[Federal Register Volume 68, Number 139 (Monday, July 21, 2003)]
[Corrections]
[Page 43260]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: C3-13650]



  Federal Register / Vol. 68, No. 139 / Monday, July 21, 2003 / 
CORRECTIONS  

[[Page 43260]]



DEPARTMENT OF TRANSPORTATION

Federal Aviation Adminstration

14 CFR Part 39

[Docket No. 2003-CE-23-AD; Amendment 39-13173; AD 2003-11-14]
RIN 2120-AA64


Airworthiness Directives; The New Piper Aircraft, Inc. Models PA-
34-200T, PA-34-220T, PA-44-180, and PA-44-180T Airplanes

Correction

    In rule document 03-13650 beginning on page 33356 in the issue of 
Wednesday, June 4, 2003, make the following correction:


Sec.  39.13  [Corrected]

    On page 33358, in Sec.  39.13(d), in the first column, in the 
table, under the column heading ``Actions'', correct (1) to read as 
follows:
    ``(1) Visually inspect any installed aircraft heater fuel pump 
(model 91E92-1 or model 91E93-1) for leakage.''.

[FR Doc. C3-13650 Filed 7-18-03; 8:45 am]
BILLING CODE 1505-01-D