[Federal Register Volume 67, Number 23 (Monday, February 4, 2002)]
[Corrections]
[Page 5148]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: C1-30951]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 99-NE-17-AD; Amendment 39-12557; AD 2001-25-04]
RIN 2120-AA64


Airworthiness Directives; Honeywell International Inc. Models 
LTS101-600A-2 and LTS101-600A-3 Turboshaft Engines; and LTP101-600A-1A 
and LTP101-700A-1A Turboprop Engines

Correction

    In rule document C1-30951 beginning on page 65426 in the issue of 
Wednesday, December 19, 2001, make the following correction:


Sec. 39.13  [Corrected]

    On page 65427, in Sec. 39.13, in the third column, under the 
heading Applicability, in the fourth line ``LTS101-6000A-2 '' should 
read ``LTS101-600A-2 ''.

[FR Doc. C1-30951 Filed 2-1-02; 8:45 am]
BILLING CODE 1505-01-D