[Federal Register Volume 72, Number 98 (Tuesday, May 22, 2007)]
[Rules and Regulations]
[Page 28589]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: E7-9719]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2006-26112; Directorate Identifier 2006-NE-35-AD; 
Amendment 39-14837; AD 2006-24-08]
RIN 2120-AA64


Airworthiness Directives; Pratt & Whitney Canada (P&WC) PW535A 
Turbofan Engines; Correction

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

ACTION: Final rule; correction.

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SUMMARY: The FAA is correcting airworthiness directive (AD) 2006-24-08. 
That AD applies to Pratt & Whitney Canada (P&WC) PW535A turbofan 
engines. We published that AD in the Federal Register on December 4, 
2006 (71 FR 70284). The fuel manifold part number (P/N) 3025267-01 
listed in paragraph (c) is incorrect. This document corrects that P/N. 
In all other respects, the original document remains the same.

EFFECTIVE DATE: Effective May 22, 2007.

FOR FURTHER INFORMATION CONTACT: Ian Dargin, Aerospace Engineer, Engine 
Certification Office, FAA, Engine & Propeller Directorate, 12 New 
EnglandExecutive Park, Burlington, MA, 01803; telephone (781) 238-7178; 
fax (781) 238-7199.

SUPPLEMENTARY INFORMATION: On December 4, 2006 (71 FR 70284), we 
published a final rule AD, FR Doc, E6-20204, in the Federal Register. 
That AD applies to P&WC PW535A turbofan engines. We need to make the 
following correction:


Sec.  39.13  [Corrected]

    On page 70286, in the second column, in paragraph (c), in the 
fourth line, ``3025267-01'' is corrected to read ``3052627-01''.

    Issued in Burlington, Massachusetts, on May 14, 2007.
Peter A. White,
Acting Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. E7-9719 Filed 5-21-07; 8:45 am]
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