[Federal Register Volume 59, Number 183 (Thursday, September 22, 1994)]
[Unknown Section]
[Page 0]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 94-23440]


[[Page Unknown]]

[Federal Register: September 22, 1994]


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DEPARTMENT OF TRANSPORTATION
14 CFR Part 39

[Docket No. 93-ANE-41; Amendment 39-8907; AD 94-09-18]

 

Airworthiness Directives; General Electric Company CF6 Series 
Turbofan Engines

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction

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SUMMARY: This document makes a correction to Airworthiness Directive 
(AD) 94-09-18 applicable to General Electric Company (GE) CF6-6/-45/-50 
series turbofan engines that was published in the Federal Register on 
May 5, 1994 (59 FR 23139). One phrase in the compliance section is 
incorrect and needs to be deleted; an additional description later in 
the compliance section needs to be added. This document corrects both 
errors. In all other respects, the original document remains the same.

Effective DATE: June 6, 1994.

FOR FURTHER INFORMATION CONTACT: Robert J. Ganley, telephone (617) 238-
7138.

SUPPLEMENTARY INFORMATION: A final rule airworthiness directive 
applicable to General Electric Company (GE) CF6-6/-45/-50 series 
turbofan engines, was published in the Federal Register on May 5, 1994 
(59 FR 23139). The following corrections are needed:
    On page 23141, in the left column, in paragraph (a)(5)(ii), in the 
fifth line, the phrase ``prior to accumulating 4,500 CSN,'' should be 
deleted.
    On page 23141, starting in the center column, in paragraph (b)(5), 
in the seventh and eighth line, the words ``and inner'' should be added 
after the word ``rim'' to read, ``ECI the rim and inner bolt holes''.

    Issued in Burlington, MA, on September 12, 1994.
Jay J. Pardee,
Manager, Engine and Propeller Directorate, Aircraft Certification 
Service.
[FR Doc. 94-23440 Filed 9-21-94; 8:45 am]
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