[Federal Register Volume 71, Number 97 (Friday, May 19, 2006)]
[Rules and Regulations]
[Page 29072]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 06-4679]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2006-24517; Directorate Identifier 2006-NE-18-AD; 
Amendment 39-14591; AD 2006-10-07]
RIN 2120-AA64


Airworthiness Directives; Hamilton Sundstrand Model 14RF-9 
Propellers; Correction

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

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SUMMARY: This document makes a correction to Airworthiness Directive 
(AD) 2006-10-07. That AD applies to Hamilton Sundstrand Model 14RF-9 
propellers. We published AD 2006-10-07 in the Federal Register on May 
12, 2006 (71 FR 27600). An incorrect phrase was used in the compliance 
section, which impacts the intent of the compliance. This document 
corrects that phrase. In all other respects, the original document 
remains the same.

DATES: Effective Date: Effective May 19, 2006.

FOR FURTHER INFORMATION CONTACT: Frank Walsh, Aerospace Engineer, 
Boston Aircraft Certification Office, FAA, Engine & Propeller 
Directorate, 12 New England Executive Park, Burlington, MA 01803; 
telephone (781) 238-7158; fax (781) 238-7170.

SUPPLEMENTARY INFORMATION: A final rule AD, FR Doc. 06-4390, that 
applies to Hamilton Sundstrand Model 14RF-9 propellers was published in 
the Federal Register on May 12, 2006 (71 FR 27600). The following 
correction is needed:


Sec.  39.13  [Corrected]

0
On page 27601, in the third column, in compliance paragraph (i)(1), in 
the second line, ``after accumulating an additional 500 flight cycles'' 
is corrected to read ``within an additional 500 flight cycles''.

    Issued in Burlington, MA, on May 15, 2006.
Robert J. Ganley,
Acting Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. 06-4679 Filed 5-18-06; 8:45 am]
BILLING CODE 4910-13-P