[Federal Register: June 6, 2003 (Volume 68, Number 109)]
[Rules and Regulations]
[Page 33854]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr06jn03-7]
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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]
BILLING CODE 4910-13-P