曝光臺(tái) 注意防騙 網(wǎng)曝天貓店富美金盛家居專營(yíng)店坑蒙拐騙欺詐消費(fèi)者

I. General Information
A. Does this action apply to me?
B. Where can I get a copy of this document
and other related information?
C. How is this preamble organized?
II. This Action
A. Background
B. Final Rule
C. Comments and Responses
D. Basis for Making This Rule Effective on
the Date of Publication
III. Statutory and Executive Order Review
A. Executive Order 12866: Regulatory
Planning and Review
B. Paperwork Reduction Act
C. Regulatory Flexibility Act
D. Unfunded Mandates Reform Act
E. Executive Order 13132: Federalism
F. Executive Order 13175: Consultation
and Coordination With Indian Tribal
Governments
G. Executive Order 13045: Protection of
Children From Environmental Health
and Safety Risks
H. Executive Order 13211: Actions
Concerning Regulations That
Significantly Affect Energy Supply,
Distribution, or Use
I. National Technology Transfer and
Advancement Act
J. Executive Order 12898: Federal Actions
To Address Environmental Justice in
Minority Populations and Low-Income
Populations
K. Determination Under Section 307(d)
L. The Congressional Review Act
M. Basis for Making This Rule Effective on
the Date of Publication
IV. Statutory Authority
II. This Action
A. Background
On May 16, 2008, the EPA (‘‘we’’)
issued a final rule amending our PSD
and nonattainment NSR regulations to
add requirements for the
preconstruction review of PM2.5. 73 FR
28321. The amendments addressed the
major source threshold, significant
emissions rate and offset ratios for
PM2.5; interpollutant trading for offsets;
and applicability of NSR to PM2.5
precursors. The rule also provided for
the transition of the new requirements
for PM2.5 in the NSR permitting process.
On February 10, 2009, Earthjustice, on
behalf of the Natural Resources Defense
Council (NRDC) and Sierra Club,
submitted a petition for reconsideration
of four specific provisions of the May
2008 final rule as provided for in Clean
Air Act (CAA) 307(d)(7)(B).1 The
specific provisions challenged by the
petitioners include: (1) A transition
period for PSD programs in States with
approved PSD rules in their approved
State Implementation Plans (SIPs) to
revise and submit their new PM2.5
regulations to EPA within three years of
the publication of the final rule. During
the transition period, the rule allows
States to continue using EPA’s 1997
surrogate policy by which an analysis
based on PM10 can be used to meet the
requirements for the otherwise required
PM2.5; (2) ‘‘grandfathering’’ under the
Federal PSD program for permit
applications submitted before the July
15, 2008, effective date of the new rule,
which allows the PM10 surrogate policy
to continue to be used as the basis for
approving such permits for PM2.5; (3) a
transition period, during which time
EPA is re-evaluating its test methods for
condensable particulate matter (CPM)
emissions, whereby States are not
required to account for CPM in the
permitting process; and (4) use of
recommended interpollutant trading
ratios to facilitate the trading of PM2.5
precursors emissions reductions for new
VerDate Nov<24>2008 15:26 Sep 21, 2009 Jkt 217001 PO 00000 Frm 00019 Fmt 4700 Sfmt 4700 E:\FR\FM\22SER1.SGM 22SER1 erowe on DSK5CLS3C1PROD with RULES
MINISTÉRIO DA AERONÁUTICA
DEPARTAMENTO DE PESQUISAS E DESENVOLVIMENTO
CENTRO TÉCNICO AEROESPACIAL
TYPE CERTIFICATE DATA SHEET Nº EA-8002-01
Type Certificate Holder:
AIRBUS INDUSTRIE
1, Rond-point Maurice Bellonte
31707 Blagnac
FRANCE
EA-8002-01
Sheet 01
AIRBUS
A300B2-203, A300B4-203;
A310-203, -204, -221, -222,
A310-304, -308, -322, -324, -325
March 1999
This data sheet, which is part of Type Certificate No. 8002, prescribes conditions and limitations under which the
product, for which the Type Certificate was issued, meets the airworthiness requirements of the Brazilian
Aeronautical Regulations.
I - Model A300B2-203 (Transport Category), approved 13 August 1982.
ENGINE Two General Electric model CF6-50C2 turbofan engines.
MAXIMUM WEIGHT (kg)
VARIANT
Basic
Model
001 with
SB 34.025 embodied
(mod. 1569)
Max. Ramp Weight 142 900 137 900
Max. Take-off Weight 142 000 137 000
Max. Landing Weight 130 000 130 000
Max. Zero Fuel Weight 120 500 120 500
CG RANGE Forward Aft
　
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