into the 

AFM, and the copy of this AD may be 

removed from the AFM. 

Note 2: For the purposes of this AD, a 

detailed inspection is: ‘‘An intensive 

examination of a specific item, installation, 

or assembly to detect damage, failure, or 

irregularity. Available lighting is normally 

supplemented with a direct source of good 

lighting at an intensity deemed appropriate. 

Inspection aids such as mirror, magnifying 

lenses, etc., may be necessary. Surface 

cleaning and elaborate procedures may be 

required.’’

(g) For airplanes on which the actions 

described in paragraph (f)(1) of this AD are 

performed, doing the actions described in 

paragraph (f)(2) of this AD is terminating 

action for the requirements of paragraph (f)(1) 

of this AD. Once the initial detailed 

inspection specified in paragraph (f)(2) of 

this AD is performed, the AFM limitation 

and placard required by paragraph (f)(1) of 

this AD may be removed. 

New Requirements of This AD 

New Inspections and Intervals 

(h) For airplanes not operated under the 

limitation in paragraph (f)(1) of this AD, 

before the next 10 flight cycles in which the 

slat anti-icing system is activated after the 

effective date of this AD: Do a boroscope 

inspection of each flexible hose installed in 

the slat anti-icing system. Do all the 

inspections and any applicable corrective 

action (including replacing the hose with a 

new hose having P/N FAL1005D), by 

accomplishing all of the applicable actions 

specified in the Accomplishment 

Instructions of Dassault Alert Service 

Bulletin F10–A312, Revision 1, dated June 

27, 2005. Any corrective action must be done 

before further flight. Repeat the inspection 

thereafter at intervals not to exceed 10 flight 

cycles in which the slat anti-icing system is 

activated. Doing this inspection terminates 

the repetitive inspection requirements of 

paragraph (f)(2) of this AD. 

(i) For airplanes on which the actions 

described in paragraph (f)(1) of this AD are 

performed, doing the actions described in 

paragraph (h) of this AD is terminating action 

for the requirements of paragraph (f)(1) of 

this AD. Once the initial boroscope 

inspection specified in paragraph (h) of this 

AD is performed, the AFM limitation and 

placard required by paragraph (f)(1) of this 

AD may be removed. 

AFM Revision 

(j) For airplanes not operated under the 

limitation in paragraph (f)(1) of this AD, 

before further flight after the effective date of 

this AD: Revise the Limitations section of the 

Dassault Aviation Falcon 10 AFM, to include 

the following information. 

‘‘After each flight in which the slat anti-ice 

system is activated, inform maintenance.’’

The AFM revision may be done by 

inserting a copy of this AD into the AFM. 

Note 3: When a statement identical to that 

in paragraph (j)(1) of this AD has been 

included in the general revision of the AFM, 

the general revision may be inserted into the 

AFM, and the copy of this AD may be 

removed from the AFM. 

Optional Replacement 

(k) For airplanes not operated under the 

limitation in paragraph (f)(1) of this AD: 

Replacing the flexible hose installed in the 

slat anti-icing system with a new hose having 

P/N FAL1007, in accordance with the 

Accomplishment Instructions of Dassault 

Service Bulletin F10–313, dated August 10, 

2005, terminates the repetitive inspection 

intervals of paragraph (h) and (f)(2) of this 

AD. Repeat the replacement thereafter at 

intervals not to exceed 90 flight cycles in 

which the slat anti-icing system is activated. 

Reporting Requirement 

(l) At the applicable time specified in 

paragraph (l)(1) or (l)(2) of this AD: After 

performing any inspection required by this 

AD, submit a report of the findings (positive 

and negative) of the inspection to: Dassault 

Falcon Jet, Attn: Service Engineering/Falcon 

10, fax: (201) 541–4700. The report must 

include the airplane serial number, the 

location of the hose (inboard or outboard), 

the number of flight hours since hose 

installation, the number of cycles in icing 

conditions, and the manufacturing date and 

batch number of the hose. Submission of the 

Service Bulletins Compliance card, which is 

attached to Dassault Alert Service Bulletin 

F10–A312, is an acceptable method of 

complying with this requirement. Under the 

provisions of the Paperwork Reduction Act of 

1980 (44 U.S.C. 3501 et seq.), the Office of 

Management and Budget (OMB) has 

approved the information collection 

requirements contained in this AD and has 

assigned OMB Control Number 2120–0056. 

(1) If the inspection is done after the 

effective date of this AD: Submit the report 

within 30 days after the inspection. 

(2) If the inspection was done before the 

effective date of this AD: Submit the report 

within 30 days after the effective date of this 

AD. 

Actions Accomplished in Accordance With 

Previous Issue of Service Bulletin 

(m) Actions accomplished before the 

effective date of this AD in accordance with 

the Accomplishment Instructions of Dassault 

Alert Service Bulletin F10–A312, dated 

February 25, 2005, are acceptable for 

compliance with the corresponding action in 

this AD. 

Alternative Methods of Compliance (AMOCs) 

(n) 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. 

Related Information 

(o) French emergency airworthiness 

directive EASA.A.AD.01001, dated June 29, 

2005, also addresses the subject of this AD. 

Material Incorporated by Reference 

(p) You must use Dassault Alert Service 

Bulletin F10–A312, dated February 25, 2005, 

including the Service Bulletins Compliance 

Card; and Dassault Alert Service Bulletin 

F10–A312, Revision 1, dated June 27, 2005, 

including the Service Bulletins Compliance 

Card; as applicable; to perform the actions 

that are required by this AD, unless the AD 

specifies otherwise. If accomplished, you 

must used Dassault Service Bulletin F10–

313, dated August 10, 2005, to perform the 

optional replacement specified by this AD. 

(1) The Director of the Federal Register 

approved the incorporation by reference of 

Dassault Alert Service Bulletin F10-A312, 

Revision 1, dated June 27, 2005, including 

the Service Bulletins Compliance Card; and 

Dassault Service Bulletin F10–313, dated 

August 10, 2005; in accordance with 5 U.S.C. 

552(a) and 1 CFR part 51. 

(2) On April 26, 2005 (70 FR 18282, April 

11, 2005), the Director of the Federal Register 

approved the incorporation by reference of 

Dassault Alert Service Bulletin F10–A312, 

dated February 25, 2005, including the 

Service Bulletins Compliance Card. 

(3) 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. 

Issued in Renton, Washington, on August 

26, 2005. 

Ali Bahrami, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 05–17598 Filed 9–8–05; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2004–19955; Directorate 

Identifier 2004–NE–17–AD; Amendment 39–

14252; AD 2005–18–12] 

RIN 2120–AA64 

Airworthiness Directives; Hartzell 

Propeller Inc. Propellers 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule.