AD Amdt-39-9347

[Federal Register Volume 61, Number 52 (Friday, March 15, 1996)]
[Rules and Regulations]
[Pages 10672-10673]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 96-5853]



=======================================================================
-----------------------------------------------------------------------

[[Page 10673]]


DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 94-ANE-41; Amendment 39-9347; AD 95-17-16]


Airworthiness Directives; General Electric Company CF6 Series 
Turbofan Engines

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

-----------------------------------------------------------------------

SUMMARY: This document makes a correction to Airworthiness Directive 
(AD) 95-17-16 applicable to General Electric Company (GE) CF6-80A 
series turbofan engines that was published in the Federal Register on 
August 20, 1995 (60 FR 46760). A compressor rear frame (CRF) part 
number (P/N) in the compliance section is incorrect. This document 
corrects that P/N. In all other respects, the original document remains 
the same.

DATES: Effective March 15, 1996.

SUPPLEMENTARY INFORMATION: A final rule airworthiness directive 
applicable to General Electric Company (GE) CF6-80A series turbofan 
engines, was published in the Federal Register on August 20, 1995 (60 
FR 46760). The following correction is needed:
    On page 46761, in the second column, in the Compliance Section, in 
paragraph (a), ``7283M77G15'' should read ``9283M77G15.'' Issued in 
Burlington, MA, on February 14, 1996.
Jay J. Pardee,
Manager, Engine and Propeller Directorate, Aircraft Certification 
Service.
[FR Doc. 96-5853 Filed 3-14-96; 8:45 am]
BILLING CODE 4910-13-U