26322 Federal Register / Vol. 74, No. 104 / Tuesday, June 2, 2009 / Proposed Rules 

time for this AD, follow the procedures 

in 14 CFR 39.19. Before using any 

approved AMOC on any airplane to 

which the AMOC applies, notify your 

principal maintenance inspector (PMI) 

or principal avionics inspector (PAI), as 

appropriate, or lacking a principal 

inspector, your local Flight Standards 

District Office. The AMOC approval 

letter must specifically reference this 

AD. 

Issued in Renton, Washington, on May 11, 

2009. 

Ali Bahrami, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. E9–12742 Filed 6–1–09; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2009–0496; Directorate 

Identifier 2008–NM–139–AD] 

RIN 2120–AA64 

Airworthiness Directives; Fokker 

Model F.27 Mark 050 and F.28 Mark 

0100 Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: We propose to adopt a new 

airworthiness directive (AD) for the 

products listed above. This proposed 

AD results from mandatory continuing 

airworthiness information (MCAI) 

originated by an aviation authority of 

another country to identify and correct 

an unsafe condition on an aviation 

product. The MCAI describes the unsafe 

condition as: 

Several incidents have been reported 

where an electrical burning smell was noted 

in the cockpit, originating from the Electrical 

Power Centre. Troubleshooting revealed a 

partly molten terminal, which normally 

attaches a wire or bus bar to a stud of an 

Electrical Power Contactor, Part Number 

(P/N) SG02206. Furthermore, heat damage to 

the contactor stud itself was found. * * * 

* * * * * 

This condition, if not corrected, could lead 

to further cases of overheating of terminals 

and studs of Electrical Power Contactors 

P/N SG02206, possibly resulting in the loss 

of electrical power systems, electrical arcing 

and fire/smoke in the cockpit. 

The proposed AD would require 

actions that are intended to address the 

unsafe condition described in the MCAI. 

DATES: We must receive comments on 

this proposed AD by July 2, 2009. 

ADDRESSES: You may send comments by 

any of the following methods: 

• Federal eRulemaking Portal: Go to 

http://www.regulations.gov. Follow the 

instructions for submitting comments. 

• Fax: (202) 493–2251. 

• Mail: U.S. Department of 

Transportation, Docket Operations, M– 

30, West Building Ground Floor, Room 

W12–140, 1200 New Jersey Avenue, SE., 

Washington, DC 20590. 

• Hand Delivery: U.S. Department of 

Transportation, Docket Operations, M– 

30, West Building Ground Floor, Room 

W12–40, 1200 New Jersey Avenue, SE., 

Washington, DC, between 9 a.m. and 5 

p.m., Monday through Friday, except 

Federal holidays. 

For Fokker service information 

identified in this proposed AD, contact 

Fokker Services B.V., Technical 

Services Dept., P.O. Box 231, 2150 AE 

Nieuw-Vennep, the Netherlands; 

telephone +31 (0) 252–627–350; fax +31 

(0) 252–627–211; e-mail 

technicalservices.

fokkerservices@stork.com; Internet 

http://www.myfokkerfleet.com. 

For Goodrich service information 

identified in this proposed AD, contact 

Goodrich Corporation, Power Systems, 

1555 Corporate Woods Parkway, 

Uniontown, Ohio 44685–8799; 

telephone 330–487–2007; fax 330–487– 

1902; e-mail twinsburg.

techpubs@goodrich.com; Internet http:// 

www.goodrich.com/TechPubs. 

You may review copies of the 

referenced service information at the 

FAA, Transport Airplane Directorate, 

1601 Lind Avenue, SW., Renton, 

Washington. For information on the 

availability of this material at the FAA, 

call 425–227–1221 or 425–227–1152. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http:// 

www.regulations.gov; or in person at the 

Docket Operations office between 9 a.m. 

and 5 p.m., Monday through Friday, 

except Federal holidays. The AD docket 

contains this proposed AD, the 

regulatory evaluation, any comments 

received, and other information. The 

street address for the Docket Operations 

office (telephone (800) 647–5527) is in 

the ADDRESSES section. Comments will 

be available in the AD docket shortly 

after receipt. 

FOR FURTHER INFORMATION CONTACT: Tom 

Rodriguez, Aerospace Engineer, 

International Branch, ANM–116, 

Transport Airplane Directorate, FAA, 

1601 Lind Avenue, SW., Renton, 

Washington 98057–3356; telephone 

(425) 227–1137; fax (425) 227–1149. 

SUPPLEMENTARY INFORMATION: 

Comments Invited 

We invite you to send any written 

relevant data, views, or arguments about 

this proposed AD. Send your comments 

to an address listed under the 

ADDRESSES section. Include ‘‘Docket No. 

FAA–2009–0496; Directorate Identifier 

2008–NM–139–AD’’ at the beginning of 

your comments. We specifically invite 

comments on the overall regulatory, 

economic, environmental, and energy 

aspects of this proposed AD. We will 

consider all comments received by the 

closing date and may amend this 

proposed AD based on those comments. 

We will post all comments we 

receive, without change, to http:// 

www.regulations.gov, including any 

personal information you provide. We 

will also post a report summarizing each 

substantive verbal contact we receive 

about this proposed AD. 

Discussion 

The European Aviation Safety Agency 

(EASA), which is the Technical Agent 

for the Member States of the European 

Community, has issued EASA 

Airworthiness Directive 2008–0091, 

dated May 13, 2008 (referred to after 

this as ‘‘the MCAI’’), to correct an unsafe 

condition for the specified products. 

The MCAI states: 

Several incidents have been reported 

where an electrical burning smell was noted 

in the cockpit, originating from the Electrical 

Power Centre. Troubleshooting revealed a 

partly molten terminal, which normally 

attaches a wire or bus bar to a stud of an 

Electrical Power Contactor, Part Number 

(P/N) SG02206. Furthermore, heat damage to 

the contactor stud itself was found. Material 

investigation revealed that the terminal, 

which was attached to the stud, was not 

properly torque tightened when the incident 

occurred. Loss of torque is considered to 

have occurred during operation, for reasons 

not fully understood. Further loosening may 

have taken place in-service under influence 

of vibration. As a result, poor contact caused 

electrical arcing during which extremely high 

temperatures were developed, leading to 

partial melting of the terminal. 

Investigation of some other burned 

contactors revealed evidence (flat spring lock 

washer) of a fully torqued terminal/stud 

connection when the overheating occurred. 

The exact cause for the increase in 

temperature in the contactor and the 

terminal/stud could not be determined. 

However, it could not be excluded that an 

increase of the temperature inside the 

contactor could lead to reduction of the 

reliability of the contactor stud/terminal 

connection due to loss of lock washer 

tension. The affected Electrical Power 

Contactor is used on several locations in the 

electrical power system, i.e. Generator Line 

Contactor (GLC), Bus Tie Contactor (BTC), 

Auxiliary Power Contactor (APC) and 

External Power Contactor (EPC). 

Federal Register / Vol. 74, No. 104 / Tuesday, June 2, 2009 / Proposed Rules 26323 

This condition, if not corrected, could lead 

to further cases of overheating of terminals 

and studs of Electrical Power Contactors P/ 

N SG02206, possibly resulting in the loss of 

electrical power systems, electrical arcing 

and fire/smoke in the cockpit. 

For the reasons described above, this EASA 

Airworthiness Directive (AD) requires the 

replacement of the current nut and spring 

washer of the standard contactor P/N 

SG02206 with a new self-locking nut. 

You may obtain further information 

by examining the MCAI in the AD 

docket. 

Relevant Service Information 

Goodrich Power Systems has issued 

Service Bulletin SG02206–24–01, dated 

March 4, 2008. Fokker Services B.V. has 

issued the service bulletins identified in 

the following table. 

TABLE—SERVICE INFORMATION

Service bulletin Date 

Fokker Service Bulletin SBF50–24–030, including the drawings identified in the subsequent table, ‘‘Table—Drawings Included in Fokker Service Bulletin SBF50–24–30’’.November 6, 2003. 

Fokker Service Bulletin SBF50–24–031 .................................................................................................................................. January 29, 2008. 

Fokker Service Bulletin SBF100–24–037, including Manual Change Notification—Maintenance Documentation MCNM 

F100–076, dated October 2, 2003, and including the drawings identified in the subsequent table, ‘‘Table—Drawings 

Included in Fokker Service Bulletin SBF100–24–037’’.

October 2, 2003. 

Fokker Service Bulletin SBF100–24–041 ................................................................................................................................ January 29, 2008. 

TABLE—DRAWINGS INCLUDED IN FOKKER SERVICE BULLETIN SBF50–24–030 

Fokker drawing— Sheet— Issue— Dated— 

W7980–236 ........................................................ 02 H ........................................................................ August 1, 2003. 

W7980–253 ........................................................ 40 BK ...................................................................... September 17, 2003. 

W7980–253 ........................................................ 41 BK ...................................................................... September 17, 2003. 

W7980–253 ........................................................ 42 BK ...................................................................... September 17, 2003. 

W7980–253 ........................................................ 43 BK ...................................................................... September 17, 2003. 

W7980–253 ........................................................ 44 BL ....................................................................... September 17, 2003. 

W7980–253 ........................................................ 45 BK ...................................................................... September 17, 2003. 

W7980–253 ........................................................ 46 BL ....................................................................... September 17, 2003. 

W7980–253 ........................................................ 47 BK ...................................................................... September 17, 2003. 

W7980–253 ........................................................ 48 BK ...................................................................... September 17, 2003. 

W7980–253 ........................................................ 49 BL ....................................................................... September 17, 2003. 

W7980–253 ........................................................ 50 BL ....................................................................... September 17, 2003. 

W7980–253 ........................................................ 51 BL ....................................................................... September 17, 2003. 

W7980–253 ........................................................ 52 BL ....................................................................... September 17, 2003. 

W7980–253 ........................................................ 53 BL ....................................................................... September 17, 2003. 

W7980–253 ........................................................ 54 BK ...................................................................... September 17, 2003. 

W7980–253 ........................................................ 55 BL ....................................................................... September 17, 2003. 

W7980–253 ........................................................ 56 BL ....................................................................... September 17, 2003. 

W7980–253 ........................................................ 57 BK ...................................................................... September 17, 2003. 

W7980–253 ........................................................ 58 BL ....................................................................... September 17, 2003. 

W7980–253 ........................................................ 59 BK ...................................................................... September 17, 2003. 

W7980–253 ........................................................ 60 BK ...................................................................... September 24, 2003. 

W7980–253 ........................................................ 61 BK ...................................................................... September 24, 2003. 

W7980–253 ........................................................ 62 BK ...................................................................... September 24, 2003. 

W7980–253 ........................................................ 63 BL ....................................................................... September 24, 2003. 

W7980–253 ........................................................ 64 BK ...................................................................... September 24, 2003. 

W7980–253 ........................................................ 65 BL ....................................................................... September 24, 2003. 

W7980–253 ........................................................ 66 BK ...................................................................... September 24, 2003. 

TABLE—DRAWINGS INCLUDED IN FOKKER SERVICE BULLETIN SBF100–24–037 

Fokker drawing— Sheet— Issue— Dated— 

W43255 .............................................................. 01 A ......................................................................... July 30, 2003. 

W43255 .............................................................. 02 Original ............................................................... July 30, 2003. 

W43255 .............................................................. 03 A ......................................................................... August 4, 2003. 

W43255 .............................................................. 04 A ......................................................................... July 30, 2003. 

W43255 .............................................................. 05 Original ............................................................... July 30, 2003. 

W43255 .............................................................. 06 A ......................................................................... July 30, 2003. 

W43255 .............................................................. 07 A ......................................................................... August 4, 2003. 

The actions described in this service 

information are intended to correct the 

unsafe condition identified in the 

MCAI. 

FAA’s Determination and Requirements 

of This Proposed AD 

This product has been approved by 

the aviation authority of another 

country, and is approved for operation 

in the United States. Pursuant to our 

bilateral agreement with the State of 

Design Authority, we have been notified 

of the unsafe condition described in the 

MCAI and service information 

26324 Federal Register / Vol. 74, No. 104 / Tuesday, June 2, 2009 / Proposed Rules 

referenced above. We are proposing this 

AD because we evaluated all pertinent 

information and determined an unsafe 

condition exists and is likely to exist or 

develop on other products of the same 

type design. 

Differences Between This AD and the 

MCAI or Service Information 

We have reviewed the MCAI and 

related service information and, in 

general, agree with their substance. But 

we might have found it necessary to use 

different words from those in the MCAI 

to ensure the AD is clear for U.S. 

operators and is enforceable. In making 

these changes, we do not intend to differ 

substantively from the information 

provided in the MCAI and related 

service information. 

We might also have proposed 

different actions in this AD from those 

in the MCAI in order to follow FAA 

policies. Any such differences are 

highlighted in a Note within the 

proposed AD. 

Costs of Compliance 

Based on the service information, we 

estimate that this proposed AD would 

affect about 5 products of U.S. registry. 

We also estimate that it would take 

about 8 work-hours per product to 

comply with the basic requirements of 

this proposed AD. The average labor 

rate is $80 per work-hour. Required 

parts would cost about $5,715 per 

product. Where the service information 

lists required parts costs that are 

covered under warranty, we have 

assumed that there will be no charge for 

these costs. As we do not control 

warranty coverage for affected parties, 

some parties may incur costs higher 

than estimated here. Based on these 

figures, we estimate the cost of the 

proposed AD on U.S. operators to be 

$31,775, or $6,355 per product. 

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 determined that this proposed AD 

would not have federalism implications 

under Executive Order 13132. This 

proposed AD would 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 this proposed 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 proposed AD and placed it in the 

AD docket. 

List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation 

safety, Incorporation by reference, 

Safety. 

The Proposed Amendment 

Accordingly, under the authority 

delegated to me by the Administrator, 

the FAA proposes to amend 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 FAA amends § 39.13 by adding 

the following new AD: 

Fokker Services B.V.: Docket No. FAA– 

2009–0496; Directorate Identifier 2008– 

NM–139–AD. 

Comments Due Date 

(a) We must receive comments by July 2, 

2009. 

Affected ADs 

(b) None. 

Applicability 

(c) This AD applies to Fokker Model F.27 

Mark 050 and F.28 Mark 0100 airplanes, 

certificated in any category, all serial 

numbers. 

Subject 

(d) Air Transport Association (ATA) of 

America Code 24: Electrical power. 

Reason 

(e) The mandatory continuing 

airworthiness information (MCAI) states: 

Several incidents have been reported 

where an electrical burning smell was noted 

in the cockpit, originating from the Electrical 

Power Centre. Troubleshooting revealed a 

partly molten terminal, which normally 

attaches a wire or bus bar to a stud of an 

Electrical Power Contactor, Part Number 

(P/N) SG02206. Furthermore, heat damage to 

the contactor stud itself was found. Material 

investigation revealed that the terminal, 

which was attached to the stud, was not 

properly torque tightened when the incident 

occurred. Loss of torque is considered to 

have occurred during operation, for reasons 

not fully understood. Further loosening may 

have taken place in-service under influence 

of vibration. As a result, poor contact caused 

electrical arcing during which extremely high 

temperatures were developed, leading to 

partial melting of the terminal. 

Investigation of some other burned 

contactors revealed evidence (flat spring lock 

washer) of a fully torqued terminal/stud 

connection when the overheating occurred. 

The exact cause for the increase in 

temperature in the contactor and the 

terminal/stud could not be determined. 

However, it could not be excluded that an 

increase of the temperature inside the 

contactor could lead to reduction of the 

reliability of the contactor stud/terminal 

connection due to loss of lock washer 

tension. The affected Electrical Power 

Contactor is used on several locations in the 

electrical power system, i.e. Generator Line 

Contactor (GLC), Bus Tie Contactor (BTC), 

Auxiliary Power Contactor (APC) and 

External Power Contactor (EPC). 

This condition, if not corrected, could lead 

to further cases of overheating of terminals 

and studs of Electrical Power Contactors 

P/N SG02206, possibly resulting in the loss 

of electrical power systems, electrical arcing 

and fire/smoke in the cockpit. 

For the reasons described above, this EASA 

Airworthiness Directive (AD) requires the 

replacement of the current nut and spring 

washer of the standard contactor P/N 

SG02206 with a new self-locking nut. 

Actions and Compliance 

(f) Unless already done, do the following 

actions: 

(1) Except as provided by paragraphs (f)(2) 

and (f)(3) of this AD: Within 36 months after 

the effective date of this AD, remove the 

standard nuts and lock washers from the 

contactors having part number (P/N) 

SG02206, install new self-locking nuts, and 

perform the applicable tests on the 

Alternating Current Bus Transfer system, in 

accordance with the Accomplishment 

Instructions of Fokker Service Bulletin 

SBF100–24–041 or SBF50–24–031, both 

dated January 29, 2008, as applicable. If any 

test fails, before further flight, repair using a 

method approved by either the Manager, 

International Branch, ANM–116, Transport 

Airplane Directorate, FAA; or EASA (or its 

delegated agent). 

Federal Register / Vol. 74, No. 104 / Tuesday, June 2, 2009 / Proposed Rules 26325 

(2) Accomplishment of paragraph (f)(1) of 

this AD is not required for Model F.28 Mark 

0100 airplanes that have been modified in 

service in accordance with Fokker Service 

Bulletin SBF100–24–037, dated October 2, 

2003. Accomplishment of Fokker Service 

Bulletin SBF100–24–037, dated October 2, 

2003, within the compliance time specified 

in paragraph (f)(1) of this AD is considered 

an acceptable method of compliance with the 

requirements of paragraph (f)(1) of this AD. 

(3) Accomplishment of paragraph (f)(1) of 

this AD is not required for Model F.27 Mark 

050 airplanes that have been modified during 

production to incorporate Fokker 

Engineering Change Record (ECR) 51780, or 

for airplanes that have been modified in 

service in accordance with Fokker Service 

Bulletin SBF50–24–030, dated November 6, 

2003. Accomplishment of Fokker Service 

Bulletin SBF50–24–030, dated November 6, 

2003, within the compliance time specified 

in paragraph (f)(1) of this AD is considered 

an acceptable method of compliance with the 

requirements of paragraph (f)(1) of this AD. 

(4) As of 36 months after the effective date 

of this AD, no person may install a contactor 

having P/N SG02206 on any airplane unless 

it has been modified in accordance with 

Goodrich Power Systems Service Bulletin 

SG02206–24–01, dated March 4, 2008. 

FAA AD Differences 

Note 1: This AD differs from the MCAI 

and/or service information as follows: The 

MCAI does not include a corrective action for 

airplanes on which the test required by 

paragraph (f)(1) of this AD fails. This AD 

requires the corrective action specified in 

paragraph (f)(1) of this AD. 

Other FAA AD Provisions 

(g) The following provisions also apply to 

this AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, International 

Branch, FAA, has the authority to approve 

AMOCs for this AD, if requested using the 

procedures found in 14 CFR 39.19. Send 

information to Attn: Tom Rodriguez, 

Aerospace Engineer, International Branch, 

ANM–116, Transport Airplane Directorate, 

FAA, 1601 Lind Avenue SW., Renton, 

Washington 98057–3356; telephone (425) 

227–1137; fax (425) 227–1149. Before using 

any approved AMOC on any airplane to 

which the AMOC applies, notify your 

appropriate principal maintenance inspector 

(PMI) or principal avionics inspector (PAI), 

as appropriate, or lacking a principal 

inspector, your local flight Standards District 

Office. 

(2) Airworthy Product: For any requirement 

in this AD to obtain corrective actions from 

a manufacturer or other source, use these 

actions if they are FAA-approved. Corrective 

actions are considered FAA-approved if they 

are approved by the State of Design Authority 

(or their delegated agent). You are required 

to assure the product is airworthy before it 

is returned to service. 

(3) Reporting Requirements: For any 

reporting requirement in this AD, under the 

provisions of the Paperwork Reduction Act, 

the Office of Management and Budget (OMB) 

has approved the information collection 

requirements and has assigned OMB Control 

Number 2120–0056. 

Related Information 

(h) Refer to MCAI EASA Airworthiness 

Directive 2008–0091, dated May 13, 2008, 

and the service information listed in Tables 

1, 2, and 3 of this AD for related information. 

TABLE 1—SERVICE INFORMATION

Service bulletin Date 

Fokker Service Bulletin SBF50–24–030, including the drawings identified in Table 2 of this AD ......................................... November 6, 2003. 

Fokker Service Bulletin SBF50–24–031 .................................................................................................................................. January 29, 2008. 

Fokker Service Bulletin SBF100–24–037, including Manual Change Notification—Maintenance Documentation MCNM 

F100–076, dated October 2, 2003, and including the drawings identified in Table 3 of this AD.

October 2, 2003. 

Fokker Service Bulletin SBF100–24–041 ................................................................................................................................ January 29, 2008. 

Goodrich Power Systems Service Bulletin SG02206–24–01 ................................................................................................. March 4, 2008. 

TABLE 2—DRAWINGS INCLUDED IN FOKKER SERVICE BULLETIN SBF50–24–030 

Fokker drawing— Sheet— Issue— Dated— 

W7980–236 ........................................................ 02 H ........................................................................ August 1, 2003. 

W7980–253 ........................................................ 40 BK ...................................................................... September 17, 2003. 

W7980–253 ........................................................ 41 BK ...................................................................... September 17, 2003. 

W7980–253 ........................................................ 42 BK ...................................................................... September 17, 2003. 

W7980–253 ........................................................ 43 BK ...................................................................... September 17, 2003. 

W7980–253 ........................................................ 44 BL ....................................................................... September 17, 2003. 

W7980–253 ........................................................ 45 BK ...................................................................... September 17, 2003. 

W7980–253 ........................................................ 46 BL ....................................................................... September 17, 2003. 

W7980–253 ........................................................ 47 BK ...................................................................... September 17, 2003. 

W7980–253 ........................................................ 48 BK ...................................................................... September 17, 2003. 

W7980–253 ........................................................ 49 BL ....................................................................... September 17, 2003. 

W7980–253 ........................................................ 50 BL ....................................................................... September 17, 2003. 

W7980–253 ........................................................ 51 BL ....................................................................... September 17, 2003. 

W7980–253 ........................................................ 52 BL ....................................................................... September 17, 2003. 

W7980–253 ........................................................ 53 BL ....................................................................... September 17, 2003. 

W7980–253 ........................................................ 54 BK ...................................................................... September 17, 2003. 

W7980–253 ........................................................ 55 BL ....................................................................... September 17, 2003. 

W7980–253 ........................................................ 56 BL ....................................................................... September 17, 2003. 

W7980–253 ........................................................ 57 BK ...................................................................... September 17, 2003. 

W7980–253 ........................................................ 58 BL ....................................................................... September 17, 2003. 

W7980–253 ........................................................ 59 BK ...................................................................... September 17, 2003. 

W7980–253 ........................................................ 60 BK ...................................................................... September 24, 2003. 

W7980–253 ........................................................ 61 BK ...................................................................... September 24, 2003. 

W7980–253 ........................................................ 62 BK ...................................................................... September 24, 2003. 

W7980–253 ........................................................ 63 BL ....................................................................... September 24, 2003. 

W7980–253 ........................................................ 64 BK ...................................................................... September 24, 2003. 

W7980–253 ........................................................ 65 BL ....................................................................... September 24, 2003. 

W7980–253 ........................................................ 66 BK ...................................................................... September 24, 2003. 

26326 Federal Register / Vol. 74, No. 104 / Tuesday, June 2, 2009 / Proposed Rules 

TABLE 3—DRAWINGS INCLUDED IN FOKKER SERVICE BULLETIN SBF100–24–037 

Fokker drawing— Sheet— Issue— Dated— 

W43255 .............................................................. 01 A ......................................................................... July 30, 2003. 

W43255 .............................................................. 02 Original ............................................................... July 30, 2003. 

W43255 .............................................................. 03 A ......................................................................... August 4, 2003. 

W43255 .............................................................. 04 A ......................................................................... July 30, 2003. 

W43255 .............................................................. 05 Original ............................................................... July 30, 2003. 

W43255 .............................................................. 06 A ......................................................................... July 30, 2003. 

W43255 .............................................................. 07 A ......................................................................... August 4, 2003. 

Issued in Renton, Washington, on May 20, 

2009. 

Stephen P. Boyd, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. E9–12803 Filed 6–1–09; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF HOMELAND 

SECURITY 

Coast Guard 

33 CFR Part 100 

[Docket No. USCG–2009–0251] 

RIN 1625–AA08 

Special Local Regulations for Marine 

Events; Patapsco River, Northwest 

Harbor, Baltimore, MD 

AGENCY: Coast Guard, DHS. 

ACTION: Notice of proposed rulemaking. 

SUMMARY: The Coast Guard proposes to 

establish special local regulations 

during the ‘‘Baltimore Dragon Boat 

Challenge,’’ a marine event to be held 

on the waters of the Patapsco River, 

Northwest Harbor, Baltimore, MD. 

These special local regulations are 

necessary to provide for the safety of life 

on navigable waters during the event. 

This action is intended to temporarily 

restrict vessel traffic in a portion of the 

Patapsco River during the event. 

DATES: Comments and related material 

must be received by the Coast Guard on 

or before July 2, 2009. 

ADDRESSES: You may submit comments 

identified by docket number USCG– 

2009–0251 using any one of the 

following methods: 

(1) Federal eRulemaking Portal: 

http://www.regulations.gov. 

(2) Fax: 202–493–2251. 

(3) Mail: Docket Management Facility 

(M–30), U.S. Department of 

Transportation, West Building Ground 

Floor, Room W12–140, 1200 New Jersey 

Avenue, SE., Washington, DC 20590– 

0001. 

(4) Hand delivery: Same as mail 

address above, between 9 a.m. and 5 

p.m., Monday through Friday, except 

Federal holidays. The telephone number 

is 202–366–9329. 

To avoid duplication, please use only 

one of these four methods. See the 

‘‘Public Participation and Request for 

Comments’’ portion of the 

SUPPLEMENTARY INFORMATION section 

below for instructions on submitting 

comments. 

FOR FURTHER INFORMATION CONTACT: If 

you have questions on this proposed 

rule, call or e-mail Mr. Ronald Houck, 

U.S. Coast Guard Sector Baltimore, MD; 

telephone 410–576–2674, e-mail 

Ronald.L.Houck@uscg.mil. If you have 

questions on viewing or submitting 

material to the docket, call Renee V. 

Wright, Program Manager, Docket 

Operations, telephone 202–366–9826. 

SUPPLEMENTARY INFORMATION: 

Public Participation and Request for 

Comments 

We encourage you to participate in 

this rulemaking by submitting 

comments and related materials. All 

comments received will be posted 

without change to http:// 

www.regulations.gov and will include 

any personal information you have 

provided. 

Submitting Comments 

If you submit a comment, please 

include the docket number for this 

rulemaking (USCG–2009–0251), 

indicate the specific section of this 

document to which each comment 

applies, and provide a reason for each 

suggestion or recommendation. You 

may submit your comments and 

material online (via http:// 

www.regulations.gov) or by fax, mail, or 

hand delivery, but please use only one 

of these means. If you submit a 

comment online via 

www.regulations.gov, it will be 

considered received by the Coast Guard 

when you successfully transmit the 

comment. If you fax, hand delivery, or 

mail your comment, it will be 

considered as having been received by 

the Coast Guard when it is received at 

the Docket Management Facility. We 

recommend that you include your name 

and a mailing address, an e-mail 

address, or a telephone number in the 

body of your document so that we can 

contact you if we have questions 

regarding your submission. 

To submit your comment online, go to 

http://www.regulations.gov, select the 

Advanced Docket Search option on the 

right side of the screen, insert ‘‘USCG– 

USCG–0251’’ in the Docket ID box, 

press Enter, and then click on the 

balloon shape in the Actions column. If 

you submit your comments by mail or 

hand delivery, submit them in an 

unbound format, no larger than 81⁄2 by 

11 inches, suitable for copying and 

electronic filing. If you submit 

comments by mail and would like to 

know that they reached the Facility, 

please enclose a stamped, self-addressed 

postcard or envelope. We will consider 

all comments and material received 

during the comment period and may 

change the rule based on your 

comments. 

Viewing Comments and Documents 

To view comments, as well as 

documents mentioned in this preamble 

as being available in the docket, go to 

http://www.regulations.gov, select the 

Advanced Docket Search option on the 

right side of the screen, insert USCG– 

2009–0251 in the Docket ID box, press 

Enter, and then click on the item in the 

Docket ID column. You may also visit 

the Docket Management Facility in 

Room W12–140 on the ground floor of 

the Department of Transportation West 

Building, 1200 New Jersey Avenue, SE., 

Washington, DC 20590, between 9 a.m. 

and 5 p.m., Monday through Friday, 

except Federal holidays. We have an 

agreement with the Department of 

Transportation to use the Docket 

Management Facility. 

Privacy Act 

Anyone can search the electronic 

form of comments received into any of 

our dockets by the name of the 

individual submitting the comment (or 

signing the comment, if submitted on 

behalf of an association, business, labor 

union, etc.). You may review a Privacy 

Act notice regarding our public dockets