[Federal Register Volume 61, Number 110 (Thursday, June 6, 1996)]
[Rules and Regulations]
[Page 28736]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 96-13888]



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DEPARTMENT OF TRANSPORTATION
14 CFR Part 39

[Docket No. 92-ANE-08; Amendment 39-8781; AD 93-25-17]


Airworthiness Directives; General Electric CT7 Series Turboprop 
and Turboshaft Engines

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

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SUMMARY: This document makes a correction to Airworthiness Directive 
(AD) 93-25-17 applicable to General Electric (GE) CT7 series turboprop 
and turboshaft engines that was published in the Federal Register on 
January 3, 1994 (59 FR 3). The docket number in the header to the 
applicability section is incorrect. This document corrects the docket 
number. In all other respects, the original document remains the same.

EFFECTIVE DATE: June 6, 1996.

FOR FURTHER INFORMATION CONTACT: Dave Keenan, Aerospace Engineer, 
Engine Certification Office, FAA, Engine and Propeller Directorate, 12 
New England Executive Park, Burlington, MA 01803-5299; telephone (617) 
238-7139, fax (617) 238-7199.

SUPPLEMENTARY INFORMATION: A final rule airworthiness directive 
applicable to General Electric (GE) CT7 series turboprop and turboshaft 
engines, was published in the Federal Register on January 3, 1994 (59 
FR 3). The following correction is needed:


Sec. 39.13  [Corrected]

    On page 4, in the first column, in the heading above the 
Applicability Section of AD 93-25-17, in the second line, ``Docket No. 
93-ANE-08'' is corrected to read ``Docket No. 92-ANE-08''.

    Issued in Burlington, Massachusetts, on May 16, 1996.
Jay J. Pardee,
Manager, Engine and Propeller Directorate, Aircraft Certification 
Service.
[FR Doc. 96-13888 Filed 6-5-96; 8:45 am]
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