Federal Register / Vol. 75, No. 7 / Tuesday, January 12, 2010 / Rules and Regulations 1527 

Authority: 7 U.S.C. 601–674. 

■ 2. Section 984.445 is revised to read 

as follows: 

§ 984.445 Procedures for voting by mail, email, telephone, videoconference, facsimile, 

or any other means of communication. 

(a) Whenever the Board votes upon 

any proposition by mail, e-mail, or 

facsimile, at least six members or 

alternates acting as members must vote 

and one dissenting vote shall prevent its 

adoption. Each proposition to be voted 

upon by mail, e-mail, or facsimile shall 

specify a time limit for members to vote, 

after which the alternates shall be given 

the opportunity to vote. 

(b) Whenever the Board conducts 

meetings by telephone, 

videoconference, or any technology that 

enables member interaction, the vote 

shall be conducted by roll call. 

Dated: January 6, 2010. 

David R. Shipman, 

Acting Administrator, Agricultural Marketing 

Service. 

[FR Doc. 2010–316 Filed 1–11–10; 8:45 am] 

BILLING CODE 3410–02–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 25 

[Docket No. NM405, Special Conditions No. 

25–394–SC] 

Special Conditions: Bombardier, Inc., 

Model DHC–8–100, –200, –300, and 

–400 Series Airplanes; Passenger 

Seats With Non-Traditional, Large, 

Non-Metallic Panels 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final special conditions; request 

for comments; correction. 

SUMMARY: This document makes a 

correction to a Final special conditions; 

request for comment document, 

published in the Federal Register on 

June 5, 2009 (74 FR 26946), which 

issued special conditions for the 

Bombardier, Inc., Model DHC–8–100, 

–200, –300, and –400 series airplanes, 

for passenger seats with non-traditional, 

large, non-metallic panels. The Final 

special conditions; request for comment 

document, included an incorrect 

Special Conditions number. 

FOR FURTHER INFORMATION CONTACT: 

Michael Menkin, FAA, Standardization 

Branch, ANM–113, Transport Airplane 

Directorate, Aircraft Certification 

Service, 1601 Lind Avenue, SW., 

Renton, Washington 98057–3356; 

telephone (425) 227–22793 facsimile 

(425) 227–1230; or e-mail: 

Michael.Menkin@faa.gov. 

SUPPLEMENTARY INFORMATION: The 

document designated as ‘‘Docket No. 

NM405, Special Conditions No. 25– 

283–SC’’ was published in the Federal 

Register on June 5, 2009 (74 FR 26946). 

The document issued special conditions 

pertaining to passenger seats with nontraditional, large, non-metallic panels 

for the Bombardier, Inc., Model DHC–8– 

100, –200, –300, and –400 series 

airplanes. 

As published, the document 

contained an incorrect Special 

Conditions number; one that was used 

for a different set of special conditions. 

To correct that problem, the special 

conditions number pertaining to these 

special conditions is being changed. 

Since no part of the regulatory 

information has been changed, the 

special conditions are not being 

republished. 

Correction 

In Final special conditions; request 

for comment document FR Doc. E9– 

13187, published on June 5, 2009 (74 FR 

26946), make the following correction: 

1. On page 26946, in the first column, 

fifth line, change No. 25–283–SC to No. 

25–394–SC. 

Issued in Renton, Washington, on 

December 28, 2009. 

Ali Bahrami, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2010–290 Filed 1–11–10; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2009–0788; Directorate 

Identifier 2009–NM–193–AD; Amendment 

39–16167; AD 2010–01–09] 

RIN 2120–AA64 

Airworthiness Directives; The Boeing 

Company Model 737–300, –400, and 

–500 Series Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 

Model 737–300, –400, and –500 series 

airplanes. This AD requires repetitive 

external non-destructive inspections to 

detect cracks in the fuselage skin along 

the chem-mill step at stringers S–1 and 

S–2 right, between station (STA) 827 

and STA 847, and repair if necessary. 

This AD results from a report of a hole 

in the fuselage skin common to stringer 

S–1 and S–2 left, between STA 827 and 

STA 847 on an airplane that diverted to 

an alternate airport due to cabin 

depressurization and subsequent 

deployment of the oxygen masks. We 

are issuing this AD to detect and correct 

fatigue cracking of the fuselage skin 

panels at the chem-milled steps, which 

could result in sudden fracture and 

failure of the fuselage skin panels, and 

consequent rapid decompression of the 

airplane. 

DATES: This AD is effective February 16, 

2010. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in the AD 

as of February 16, 2010. 

ADDRESSES: For service information 

identified in this AD, contact Boeing 

Commercial Airplanes, Attention: Data 

& Services Management, P.O. Box 3707, 

MC 2H–65, Seattle, Washington 98124– 

2207; telephone 206–544–5000, 

extension 1; fax 206–766–5680; e-mail 

me.boecom@boeing.com; Internet 

https://www.myboeingfleet.com. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http:// 

www.regulations.gov; or in person at the 

Docket Management Facility between 9 

a.m. and 5 p.m., Monday through 

Friday, except Federal holidays. The AD 

docket contains this AD, the regulatory 

evaluation, any comments received, and 

other information. The address for the 

Docket Office (telephone 800–647–5527) 

is the Document Management Facility, 

U.S. Department of Transportation, 

Docket Operations, M–30, West 

Building Ground Floor, Room W12–140, 

1200 New Jersey Avenue, SE., 

Washington, DC 20590. 

FOR FURTHER INFORMATION CONTACT: 

Wayne Lockett, Aerospace Engineer, 

Airframe Branch, ANM–120S, FAA, 

Seattle Aircraft Certification Office, 

1601 Lind Avenue, SW., Renton, 

Washington 98057–3356; telephone 

(425) 917–6447; fax (425) 917–6590. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 to include an airworthiness 

directive (AD) that would apply to 

certain Model 737–300, –400, and –500 

series airplanes. That NPRM was 

published in the Federal Register on 

September 15, 2009 (74 FR 47148). That 

NPRM proposed to require repetitive 

WReier-Aviles on DSKGBLS3C1PROD with RULES