Airworthiness Directives; BAE Systems (Operations) Limited Model BAe 146-100A and 146-200A Series Airplanes, 45311 [E9-21039]
Download as PDF
<![CDATA[
Federal Register / Vol. 74, No. 169 / Wednesday, September 2, 2009 / Rules and Regulations
(4) A turbine entry gas temperature
equal to the maximum steady state
temperature approved for use during
periods longer than 20 seconds when
operating at conditions not associated
with 30-second or 2 minutes OEI
ratings. The requirement to run the test
at the maximum approved steady state
temperature may be waived by the FAA
if the applicant can demonstrate that
other testing provides substantiation of
the temperature effects when considered
in combination with the other
parameters identified in paragraphs
(b)(1), (b)(2) and (b)(3) of this section.
■ 6. Amend § 33.87 by revising
paragraph (a)(8) to read as follows:
§ 33.87
Endurance test.
(a) * * *
(8) If the number of occurrences of
either transient rotor shaft overspeed,
transient gas overtemperature or
transient engine overtorque is limited,
that number of the accelerations
required by paragraphs (b) through (g) of
this section must be made at the
limiting overspeed, overtemperature or
overtorque. If the number of occurrences
is not limited, half the required
accelerations must be made at the
limiting overspeed, overtemperature or
overtorque.
*
*
*
*
*
Issued in Washington, DC, on August 21,
2009.
J. Randolph Babbitt,
Administrator.
[FR Doc. E9–20960 Filed 9–1–09; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2009–0432; Directorate
Identifier 2008–NM–168–AD; Amendment
39–15982; AD 2009–15–19]
RIN 2120–AA64
Airworthiness Directives; BAE
Systems (Operations) Limited Model
BAe 146–100A and 146–200A Series
Airplanes
erowe on DSK5CLS3C1PROD with RULES
SUMMARY: The FAA is correcting a
typographical error in an existing
airworthiness directive (AD) that was
published in the Federal Register on
July 29, 2009. The error resulted in an
incorrect AD number appearing in one
Jkt 217001
Effective September 2, 2009.
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.
ADDRESSES:
FOR FURTHER INFORMATION CONTACT:
Todd Thompson, Aerospace Engineer,
International Branch, ANM–116,
Transport Airplane Directorate, FAA,
1601 Lind Avenue, SW., Renton,
Washington 98057–3356; telephone
(425) 227–1175; fax (425) 227–1149.
On July
13, 2009, the FAA issued AD 2009–15–
19, amendment 39–15982 (74 FR 37528,
July 29, 2009), for certain BAE Systems
(Operations) Limited Model BAe 146–
100A and 146–200A series airplanes.
This AD requires inspecting for damage
of the horizontal stabilizer lower skin
and joint plates, and doing related
investigative and corrective actions.
As published, the final rule
incorrectly specified the AD number in
a single location in the AD as ‘‘2008–
15–19’’ instead of ‘‘2009–15–19.’’
No other part of the regulatory
information has been changed;
therefore, the final rule is not
republished in the Federal Register.
The effective date of this AD remains
September 2, 2009.
SUPPLEMENTARY INFORMATION:
[Corrected]
In the Federal Register of July 29,
2009, on page 37529, in the first
column, paragraph 2. of PART 39—
AIRWORTHINESS DIRECTIVES is
corrected to read as follows:
*
*
*
*
*
■
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; correction.
15:07 Sep 01, 2009
DATES:
§ 39.13
AGENCY:
VerDate Nov<24>2008
location of the document. This AD
applies to certain BAE Systems
(Operations) Limited Model BAe 146–
100A and 146–200A series airplanes.
This AD requires inspecting for damage
of the horizontal stabilizer lower skin
and joint plates, and doing related
investigative and corrective actions.
2009–15–19 BAE Systems (Operations)
Limited (Formerly British Aerospace
Regional Aircraft): Amendment 39–
15982. Docket No. FAA–2009–0432;
Directorate Identifier 2008–NM–168–AD.
*
PO 00000
*
*
Frm 00007
*
Fmt 4700
*
Sfmt 4700
45311
Issued in Renton, Washington, on August
24, 2009.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E9–21039 Filed 9–1–09; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF HOUSING AND
URBAN DEVELOPMENT
24 CFR Part 206
[Docket No. FR–4989–F–02]
RIN 2502–AI34
Home Equity Conversion Mortgage
(HECM) Counseling Standardization
and Roster
AGENCY: Office of the Assistant
Secretary for Housing—Federal Housing
Commissioner, HUD.
ACTION: Final rule.
SUMMARY: This final rule amends HUD’s
HECM program regulations by
establishing testing standards to qualify
individuals as HECM counselors eligible
to provide HECM counseling to
prospective HECM borrowers. The rule
also establishes a HECM Counseling
Roster (Roster) of eligible HECM
counselors and provides for their
removal for cause. This rule is intended
to contribute to improving the quality of
HECM counseling. HECM counseling
enables elderly homeowners to make
more informed decisions when
considering mortgage options and
whether to pursue a HECM loan. This
final rule follows the publication of a
January 8, 2007, proposed rule, takes
into consideration the public comments
received on the proposed rule, and
makes certain changes in response to
public comment and upon further
consideration of certain issues by HUD.
DATES: Effective Date: October 2, 2009.
FOR FURTHER INFORMATION CONTACT:
Margaret Burns, Director, Office of
Single Family Program Development,
Office of Housing, Department of
Housing and Urban Development, 451
Seventh Street, SW., Room 9278,
Washington, DC 20410–8000; telephone
number 202–708–2121 (this is not a tollfree number). Hearing- and speechimpaired individuals may access this
number through TTY by calling the tollfree Federal Information Relay Service
at 800–877–8339.
SUPPLEMENTARY INFORMATION:
I. Background—The January 8, 2007
Proposed Rule
Section 255 of the National Housing
Act (12 U.S.C. 1715z–20) (NHA)
E:\FR\FM\02SER1.SGM
02SER1
]]>Agencies
[Federal Register Volume 74, Number 169 (Wednesday, September 2, 2009)]
[Rules and Regulations]
[Page 45311]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E9-21039]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2009-0432; Directorate Identifier 2008-NM-168-AD;
Amendment 39-15982; AD 2009-15-19]
RIN 2120-AA64
Airworthiness Directives; BAE Systems (Operations) Limited Model
BAe 146-100A and 146-200A Series Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; correction.
-----------------------------------------------------------------------
SUMMARY: The FAA is correcting a typographical error in an existing
airworthiness directive (AD) that was published in the Federal Register
on July 29, 2009. The error resulted in an incorrect AD number
appearing in one location of the document. This AD applies to certain
BAE Systems (Operations) Limited Model BAe 146-100A and 146-200A series
airplanes. This AD requires inspecting for damage of the horizontal
stabilizer lower skin and joint plates, and doing related investigative
and corrective actions.
DATES: Effective September 2, 2009.
ADDRESSES: 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: Todd Thompson, Aerospace Engineer,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425)
227-1175; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION: On July 13, 2009, the FAA issued AD 2009-15-
19, amendment 39-15982 (74 FR 37528, July 29, 2009), for certain BAE
Systems (Operations) Limited Model BAe 146-100A and 146-200A series
airplanes. This AD requires inspecting for damage of the horizontal
stabilizer lower skin and joint plates, and doing related investigative
and corrective actions.
As published, the final rule incorrectly specified the AD number in
a single location in the AD as ``2008-15-19'' instead of ``2009-15-
19.''
No other part of the regulatory information has been changed;
therefore, the final rule is not republished in the Federal Register.
The effective date of this AD remains September 2, 2009.
Sec. 39.13 [Corrected]
0
In the Federal Register of July 29, 2009, on page 37529, in the first
column, paragraph 2. of PART 39--AIRWORTHINESS DIRECTIVES is corrected
to read as follows:
* * * * *
2009-15-19 BAE Systems (Operations) Limited (Formerly British
Aerospace Regional Aircraft): Amendment 39-15982. Docket No. FAA-
2009-0432; Directorate Identifier 2008-NM-168-AD.
* * * * *
Issued in Renton, Washington, on August 24, 2009.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E9-21039 Filed 9-1-09; 8:45 am]
BILLING CODE 4910-13-P
