This section of the FEDERAL REGISTER

contains regulatory documents having general

applicability and legal effect, most of which

are keyed to and codified in the Code of

Federal Regulations, which is published under

50 titles pursuant to 44 U.S.C. 1510.

The Code of Federal Regulations is sold by

the Superintendent of Documents. Prices of

new books are listed in the first FEDERAL

REGISTER issue of each week.

Rules and Regulations Federal Register

10455 

Vol. 74, No. 46 

Wednesday, March 11, 2009 

DEPARTMENT OF HOMELAND 

SECURITY 

U.S. Citizenship and Immigration 

Services 

8 CFR Part 274a 

[CIS No. 2441–08; Docket No. USCIS–2008– 

0001] 

RIN 1615–AB69 

Documents Acceptable for 

Employment Eligibility Verification; 

Correction 

AGENCY: U.S. Citizenship and 

Immigration Services, DHS. 

ACTION: Interim rule; correction. 

SUMMARY: On December 17, 2008, the 

Department of Homeland Security 

(DHS) published an interim rule in the 

Federal Register amending its 

regulations governing the types of 

acceptable identity and employment 

authorization documents and receipts 

for completion of the Form I–9, 

Employment Eligibility Verification. On 

February 3, 2009, USCIS delayed the 

effective date of the interim rule until 

April 3, 2009. On February 23, 2009, 

DHS published a final rule that 

amended the same section of the Code 

of Federal Regulations (CFR) as the 

interim rule, resulting in an inadvertent 

error in the interim rule’s amendatory 

language. This document corrects that 

inadvertent error. 

DATES: Effective Date: This correction is 

effective April 3, 2009. 

FOR FURTHER INFORMATION CONTACT: 

Stephen McHale, Verification Division, 

U.S. Citizenship and Immigration 

Services, Department of Homeland 

Security, 470 L’Enfant Plaza East, SW., 

Suite 8001, Washington, DC 20529– 

2600, telephone (888) 464–4218 or email at Everify@dhs.gov. 

SUPPLEMENTARY INFORMATION: 

Need for Correction 

On December 17, 2008, DHS 

published an interim rule in the Federal 

Register at 73 FR 76505. The interim 

rule amended 8 CFR 274a.2 by revising 

paragraph (b)(1)(v)(A). 

On February 3, 2009, DHS published 

a document in the Federal Register at 

74 FR 5899, delaying the effective date 

of the December 17th interim rule until 

April 3, 2009, and extending the 

comment period until March 4, 2009. 

This extension was necessary to allow 

for further review and consideration of 

the interim rule by DHS officials. 

On February 23, 2009, DHS published 

a final rule in the Federal Register at 74 

FR 7993, providing for employerspecific employment authorization for 

certain aliens lawfully enlisted in the 

U.S. Armed Forces. The final rule 

became effective on February 23, 2009, 

and amended 8 CFR 274a.2 by: 

• Adding and reserving paragraph 

(b)(1)(v)(A)(6) and by 

• Adding paragraph (b)(1)(v)(A)(7). 

Since the December 17th interim rule 

becomes effective after the February 

23rd final rule, the amendatory language 

revising 8 CFR 274a.2(b)(1)(v)(A) in the 

interim rule would inadvertently 

remove the new paragraph 

(b)(1)(v)(A)(7) of the final rule. This 

correction will fix that inadvertent error. 

Correction of Publication 

■ Accordingly, the publication on 

December 17, 2008 (73 FR 76505) of the 

interim rule that was the subject of FR 

Doc. E8–29874 is corrected as follows: 

PART 274a—CONTROL OF 

EMPLOYMENT OF ALIENS 

§ 274a.2 [Corrected] 

■ 1. On page 76511, in the first column, 

instruction 2d should be revised to read: 

‘‘Revising paragraphs (b)(1)(v)(A)(1) 

through (5), and adding paragraph 

(b)(1)(v)(A)(6);’’ 

■ 2. On page 76511, in the first column, 

add an instruction immediately after 

instruction 2d to read: ‘‘Paragraph 

(b)(1)(v)(A) is further amended by 

removing the period at the end of 

paragraph (b)(1)(v)(A)(6) and adding a ‘‘; 

‘‘ in its place. 

Dated: March 5, 2009. 

Michael Aytes, 

Acting Deputy Director, U.S. Citizenship and 

Immigration Services. 

[FR Doc. E9–5164 Filed 3–10–09; 8:45 am] 

BILLING CODE 9111–97–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2008–1319; Directorate 

Identifier 2008–CE–071–AD; Amendment 

39–15836; AD 2009–05–12] 

RIN 2120–AA64 

Airworthiness Directives; Cessna 

Aircraft Company Models 208 and 

208B Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 

Cessna Aircraft Company (Cessna) 

Models 208 and 208B airplanes. This 

AD requires you to modify the aileron 

carry-through cable attachment to the 

aileron upper quadrant with parts of 

improved design. This AD results from 

reports of a ‘‘catch’’ in the aileron 

control system when the control yoke is 

turned. We are issuing this AD to 

prevent the cable attach fitting on the 

aileron upper quadrant assembly from 

rotating and possibly contacting or 

interfering with the aileron lower 

quadrant assembly, which could result 

in limited roll control and reduced 

handling capabilities. 

DATES: This AD becomes effective on 

April 15, 2009. 

On April 15, 2009, the Director of the 

Federal Register approved the 

incorporation by reference of certain 

publications listed in this AD. 

ADDRESSES: For service information 

identified in this AD, contact Cessna 

Aircraft Company, P.O. Box 7704, 

Wichita, Kansas 67277; telephone: (800) 

423–7762 or (316) 517–6056; Internet: 

http://www.cessna.com. 

To view the AD docket, go to U.S. 

Department of Transportation, Docket 

Operations, M–30, West Building 

Ground Floor, Room W12–140, 1200 

New Jersey Avenue, SE., Washington, 


rwilkins on PROD1PC63 with RULES
10456 Federal Register / Vol. 74, No. 46 / Wednesday, March 11, 2009 / Rules and Regulations 

DC 20590, or on the Internet at http:// 

www.regulations.gov. The docket 

number is FAA–2008–1319; Directorate 

Identifier 2008–CE–071–AD. 

FOR FURTHER INFORMATION CONTACT: Ann 

Johnson, Aerospace Engineer, FAA, 

Wichita Aircraft Certification Office, 

1801 Airport Road, Room 100, Wichita, 

Kansas 67209; telephone: 316–946– 

4105; fax: 316–946–4107; e-mail 

address: ann.johnson@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Discussion 

On December 12, 2008, we issued a 

proposal to amend part 39 of the Federal 

Aviation Regulations (14 CFR part 39) to 

include an AD that would apply to 

certain Cessna Models 208 and 208B 

airplanes.This proposal was published 

in the Federal Register as a notice of 

proposed rulemaking (NPRM) on 

December 18, 2008 (73 FR 76979). The 

NPRM proposed to require you to 

modify the aileron carry-through cable 

attachment to the aileron upper 

quadrant with parts of improved design. 

Comments 

We provided the public the 

opportunity to participate in developing 

this AD. We received no comments on 

the proposal or on the determination of 

the cost to the public. 

Conclusion 

We have carefully reviewed the 

available data and determined that air 

safety and the public interest require 

adopting the AD as proposed except for 

minor editorial corrections. We have 

determined that these minor 

corrections: 

• Are consistent with the intent that 

was proposed in the NPRM for 

correcting the unsafe condition; and 

• Do not add any additional burden 

upon the public than was already 

proposed in the NPRM. 

Costs of Compliance 

We estimate that this AD affects 794 

airplanes in the U.S. registry. 

We estimate the following costs to do 

the modification: 

Labor cost Parts cost Total cost per 

airplane 

Total cost on 

U.S. operators 

2 work-hours × $80 per hour = $160 ................................................... Not applicable ............................... $160 $127,040 

We estimate the following costs to do 

any necessary repairs and replacements 

that will be required based on doing the 

modification. We have no way of 

determining the number of airplanes 

that may need these repairs or 

replacements. 

We estimate the following costs to do 

possible damage repair to the aileron 

lower quadrant assembly, if necessary: 

Labor cost Parts cost Total cost per 

airplane 

.5 work-hour × $80 per hour = $40 ........................................................................... Not applicable .......................................... $40 

We estimate the following costs to do 

possible removal and installation of the 

aileron lower quadrant assembly, if 

necessary: 

Labor cost Parts cost Total cost per 

airplane 

2 work-hours × $80 per hour = $160 ........................................................................ Not applicable .......................................... $160 

We estimate the following costs to do 

possible removal and installation of the 

headliner, if necessary: 

Labor cost Parts cost Total cost per 

airplane 

16 work-hours × $80 per hour = $1,280 ................................................................... Not applicable .......................................... $1,280 

Warranty credit will be given for parts 

and labor to the extent specified in the 

manufacturer’s service bulletin. 

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 AD. 

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. 


rwilkins on PROD1PC63 with RULES
Federal Register / Vol. 74, No. 46 / Wednesday, March 11, 2009 / Rules and Regulations 10457 

For the reasons discussed above, I 

certify that this AD: 

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 summary of the costs 

to comply with this AD (and other 

information as included in the 

Regulatory Evaluation) and placed it in 

the AD Docket. You may get a copy of 

this summary by sending a request to us 

at the address listed under ADDRESSES. 

Include ‘‘Docket No. FAA–2008–1319; 

Directorate Identifier 2008–CE–071– 

AD’’ in your request. 

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 Federal Aviation Administration 

amends part 39 of the Federal Aviation 

Regulations (14 CFR part 39) as follows: 

PART 39—AIRWORTHINESS 

DIRECTIVES 

■ 1. The authority citation for part 39 

continues to read as follows: 

Authority: 49 U.S.C. 106(g), 40113, 44701. 

§ 39.13 [Amended] 

■ 2. FAA amends § 39.13 by adding the 

following new AD: 

2009–05–12 Cessna Aircraft Company: 

Amendment 39–15836; Docket No. 

FAA–2008–1319; Directorate Identifier 

2008–CE–071–AD. 

Effective Date 

(a) This AD becomes effective on April 15, 

2009. 

Affected ADs 

(b) None. 

Applicability 

(c) This AD applies to the following 

airplane models and serial numbers that are 

certificated in any category: 

Model Serial Nos. 

208 ............... 20800001 through 20800415 and 20800417 through 20800419. 

208B ............. 208B0001 through 208B1081, 208B1083 through 208B1215, 208B1217 through 208B1257, 208B1259 through 208B1305, 

208B1307, and 208B1309 through 208B1310. 

Unsafe Condition 

(d) This AD results from reports of a 

‘‘catch’’ in the aileron control system when 

the control yoke is turned. We are issuing 

this AD to prevent the cable attach fitting on 

the aileron upper quadrant assembly from 

rotating and possibly contacting or 

interfering with the aileron lower quadrant 

assembly, which could result in limited roll 

control and reduced handling capabilities. 

Compliance 

(e) To address this problem, you must do 

the following, unless already done: 

Actions Compliance Procedures 

Modify the aileron carry-through cable attachment to the aileron upper quadrant with parts 

of improved design.

Within the next 100 hours time-in-service after 

April 15, 2009 (the effective date of this AD) 

or within the next 6 months after April 15, 

2009 (the effective date of this AD), whichever occurs first.

Follow the Accomplishment Instructions in 

Cessna Caravan Service Bulletin CAB08–6, 

dated October 27, 2008. 

Alternative Methods of Compliance 

(AMOCs) 

(f) The Manager, Wichita Aircraft 

Certification Office (ACO), 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: Ann 

Johnson, Aerospace Engineer, FAA, Wichita 

Aircraft Certification Office, 1801 Airport 

Road, Room 100, Wichita, Kansas 67209; 

telephone: 316–946–4105; fax: 316–946– 

4107; e-mail address: ann.johnson@faa.gov. 

Before using any approved AMOC on any 

airplane to which the AMOC applies, notify 

your appropriate principal inspector (PI) in 

the FAA Flight Standards District Office 

(FSDO), or lacking a PI, your local FSDO. 

Material Incorporated by Reference 

(g) You must use Cessna Caravan Service 

Bulletin CAB08–6, dated October 27, 2008, to 

do the actions required by this AD, unless the 

AD specifies otherwise. 

(1) The Director of the Federal Register 

approved the incorporation by reference of 

this service information under 5 U.S.C. 

552(a) and 1 CFR part 51. 

(2) For service information identified in 

this AD, contact Cessna Aircraft Company, 

P.O. Box 7704, Wichita, Kansas 67277; 

telephone: (800) 423–7762 or (316) 517–6056; 

Internet: http://www.cessna.com. 

(3) You may review copies of the service 

information incorporated by reference for 

this AD at the FAA, Central Region, Office of 

the Regional Counsel, 901 Locust, Kansas 

City, Missouri 64106. For information on the 

availability of this material at the Central 

Region, call (816) 329–3768. 

(4) You may also review copies of the 

service information incorporated by reference 

for this AD at the National Archives and 

Records Administration (NARA). For 

information on the availability of this 

material at NARA, call (202) 741–6030, or go 

to: http://www.archives.gov/federal_register/ 

code_of_federal_regulations/ 

ibr_locations.html. 

Issued in Kansas City, Missouri, on 

February 27, 2009. 

John Colomy, 

Acting Manager, Small Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. E9–4828 Filed 3–10–09; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2008–1318; Directorate 

Identifier 2008–NM–155–AD; Amendment 

39–15848; AD 2009–06–12] 

RIN 2120–AA64 

Airworthiness Directives; Bombardier 

Model CL–600–2B19 (Regional Jet 

Series 100 & 440) Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: We are superseding an 

existing airworthiness directive (AD) for 

the products listed above. This AD 

results from mandatory continuing 

airworthiness information (MCAI) 

originated by an aviation authority of 

another country to identify and correct 


rwilkins on PROD1PC63 with RULES