[Federal Register Volume 76, Number 87 (Thursday, May 5, 2011)]
[Rules and Regulations]
[Pages 25534-25535]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2011-10898]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2009-0113; Directorate Identifier 2008-NE-25-AD;
Amendment 39-16602; AD 2011-04-02]
RIN 2120-AA64
Airworthiness Directives; Hamilton Sundstrand Propellers Model
247F Propellers
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; correction.
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SUMMARY: The FAA is correcting an airworthiness directive (AD) that
published in the Federal Register. That AD applies to the products
listed above. The blade part number (P/N) 817370-1 in the SUPPLEMENTARY
INFORMATION, the Applicability, and the Compliance sections is
incorrect. We are also adding a statement to the Compliance section to
clarify the applicability. This document corrects those errors. In all
other respects, the original document remains the same.
DATES: This final rule is effective May 5, 2011.
ADDRESSES: You may examine the AD docket on the Internet at http://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
[[Page 25535]]
Docket Office (phone: 800-647-5527) is 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: Michael Schwetz, Aerospace Engineer,
Boston Aircraft Certification Office, FAA, Engine and Propeller
Directorate, 12 New England Executive Park, Burlington, MA 01803;
telephone (781) 238-7761; fax (781) 238-7170; e-mail:
[email protected].
SUPPLEMENTARY INFORMATION: Airworthiness Directive 2011-04-02,
amendment 39-16602 (76 FR 7101, February 9, 2011), currently requires
removing from service, certain part number and serial number propeller
blades for Hamilton Sundstrand Propellers Model 247F Propellers.
As published, the propeller blade part number 817370-1 and ATR72-
210 and ATR722-210E airplanes in the SUPPLEMENTARY INFORMATION, the
Applicability, and the Compliance sections are incorrect.
No other part of the preamble or regulatory information has been
changed; therefore, only the changed portion of the final rule is being
published in the Federal Register.
The effective date of this AD remains March 16, 2011.
Correction of Non-Regulatory Text
In the Federal Register of February 9, 2011, AD 2011-04-02;
Amendment 39-16602 is corrected as follows:
On page 7101 in the third column, on line 26, SUPPLEMENTARY
INFORMATION, change ``817370-1'' to ``R817370-1''.
On page 7101 in the third column, on line 33, SUPPLEMENTARY
INFORMATION, change ``817370-1'' to ``R817370-1''.
Correction of Regulatory Text
Sec. 39.13 [Corrected]
In the Federal Register of February 9, 2011, on page 7102, in the
second column, paragraph (c) of AD 2011-04-02 is corrected to read as
follows:
* * * * *
(c) This AD applies to Hamilton Sundstrand model 247F series
propellers with blades part number (P/N) R817370-1, serial numbers (S/
Ns) FR2018, FR2103, FR2108, FR2109, FR2111, FR2123, FR2183, FR2187,
FR2262, FR2276 through FR2279 inclusive, FR 2398, FR2449 to FR2958
inclusive, FR20010710 to FR20010722 inclusive, and FR20010723RT to
FR20020127RT inclusive, installed. Propeller blades reworked to
Hamilton Sundstrand Service Bulletin 247F-61-54 with the part number
re-marked as R817370R1 are in compliance with this AD.
* * * * *
In the Federal Register of February 9, 2011, on page 7102, in the
second column, paragraph (f) of AD 2011-04-02 is corrected to read as
follows:
* * * * *
Removing Blades P/N R817370-1
(f) Remove from service, blades P/N R817370-1, S/Ns FR2018, FR2103,
FR2108, FR2109, FR2111, FR2123, FR2183, FR2187, FR2262, FR2276 through
FR2279, FR2398, FR2449 to FR2958 inclusive, FR20010710 to FR20010722
inclusive, and FR20010723RT to FR20020127RT inclusive, within 30 days
after the effective date of this AD.
* * * * *
Issued in Burlington, Massachusetts, on April 29, 2011.
Peter A. White,
Acting Manager, Engine & Propeller Directorate, Aircraft Certification
Service.
[FR Doc. 2011-10898 Filed 5-4-11; 8:45 am]
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