Published 2006-05-19 · Federal Register document 06-4679
Airworthiness Directives; Hamilton Sundstrand Model 14RF-9 Propellers; Correction
Publication 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.
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Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:20.745856+00:00. The title, summary and date are source facts.
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- 8d787f8b35bc80165a417cea66de09cd32a1700face13759db364c607e405963
Correction notice · separate source edition
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- 2006-10-07
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Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: a615f53dad2599491a3357f70584c86b8d1de42a94fa15762c60d8045721fa8c. Source manifest: 95a8b537e3d217dccbf45a5b636e722c9b479b88a34f2c95ceb48a87f3162eac.
Official source · 2006-05-19
Publication text
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[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
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