[Federal Register Volume 63, Number 181 (Friday, September 18, 1998)]
[Rules and Regulations]
[Page 49819]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 98-25005]


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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 97-ANE-29-AD; Amendment 39-10286; AD 98-02-04]
RIN 2120-AA64


Airworthiness Directives; CFM International CFM56-5B/2P Series 
Turbofan Engines

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

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

SUMMARY: This document makes a correction to Airworthiness Directive 
(AD) 98-02-04 applicable to CFM International (CFMI) CFM56-5B/2P series 
turbofan engines that was published in the Federal Register on January 
21, 1998 (63 FR 3031). The low pressure turbine (LPT) case 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.

EFFECTIVE DATE: September 18, 1998.

FOR FURTHER INFORMATION CONTACT: Robert J. Ganley, Aerospace Engineer, 
Engine Certification Office, FAA, Engine and Propeller Directorate, 12 
New England Executive Park, Burlington, MA 01803-5299; telephone (781) 
238-7138; fax (781) 238-7199.

SUPPLEMENTARY INFORMATION: A final rule airworthiness directive 
applicable to CFM International (CFMI) CFM56-5B/2P series turbofan 
engines, was published in the Federal Register on January 21, 1998 (63 
FR 3031). The following correction is needed:


Sec. 39.13  [Corrected]

    On page 3031, in the third column, in the Compliance Section, in 
the Applicability paragraph, in the fifth line, ``338-117-004-0'' is 
corrected to read ``338-117-404-0''.
    On page 3031, in the third column, in the Compliance Section, in 
paragraph (a), in the second line, ``338-117-004-0'' is corrected to 
read ``338-117-404-0''.
    On page 3031, in the third column, in the Compliance Section, in 
paragraph (d), in the third line, ``338-117-004-0'' is corrected to 
read ``338-117-404-0''.

    Issued in Burlington, Massachusetts, on September 11, 1998.
David A. Downey,
Assistant Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. 98-25005 Filed 9-17-98; 8:45 am]
BILLING CODE 4910-13-U