[Federal Register Volume 68, Number 132 (Thursday, July 10, 2003)]
[Corrections]
[Page 41210]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: C3-15992]



  Federal Register / Vol. 68, No. 132 / Thursday, July 10, 2003 / 
CORRECTIONS  

[[Page 41210]]



DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2003-NE-24-AD; Amendment 39-13211; AD 2003-13-11]
RIN 2120-AA64


Airworthiness Directives: Pratt & Whitney PW4074, PW4074D, 
PW4077, PW4077D, PW4090, and PW4090-3 Turbofan Engines

Correction

    In rule document 03-15992 beginning on page 38592 in the issue of 
Monday, June 30, 2003 make the following correction:


Sec.  39.13  [Corrected]

    On page 38594, in Table 1., in Sec.  39.13, in the first column, in 
the second entry, in the second line, ``incorporating a scalloped J'' 
should read ``incorporating a scalloped J flange design during 
production''.

[FR Doc. C3-15992 Filed 7-9-03; 8:45 am]
BILLING CODE 1505-01-D