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Airworthiness Directives; Turbomeca Arriel 1 Series Turboshaft Engines; Correction

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Information about this document as published in the Federal Register.

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Federal Aviation Administration, DOT.


Final rule; correction


This document makes a correction to Airworthiness Directive (AD) 2000-20-01 applicable to Turbomeca Arriel 1 series turboshaft engines that was published in the Federal Register on October 2, 2000 (65 FR 58640). The listing of helicopters on which the affected engines might be installed in the table in the Applicability section is incorrect. This document corrects that listing. In all other respects, the original document remains the same.


October 17, 2000.

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James Rosa, Aerospace Engineer, Engine Certification Office, FAA, Engine and Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803-5299; telephone (781) 238-7152, fax (781) 238-7199 .

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A final rule airworthiness directive (FR Doc 00-24900) applicable to Turbomeca Arriel 1 series turboshaft engines, was published in the Federal Register on October 2, 2000 (65 FR 58640). The following correction is needed:

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On page 58641, in the second column, in the APPLICABILITY Section, the table in the third paragraph from the top of the column,

Eurocopter AS 356 CEurocopter AS 365 C1Eurocopter AS 350 BA.
Eurocopter AS 356 N2Eurocopter AS 350 BEurocopter AS 350 B2N.
Eurocopter AS 350 DEurocopter AS 550 U2Augusta A109K2.
Sikorsky S76ASikorsky 76ASikorsky 76A.
Sikorsky S76C”

is corrected to read “

Eurocopter SA 365 C;Eurocopter SA 365 C1;Eurocopter AS 350 BA;
Eurocopter AS 365 N2;Eurocopter AS 350 B;Eurocopter AS 350 B2;
Sikorsky S76C;Augusta A109K2”
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Issued in Burlington, MA, on September 21, 2000.

David A. Downey,

Assistant Manager, Engine and Propeller Directorate, Aircraft Certification Service.

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[FR Doc. 00-28959 Filed 11-24-00; 8:45 am]