Published 2003-09-18 · Federal Register document 03-23816
Airworthiness Directives; Turbomeca Arriel 1 Series Turboshaft Engines; Correction
Publication 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.
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Correction notice · separate source edition
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- AD identifier printed in this edition
- 2003-16-03
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Official source · 2003-09-18
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[Federal Register Volume 68, Number 181 (Thursday, September 18, 2003)]
[Rules and Regulations]
[Page 54653]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 03-23816]
[[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]
BILLING CODE 4910-13-P
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