61580 Federal Register / Vol. 70, No. 205 / Tuesday, October 25, 2005 / Proposed Rules 

Reduction Act of 1995 (44 U.S.C. 3501 

et seq.). 

List of Subjects in 9 CFR Part 94 

Animal diseases, Imports, Livestock, 

Meat and meat products, Milk, Poultry 

and poultry products, Reporting and 

recordkeeping requirements. 

Accordingly, we propose to amend 9 

CFR part 94 as follows: 

PART 94—RINDERPEST, FOOT-ANDMOUTH DISEASE, FOWL PEST (FOWL 

PLAGUE), EXOTIC NEWCASTLE 

DISEASE, AFRICAN SWINE FEVER, 

CLASSICAL SWINE FEVER, AND 

BOVINE SPONGIFORM 

ENCEPHALOPATHY: PROHIBITED 

AND RESTRICTED IMPORTATIONS 

1. The authority citation for part 94 

would continue to read as follows: 

Authority: 7 U.S.C. 450, 7701–7772, 7781–

7786, and 8301–8317; 21 U.S.C. 136 and 

136a; 31 U.S.C. 9701; 7 CFR 2.22, 2.80, and 

371.4. 

2. In § 94.4, the introductory text of 

paragraph (a), paragraph (a)(4), 

paragraph (b)(3), and paragraph (b)(8)(i) 

would be revised to read as follows: 

§ 94.4 Cured or cooked meat originating in 

regions where rinderpest or foot-and-mouth 

disease exists. 

(a) Whether the meat is cured in the 

region of origin or in another region, the 

importation of cured meats derived from 

any ruminant or swine that originates in 

a region where rinderpest or foot-andmouth disease exists, as designated in 

§ 94.1, is prohibited unless the 

following conditions have been 

fulfilled: 

* * * * * 

(4) The cured meat shall be 

accompanied by a certificate stating that 

such meat has been prepared in 

accordance with paragraphs (a)(1), 

(a)(2), and (a)(3)(i) of this section. The 

certificate shall be issued by an official 

of the national government of the region 

of origin or, if the meat was cured in 

another region, by an official of the 

national government of the region in 

which the meat was cured, who is 

authorized to issue the foreign meat 

inspection certificate required by 

§ 327.4 of this title. Upon arrival of the 

cured meat in the United States, the 

certificate must be presented to an 

authorized inspector at the port of 

arrival. 

(b) * * * 

(3) Shelf-stable canned meat. Shelfstable canned meat, whether cooked and 

sealed in the region of origin or in 

another region, is exempt from the 

requirements of this section if cooked 

and sealed in the following manner: The 

meat or meat product has been fully 

cooked by a commercial method in a 

container hermetically sealed promptly 

after filling but before such cooking, so 

that such cooking and sealing produce 

a fully sterilized product that is shelfstable without refrigeration. 

* * * * * 

(8) * * * (i) The cooked meat must be 

accompanied by a certificate stating: 

‘‘This cooked meat produced for export 

to the United States meets the 

requirements of title 9, Code of Federal 

Regulations, § 94.4(b).’’ The certificate 

must be issued by an official of the 

national government of the region of 

origin or, if the meat is shelf-stable 

canned meat that was cooked and sealed 

in accordance with § 94.4(b)(3) in 

another region, by an official of the 

national government of the region in 

which the meat was cooked and sealed, 

who is authorized to issue the foreign 

meat inspection certificate required by 

§ 327.4 of this title. Upon arrival of the 

cooked meat in the United States, the 

certificate must be presented to an 

authorized inspector at the port of 

arrival. 

* * * * * 

Done in Washington, DC, this 19th day of 

October 2005. 

Elizabeth E. Gaston, 

Acting Administrator, Animal and Plant 

Health Inspection Service. 

[FR Doc. 05–21306 Filed 10–24–05; 8:45 am] 

BILLING CODE 3410–34–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2005–20970; Directorate 

Identifier 2004–NM–53–AD] 

RIN 2120–AA64 

Airworthiness Directives; Cessna 

Model 500, 501, 550, S550, 551, and 560 

Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Supplemental notice of 

proposed rulemaking (NPRM); 

reopening of comment period. 

SUMMARY: The FAA is revising an earlier 

proposed airworthiness directive (AD) 

for certain Cessna Model 500, 501, 550, 

S550, 551, and 560 airplanes. The 

original NPRM would have required 

revising the airplane flight manual 

(AFM) to prohibit use of the wing fuel 

boost pumps for defueling under certain 

conditions; installing a placard; doing 

other specified investigative and 

corrective actions as necessary; and 

modifying the boost pumps. The 

original NPRM also would have 

required the subsequent removal of the 

AFM revision and placard. The original 

NPRM resulted from a report of a chafed 

electrical wiring harness, which was 

arcing inside the fuel tank. This action 

revises the original NPRM by 

identifying certain service information 

not identified in the original NPRM. We 

are proposing this supplemental NPRM 

to prevent potential fuel vapor ignition 

in a fuel tank, which could result in 

explosion and loss of the airplane. 

DATES: We must receive comments on 

this supplemental NPRM by November 

21, 2005. 

ADDRESSES: Use one of the following 

addresses to submit comments on this 

supplemental NPRM. 

• 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, 

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

through Friday, except Federal holidays. 

For service information identified in 

this proposed AD, contact Cessna 

Aircraft Co., P.O. Box 7706, Wichita, 

Kansas 67277. 

FOR FURTHER INFORMATION CONTACT: 

Bryan Easterwood, Aerospace Engineer, 

Electrical Systems and Avionics Branch, 

ACE–119W, FAA, Wichita Aircraft 

Certification Office, 1801 Airport Road, 

room 100, Mid-Continent Airport, 

Wichita, Kansas 67209; telephone (316) 

946–4132; fax (316) 946–4107. 

SUPPLEMENTARY INFORMATION: 

Comments Invited 

We invite you to submit any relevant 

written data, views, or arguments 

regarding this supplemental NPRM. 

Send your comments to an address 

listed in the ADDRESSES section. Include 

the docket number ‘‘Docket No. FAA–

2005–20970; Directorate Identifier 

2004–NM–53–AD’’ at the beginning of 

your comments. We specifically invite 

comments on the overall regulatory, 

economic, environmental, and energy 

aspects of this supplemental NPRM. We 

Federal Register / Vol. 70, No. 205 / Tuesday, October 25, 2005 / Proposed Rules 61581 

will consider all comments received by 

the closing date and may amend this 

supplemental NPRM in light of those 

comments. 

We will post all comments submitted, 

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 supplemental NPRM. 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 

(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 in the Nassif Building at the DOT 

street address stated in ADDRESSES. 

Comments will be available in the AD 

docket shortly after the Docket 

Management System receives them. 

Discussion 

We proposed to amend 14 CFR part 

39 with a notice of proposed rulemaking 

(NPRM) for an AD (the ‘‘original 

NPRM’’) for certain Cessna Model 500, 

501, 550, S550, 551, and 560 airplanes. 

The original NPRM was published in 

the Federal Register on April 18, 2005 

(70 FR 20083). The original NPRM 

proposed to require revising the 

airplane flight manual (AFM) to prohibit 

use of the wing fuel boost pumps for 

defueling under certain conditions; 

installing a placard; doing other 

specified investigative and corrective 

actions as necessary; and modifying the 

boost pumps. The original NPRM also 

proposed to require the subsequent 

removal of the AFM revision and 

placard. 

Actions Since Original NPRM Was 

Issued 

Since we issued the original NPRM, 

we received no comments on the 

original NPRM or on the determination 

of the cost to the public. However, we 

have learned that the temporary 

revisions (TRs) were not identified in 

certain service bulletins cited in the 

original NPRM. This information is 

provided in the table in the next section. 

Relevant Service Information 

We have reviewed the TRs identified 

in the following table. 

TRS

Cessna temporary change— Dated— To the—

500FM TC–R57–01 ............................................. April 5, 2004 ........................................................ Cessna Model 500 AFM. 

500FM TC–R57–02 ............................................. April 5, 2004 ........................................................ Cessna Model 500 AFM. 

500FM TC–R57–03 ............................................. April 5, 2004 ........................................................ Cessna Model 500 AFM. 

55BFM TC–R10–07 ............................................. March 17, 2004 ................................................... Cessna Model 550 Citation Bravo AFM. 

55BFM TC–R10–08 ............................................. March 17, 2004 ................................................... Cessna Model 550 Citation Bravo AFM. 

55BFM TC–R10–09 ............................................. March 17, 2004 ................................................... Cessna Model 550 Citation Bravo AFM. 

560FM TC–R13–01 ............................................. March 4, 2004 ..................................................... Cessna Model 560 Citation V AFM. 

560FM TC–R13–02 ............................................. March 4, 2004 ..................................................... Cessna Model 560 Citation V AFM. 

560FM TC–R13–03 ............................................. March 4, 2004 ..................................................... Cessna Model 560 Citation V AFM. 

56FMA TC–04–01 ............................................... March 4, 2004 ..................................................... Cessna Model 560 Citation Ultra AFM. 

56FMA TC–04–02 ............................................... March 4, 2004 ..................................................... Cessna Model 560 Citation Ultra AFM. 

56FMA TC–04–03 ............................................... March 4, 2004 ..................................................... Cessna Model 560 Citation Ultra AFM. 

56FMB TC–R03–10 ............................................. March 12, 2004 ................................................... Cessna Model 550 AFM. 

56FMB TC–R03–11 ............................................. March 12, 2004 ................................................... Cessna Model 560 AFM. 

56FMB TC–R03–12 ............................................. March 12, 2004 ................................................... Cessna Model 560 AFM. 

S55CA TC–04–01 ................................................ July 8, 2004 ......................................................... Cessna Model S550 Citation S/II AFM. 

S55CA TC–04–02 ................................................ July 8, 2004 ......................................................... Cessna Model S550 Citation S/II AFM. 

S55CA TC–04–03 ................................................ July 8, 2004 ......................................................... Cessna Model S550 Citation S/II AFM. 

S55FM TC–04–01 ............................................... March 4, 2004 ..................................................... Cessna Model S550 Citation S/II AFM. 

S55FM TC–04–02 ............................................... March 4, 2004 ..................................................... Cessna Model S550 Citation S/II AFM. 

S55FM TC–04–03 ............................................... March 4, 2004 ..................................................... Cessna Model S550 Citation S/II AFM. 

The TRs prohibit use of the wing fuel 

boost pumps for defueling under certain 

conditions. Accomplishing the actions 

specified in the service information 

described in the original and 

supplemental NPRMs is intended to 

adequately address the unsafe 

condition. 

FAA’s Determination and Proposed 

Requirements of the Supplemental 

NPRM 

The changes discussed above expand 

the scope of the original NPRM; 

therefore, we have determined that it is 

necessary to reopen the comment period 

to provide additional opportunity for 

public comment on this supplemental 

NPRM. 

Costs of Compliance 

There are about 2,397 airplanes of the 

affected design in the worldwide fleet. 

The following table provides the 

estimated costs for U.S. operators to 

comply with this supplemental NPRM. 

ESTIMATED COSTS

Applicable service bulletin Work 

hours 

Average 

hourly labor 

rate 

Parts Cost per 

airplane 

Number 

of U.S.- 

registered 

airplanes 

Fleet cost 

SB500–28–12 ............................................................................ 20 $65 $2,229 $3,529 444 $1,566,876 

61582 Federal Register / Vol. 70, No. 205 / Tuesday, October 25, 2005 / Proposed Rules 

ESTIMATED COSTS—Continued 

Applicable service bulletin Work 

hours 

Average 

hourly labor 

rate 

Parts Cost per 

airplane 

Number 

of U.S.- 

registered 

airplanes 

Fleet cost 

SBS550–28–08 .......................................................................... 12 65 102 882 126 111,132 

SB550–28–14 ............................................................................ 8 65 1,992 2,512 469 1,178,128 

SB550–28–15 ............................................................................ 8 65 1,936 2,456 194 476,464 

SB560–28–10 ............................................................................ 12 65 1,949 2,729 428 1,168,012 

SB560–28–11 ............................................................................ 8 65 1,052 1,572 101 158,772 

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 

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 that the 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 supplemental NPRM 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, 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 Federal Aviation 

Administration (FAA) amends § 39.13 

by adding the following new 

airworthiness directive (AD): 

Cessna Aircraft Company: Docket No. FAA–

2005–20970; Directorate Identifier 2004–

NM–53–AD. 

Comments Due Date 

(a) The FAA must receive comments on 

this AD action by November 21, 2005. 

Affected ADs 

(b) None. 

Applicability 

(c) This AD applies to the Cessna airplanes 

listed in Table 1 of this AD, certificated in 

any category. 

TABLE 1.—APPLICABILITY

Airplane 

model(s) Serial Nos. 

500 and 501 ..... 0001 through 0689 inclusive. 

S550 ................. 0001 through 0160 inclusive. 

550 and 551 ..... 0002 through 0733 inclusive. 

550 .................... 0801 through 1075 inclusive. 

560 .................... 0001 through 0648 inclusive. 

Unsafe Condition 

(d) This AD was prompted by a report of 

a chafed electrical wiring harness, which was 

arcing inside the fuel tank. We are issuing 

this AD to prevent potential fuel vapor 

ignition in a fuel tank, which could result in 

explosion and loss 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. 

Service Information 

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

this AD refers to the applicable service 

bulletin listed in Table 2 of this AD. 

TABLE 2.—SERVICE INFORMATION

For Cessna model— Having serial 

numbers—

Use Cessna 

service bulletin— Dated—

500 and 501 airplanes ............................................................................................... 0001–0689 SB500–28–12 June 14, 2004. 

S550 airplanes ........................................................................................................... 0001–0160 SBS550–28–08 May 7, 2004. 

550 and 551 airplanes ............................................................................................... 0002–0733 SB550–28–14 December 2, 2003. 

550 airplanes ............................................................................................................. 0801–1075 SB550–28–15 January 20, 2004. 

560 airplanes ............................................................................................................. 0001–0538 SB560–28–10 April 23, 2004. 

560 airplanes ............................................................................................................. 0539–0648 SB560–28–11 March 12, 2004. 

Federal Register / Vol. 70, No. 205 / Tuesday, October 25, 2005 / Proposed Rules 61583 

AFM Revision 

(g) Within 25 flight hours after the effective 

date of this AD: Revise the Limitations 

section of the applicable Cessna airplane 

flight manual (AFM) to prohibit use of the 

wing fuel boost pumps for defueling under 

certain conditions, by inserting the 

applicable temporary change identified in 

Cessna Service Bulletin SB550–28–14, dated 

December 2, 2003, or identified in Table 3 of 

this AD. 

TABLE 3.—TEMPORARY CHANGES

Cessna temporary change— Dated— To the—

500FM TC–R57–01 ............................................. April 5, 2004 ........................................................ Cessna Model 500 AFM. 

500FM TC–R57–02 ............................................. April 5, 2004 ........................................................ Cessna Model 500 AFM. 

500FM TC–R57–03 ............................................. April 5, 2004 ........................................................ Cessna Model 500 AFM. 

55BFM TC–R10–07 ............................................. March 17, 2004 ................................................... Cessna Model 550 Citation Bravo AFM. 

55BFM TC–R10–08 ............................................. March 17, 2004 ................................................... Cessna Model 550 Citation Bravo AFM. 

55BFM TC–R10–09 ............................................. March 17, 2004 ................................................... Cessna Model 550 Citation Bravo AFM. 

560FM TC–R13–01 ............................................. March 4, 2004 ..................................................... Cessna Model 560 Citation V AFM. 

560FM TC–R13–02 ............................................. March 4, 2004 ..................................................... Cessna Model 560 Citation V AFM. 

560FM TC–R13–03 ............................................. March 4, 2004 ..................................................... Cessna Model 560 Citation V AFM. 

56FMA TC–04–01 ............................................... March 4, 2004 ..................................................... Cessna Model 560 Citation Ultra AFM. 

56FMA TC–04–02 ............................................... March 4, 2004 ..................................................... Cessna Model 560 Citation Ultra AFM. 

56FMA TC–04–03 ............................................... March 4, 2004 ..................................................... Cessna Model 560 Citation Ultra AFM. 

56FMB TC–R03–10 ............................................. March 12, 2004 ................................................... Cessna Model 560 AFM. 

56FMB TC–R03–11 ............................................. March 12, 2004 ................................................... Cessna Model 560 AFM. 

56FMB TC–R03–12 ............................................. March 12, 2004 ................................................... Cessna Model 560 AFM. 

S55CA TC–04–01 ................................................ July 8, 2004 ......................................................... Cessna Model S550 Citation S/II AFM. 

S55CA TC–04–02 ................................................ July 8, 2004 ......................................................... Cessna Model S550 Citation S/II AFM. 

S55CA TC–04–03 ................................................ July 8, 2004 ......................................................... Cessna Model S550 Citation S/II AFM. 

S55FM TC–04–01 ............................................... March 4, 2004 ..................................................... Cessna Model S550 Citation S/II AFM. 

S55FM TC–04–02 ............................................... March 4, 2004 ..................................................... Cessna Model S550 Citation S/II AFM. 

S55FM TC–04–03 ............................................... March 4, 2004 ..................................................... Cessna Model S550 Citation S/II AFM. 

Placard Installation 

(h) Within 25 flight hours after the effective 

date of this AD: Install a placard close to the 

fuel quantity gauge, in accordance with the 

Accomplishment Instructions of the service 

bulletin. In addition to the specifications in 

the service bulletin, the letters on the placard 

must be at least 1⁄4-inch tall. 

Inspection and Modification 

(i) Within 300 flight hours after the 

effective date of this AD: Do the actions 

specified in paragraphs (i)(1) and (i)(2) of this 

AD in accordance with the Accomplishment 

Instructions of the service bulletin. 

(1) Do a detailed inspection for chafed 

wiring of the wing fuel boost pumps, and, 

before further flight thereafter, do all 

applicable corrective and other specified 

actions. 

(2) Modify the wing fuel boost pumps. 

Note 1: 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.’’ 

(j) Before further flight after the inspection 

and modification required by paragraph (i) of 

this AD, remove the AFM temporary change 

and placard required by paragraphs (g) and 

(h) of this AD. 

Reporting Clarification 

(k) Although the service bulletin specifies 

to submit certain information to the 

manufacturer, this AD does not include that 

requirement. 

Alternative Methods of Compliance 

(AMOCs) 

(l) The Manager, Wichita Aircraft 

Certification Office (ACO), FAA, has the 

authority to approve AMOCs for this AD, if 

requested in accordance with the procedures 

found in 14 CFR 39.19. 

Issued in Renton, Washington, on October 

18, 2005. 

Kevin M. Mullin, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 05–21309 Filed 10–24–05; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 71 

[Docket No. FAA–2005–22538; Airspace 

Docket No. 05–AAL–30] 

Proposed Revision of Class E 

Airspace; Koliganek, AK 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Notice of proposed rulemaking. 

SUMMARY: This action proposes to revise 

Class E airspace at Koliganek, AK. Two 

new Standard Instrument Approach 

Procedures (SIAPs) are being published 

for the Koliganek Airport. Additional 

Class E Airspace is needed to contain 

aircraft executing instrument 

approaches at Koliganek Airport. 

Adoption of this proposal would result 

in additional Class E airspace upward 

from 1,200 feet (ft.) above the surface at 

Koliganek, AK. 

DATES: Comments must be received on 

or before December 9, 2005. 

ADDRESSES: Send comments on the 

proposal to the Docket Management 

System, U.S. Department of 

Transportation, Room Plaza 401, 400 

Seventh Street, SW., Washington, DC 

20590–0001. You must identify the 

docket number FAA–2005–22538/ 

Airspace Docket No. 05–AAL–30, at the 

beginning of your comments. You may 

also submit comments on the Internet at 

http://dms.dot.gov. You may review the 

public docket containing the proposal, 

any comments received, and any final 

disposition in person in the Dockets 

Office between 9 a.m. and 5 p.m., 

Monday through Friday, except Federal 

holidays. The Docket Office (telephone 

1–800–647–5527) is on the plaza level 

of the Department of Transportation 

NASSIF Building at the above address. 

An informal docket may also be 

examined during normal business hours 

at the office of the Manager, Safety, 

Alaska Flight Service Operations, 

Federal Aviation Administration, AAL– 

530, 222 West 7th Avenue, Box 14, 

Anchorage, AK 99513–7587. 

FOR FURTHER INFORMATION CONTACT: Gary 

Rolf, Federal Aviation Administration, 

222 West 7th Avenue, Box 14, 

Anchorage, AK 99513–7587; telephone 

number (907) 271–5898; fax: (907) 271– 

2850; e-mail: gary.ctr.rolf@faa.gov.