Published 2013-10-25 · Federal Register document 2013-25108
Airworthiness Directives; Hamilton Standard Division and Hamilton Sundstrand Corporation Propellers
Publication 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.
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Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:42.577882+00:00. The title, summary and date are source facts.
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Correction notice · separate source edition
Recorded publication clauses
- AD identifier printed in this edition
- 2013-16-10
- Effective date printed in this edition
- Unknown
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Official source · 2013-10-25
Publication text
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Read the complete official publication text
[Federal Register Volume 78, Number 207 (Friday, October 25, 2013)]
[Rules and Regulations]
[Pages 63852-63853]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2013-25108]
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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.
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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 October 25, 2013. 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, 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: [email protected].
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.
[[Page 63853]]
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
Sec. 39.13 [Corrected]
0
In the Federal Register of August 15, 2013, on page 49662, in the 1st
column, paragraph (g) of AD 2013-16-10 is corrected to read as follows:
* * * * *
(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, 14SF-15, 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, 14SF-11/P5196, 14SF-15/P5197,
14SF-23/P5197, 14SF-17/P5198, 14SF-19/P5198, 247F-1/P5202, 247F-1E/
P5204, 247F-3/P5205, 568F-1/P5214, 568F-5/P5203, and 568F-7/P5211.
* * * * *
Issued in Burlington, Massachusetts, on October 15, 2013.
Colleen M. D'Alessandro,
Assistant Directorate Manager, Engine & Propeller Directorate, Aircraft
Certification Service.
[FR Doc. 2013-25108 Filed 10-24-13; 8:45 am]
BILLING CODE 4910-13-P
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