Civil Penalty Factors; Withdrawal of Proposed Rule, 45133 [Z9-20590]
Download as PDF
<![CDATA[
45133
Proposed Rules
Federal Register
Vol. 74, No. 168
Tuesday, September 1, 2009
This section of the FEDERAL REGISTER
contains notices to the public of the proposed
issuance of rules and regulations. The
purpose of these notices is to give interested
persons an opportunity to participate in the
rule making prior to the adoption of the final
rules.
CONSUMER PRODUCT SAFETY
COMMISSION
16 CFR Part 1119
Civil Penalty Factors; Withdrawal of
Proposed Rule
Correction
In proposed rule document E9–20590
beginning on page 43085 in the issue of
Wednesday, August 26, 2009 make the
following correction:
On page 43085, in the first column,
the last paragraph should read ‘‘In a
forthcoming issue of the Federal
Register, the Commission is issuing a
new interim final rule to interpret the
penalty factors pursuant to section 217
of the CPSIA.’’
[FR Doc. Z9–20590 Filed 8–31–09; 8:45 am]
BILLING CODE 1505–01–D
fuel temperature. The applicable
airworthiness regulations do not contain
adequate or appropriate safety standards
for this design feature. These proposed
special conditions contain the
additional safety standards that the
Administrator considers necessary to
establish a level of safety equivalent to
that established by the existing
airworthiness standards.
DATES: Comments must be received on
or before October 1, 2009.
ADDRESSES: Comments on this proposal
may be mailed in duplicate to: Federal
Aviation Administration, Regional
Counsel, ACE–7, Attention: Rules
Docket, Docket No. CE299, 901 Locust,
Room 506, Kansas City, Missouri 64106,
or delivered in duplicate to the Regional
Counsel at the above address.
Comments must be marked: CE299.
Comments may be inspected in the
Rules Docket weekdays, except Federal
holidays, between 7:30 a.m. and 4 p.m.
FOR FURTHER INFORMATION CONTACT:
Peter L. Rouse, Federal Aviation
Administration, Aircraft Certification
Service, Small Airplane Directorate,
ACE–111, 901 Locust, Kansas City,
Missouri, 816–329–4135, fax 816–329–
4090.
SUPPLEMENTARY INFORMATION:
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 23
[Docket No. CE299; Notice No. 23–09–03–
SC]
Special Conditions: Cessna Aircraft
Company, Model 525C; High Fuel
Temperature
mstockstill on DSKH9S0YB1PROD with PROPOSALS
AGENCY: Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed special
conditions.
SUMMARY: This notice proposes special
conditions for the Cessna Aircraft
Company, Model 525C airplane. This
airplane will have a novel or unusual
design feature(s) associated with high
VerDate Nov<24>2008
18:00 Aug 31, 2009
Jkt 217001
Comments Invited
Interested persons are invited to
participate in the making of these
proposed special conditions by
submitting such written data, views, or
arguments as they may desire.
Communications should identify the
regulatory docket or notice number and
be submitted in duplicate to the address
specified above. All communications
received on or before the closing date
for comments will be considered by the
Administrator. The proposals described
in this notice may be changed in light
of the comments received. All
comments received will be available in
the Rules Docket for examination by
interested persons, both before and after
the closing date for comments. A report
summarizing each substantive public
contact with FAA personnel concerning
PO 00000
Frm 00001
Fmt 4702
Sfmt 4702
this rulemaking will be filed in the
docket. Persons wishing the FAA to
acknowledge receipt of their comments
submitted in response to this notice
must include with those comments a
self-addressed, stamped postcard on
which the following statement is made:
‘‘Comments to CE299.’’ The postcard
will be date stamped and returned to the
commenter.
Background
On August 9, 2006, Cessna Aircraft
Company applied for an amendment to
Type Certificate Number A1WI to
include the new model 525C (CJ4). The
model 525C (CJ4), which is a derivative
of the model 525B (CJ3) currently
approved under Type Certificate
Number A1WI, is a commuter category,
low-winged monoplane with ‘‘T’’ tailed
vertical and horizontal stabilizers,
retractable tricycle type landing gear
and twin turbofan engines mounted on
the aircraft fuselage. The maximum
takeoff weight is 16,950 pounds, the
VMO/MMO is 305 KIAS/M 0.77 and
maximum altitude is 45,000 feet.
The Cessna Model 525C (CJ4) fuel
tank system is similar to other Cessna
Model 525 designs which use the
Williams FJ44 series of engine. The fuel
tank system is configured to reject
engine heat through the airplane fuel
tank system by using an engine oil/fuel
heat exchanger. Certified as part of the
engine, the engine oil/fuel heat
exchanger cools the oil and heats the
fuel. Over time the engine
manufacturers have optimized the
design, size, placement, and space
management of the oil/fuel heat
exchanger such that today’s engines
now reject more heat back into the
airplane fuel tank system than has
existed in the past. As can be seen by
the chart below we are now exposing
the fuel tank system and airplane to
temperatures above the critical
temperature test requirements of
§§ 23.961 and 23.965(d), which has been
the FAA standard for fuel system hot
weather operations and fuel tank test
and evaluation since 1951.
E:\FR\FM\01SEP1.SGM
01SEP1
]]>Agencies
[Federal Register Volume 74, Number 168 (Tuesday, September 1, 2009)]
[Proposed Rules]
[Page 45133]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: Z9-20590]
========================================================================
Proposed Rules
Federal Register
________________________________________________________________________
This section of the FEDERAL REGISTER contains notices to the public of
the proposed issuance of rules and regulations. The purpose of these
notices is to give interested persons an opportunity to participate in
the rule making prior to the adoption of the final rules.
========================================================================
Federal Register / Vol. 74, No. 168 / Tuesday, September 1, 2009 /
Proposed Rules
[[Page 45133]]
CONSUMER PRODUCT SAFETY COMMISSION
16 CFR Part 1119
Civil Penalty Factors; Withdrawal of Proposed Rule
Correction
In proposed rule document E9-20590 beginning on page 43085 in the
issue of Wednesday, August 26, 2009 make the following correction:
On page 43085, in the first column, the last paragraph should read
``In a forthcoming issue of the Federal Register, the Commission is
issuing a new interim final rule to interpret the penalty factors
pursuant to section 217 of the CPSIA.''
[FR Doc. Z9-20590 Filed 8-31-09; 8:45 am]
BILLING CODE 1505-01-D
