[Federal Register: March 17, 2005 (Volume 70, Number 51)]
[CORRECTIONS]               
[Page 13074]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr17mr05-113]                         



[[Page 13074]]



DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2004-19530; Directorate Identifier 2002-NM-274-AD; 
Amendment 39-14008; AD 2005-05-19]
RIN 2120-AA64

 
Airworthiness Directives; Boeing Model 727 Airplanes

Correction

    In rule document 05-4826 beginning on page 12120 in the issue of 
Friday, March 11, 2005, make the following corrections:


Sec.  39.13  [Corrected]

    1. On page 12122 in 39.13(h), in the table, in the fifth column, in 
the first entry, in the fourth line, ``of the upper chord the'' should 
read ``of the upper chord of the''.
    2. On the same page, in the same section, in the same table, in the 
same column, in the second entry, in the third line, ``chord'' should 
read ``chords''.
    3. On the same page, in the same section, in the same table, in the 
same column, in the third entry, in the third line, ``of the rear spar 
from'' should read ``of the front spar and the lower chord of the rear 
spar from ''.
    4. On the same page, in the same section, in the same table, in the 
same column, in the fourth entry, in the third line, ``rear spar WBL'' 
should read ``rear spar from WBL''.
    5. On page 12123, in the same section, in the same table, in the 
same column, the first entry is corrected to read as follows:

An HFEC inspection of the upper chord of the rear spar from WBL 70.5 
to the wing tip for cracks, corrosion, minor surface defects, and 
existing stop-drilled repairs of cracking (initial inspection only), 
in accordance with paragraph 3.B., Work Instructions, Part 9, of the 
Accomplishment Instructions of the service bulletin.

[FR Doc. C5-4826 Filed 3-16-05; 8:45 am]

BILLING CODE 1505-01-D