Special Conditions: Bombardier, Inc., Model DHC-8-100, -200, -300, and -400 Series Airplanes; Passenger Seats With Non-Traditional, Large, Non-Metallic Panels, 1527 [2010-290]
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Federal Register / Vol. 75, No. 7 / Tuesday, January 12, 2010 / Rules and Regulations
Authority: 7 U.S.C. 601–674.
telephone (425) 227–22793 facsimile
(425) 227–1230; or e-mail:
Michael.Menkin@faa.gov.
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
Federal Aviation
Administration (FAA), DOT.
ACTION: Final special conditions; request
for comments; correction.
WReier-Aviles on DSKGBLS3C1PROD with RULES
AGENCY:
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;
VerDate Nov<24>2008
14:29 Jan 11, 2010
Jkt 220001
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.
SUPPLEMENTARY INFORMATION:
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
PO 00000
Frm 00003
Fmt 4700
Sfmt 4700
1527
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 https://
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
E:\FR\FM\12JAR1.SGM
12JAR1
]]>Agencies
[Federal Register Volume 75, Number 7 (Tuesday, January 12, 2010)]
[Rules and Regulations]
[Page 1527]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2010-290]
=======================================================================
-----------------------------------------------------------------------
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 non-traditional, 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
