[4910-13-P]

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2013-0262; Directorate Identifier 2013-NE-13-AD; Amendment 

39-17548; AD 2013-16-10]

RIN 2120-AA64

Airworthiness Directives; Hamilton Standard Division and Hamilton Sundstrand 

Corporation Propellers

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; correction.

SUMMARY: The FAA is correcting an airworthiness directive (AD) that published in 

the Federal Register. That AD applies to all Hamilton Standard Division model 6/5500/F 

and 24PF and Hamilton Sundstrand Corporation model 14RF, 14SF, 247F, and 568F 

series propellers. A maintenance manual number in paragraph (g) of the Compliance 

section is incorrect. This document corrects that error. In all other respects, the original 

document remains the same.

DATES: This final rule is effective [INSERT DATE OF PUBLICATION IN THE 

FEDERAL REGISTER]. The effective date for AD 2013-16-10 (78 FR 49660, August 

15, 2013) remains September 19, 2013.

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 Docket Office (phone: 800-647-5527) is Document 

Management Facility, U.S. Department of Transportation, Docket Operations, M-30, 
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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, 12 New England Executive Park, 

Burlington, MA 01803; phone: 781-238-7761; fax: 781-238-7170; email: 

michael.schwetz@faa.gov.

SUPPLEMENTARY INFORMATION: AD 2013-16-10, Amendment 39-17548 (78 

FR 49660, August 15, 2013), currently requires incorporating inspections, based on a 

calendar time, into the propeller maintenance schedule for Hamilton Standard Division 

model 6/5500/F and 24PF and Hamilton Sundstrand Corporation model 14RF, 14SF, 

247F, and 568F series propellers.

As published, the maintenance manual number, P4202, as part of the 

model/manual number, 247F-1/P4202, in paragraph (g) of the Compliance section is 

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 for AD 2013-16-10 (78 FR 49660, August 15, 2013) remains 

September 19, 2013.

Correction of Regulatory Text

§ 39.13 [Corrected]

In the Federal Register of August 15, 2013, on page 49662, in the 1

st column, 

paragraph (g) of AD 2013-16-10 is corrected to read as follows:

* * * * *
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(g) MI for Blades and Hubs That Do Not Have an Updated ALS

For Hamilton Standard Division propeller models 6/5500/F and 24PF and 

Hamilton Sundstrand Corporation propeller models 14RF-19, 14RF-37, 14SF-11, 14SF15, 14SF-23, 14SF-17, 14SF-19, 247F-1, 247F-1E, 247F-3, 568F-1, 568F-5, and 568F-7, 

that do not have an approved update to the ALS, within one year after the effective date 

of this AD, perform an MI on the blades and hubs no later than seven years after the DSI. 

The DSI will begin at initial installation after the most recent MI or initial installation 

after production. Guidance on the inspections can be found in the applicable Hamilton 

Standard Division models/manuals 6/5500/F/P5190 and 24PF/61-12-01, and Hamilton 

Sundstrand Corporation models/manuals 14RF-19/P5199, 14RF-37/P5209, 14SF11/P5196, 14SF-15/P5197, 14SF-23/P5197, 14SF-17/P5198, 14SF-19/P5198, 247F1/P5202, 247F-1E/P5204, 247F-3/P5205, 568F-1/P5214, 568F-5/P5203, and 568F7/P5211.

* * * * *

Issued in Burlington, Massachusetts, on October 15, 2013.

Colleen M. D’Alessandro,

Assistant Directorate Manager, Engine & Propeller Directorate,

Aircraft Certification Service.