[Federal Register: September 18, 2003 (Volume 68, Number 181)]
[Rules and Regulations]               
[Page 54653]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr18se03-2]                         


[[Page 54653]]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 94-ANE-08-AD; Amendment 39-13256; AD 2003-16-03]
RIN 2120-AA64

 
Airworthiness Directives; Turbomeca Arriel 1 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) 2003-16-03 applicable to Turbomeca Arriel 1 Series turboshaft 
engines that was published in the Federal Register on August 8, 2003 
(68 FR 47208). Turbomeca Arriel turboshaft engine 1 C1 was omitted from 
the Applicability. This document corrects that omission. In all other 
respects, the original document remains the same.

EFFECTIVE DATE: Effective September 18, 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. 03-19836, 
applicable to Turbomeca Arriel 1 Series turboshaft engines, was 
published in the Federal Register on August 8, 2003 (68 FR 47208). The 
following correction is needed:

PART 39--AIRWORTHINESS DIRECTIVES


Sec.  39.13  [Corrected]

0
On page 47209, in the third column, in the Applicability Section, the 
first sentence ``This airworthiness directive (AD) applies to Turbomeca 
turboshaft engine models Arriel 1 A, 1 A1, 1 A2, 1 B, 1 C, 1 C2, 1 D, 1 
D1, 1 E2, 1 K, 1 K1, 1 S, and 1 S1 that have not incorporated 
modification TU 202'' is corrected to read, ``This airworthiness 
directive (AD) applies to Turbomeca turboshaft engine models Arriel 1 
A, 1 A1, 1 A2, 1 B, 1 C, 1 C1, 1 C2, 1 D, 1 D1, 1 E2, 1 K, 1 K1, 1 S, 
and 1 S1 that have not incorporated modification TU 202''.

    Issued in Burlington, MA, on September 11, 2003.
Francis A. Favara,
Assistant Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. 03-23816 Filed 9-17-03; 8:45 am]

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