Airworthiness Directives; BAE Systems (Operations) Limited Model BAe 146-100A and 146-200A Series Airplanes, 45311 [E9-21039]

Download as PDF 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]


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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
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