[Federal Register Volume 68, Number 109 (Friday, June 6, 2003)]
[Rules and Regulations]
[Page 33854]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 03-14275]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 99-NE-12-AD; Amendment 39-13168; AD 2003-11-09]
RIN 2120-AA64


Airworthiness Directives; Turbomeca Turmo IV A and IV C Series 
Turboshaft Engines; Correction

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

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SUMMARY: This document makes a correction to Airworthiness Directive 
(AD) 2003-11-09 applicable to Turbomeca Turmo IV A and IV C series 
turboshaft engines that was published in the Federal Register on May 
29, 2003 (68 FR 31970). The engine model in the regulatory section, 
under applicability, is incorrect. This document corrects that model. 
In all other respects, the original document remains the same.

EFFECTIVE DATE: July 3, 2003.

FOR FURTHER INFORMATION CONTACT: Antonio Cancelliere, Aerospace 
Engineer, Engine Certification Office, FAA, Engine and Propeller 
Directorate, 12 New England Executive Park, Burlington, MA 01803-5299; 
telephone (781) 238-7751; fax (781) 238-7199.

SUPPLEMENTARY INFORMATION: A final rule AD, FR Doc. 03-13115 applicable 
to Turbomeca Turmo IV A and IV C series turboshaft engines, was 
published in the Federal Register on May 29, 2003 (68 FR 31970). The 
following correction is needed:


Sec.  39.13  [Corrected]

0
On page 31970, in the third column, in the regulatory section, under 
applicability, in the first paragraph, in the fifth line, ``FA 330-
PUMA'' is corrected to read ``SA 330-PUMA''.

    Issued in Burlington, MA, on June 2, 2003.
Jay J. Pardee,
Manager, Engine and Propeller Directorate, Aircraft Certification 
Service.
[FR Doc. 03-14275 Filed 6-5-03; 8:45 am]
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