Legal Status
Legal Status
Correction
Airworthiness Directives; Boeing Model 727 Airplanes
A Correction by the Federal Aviation Administration on
Document Details
Information about this document as published in the Federal Register.
- Printed version:
- Publication Date:
- 03/17/2005
- Agencies:
- Federal Aviation Administration
- Document Type:
- Correction
- Document Citation:
- 70 FR 13074
- Page:
- 13074 (1 page)
- CFR:
- 14 CFR 39
- Agency/Docket Numbers:
- Docket No. FAA-2004-19530
- Directorate Identifier 2002-NM-274-AD
- Amendment 39-14008
- AD 2005-05-19
- RIN:
- 2120-AA64
- Document Number:
- C5-4826
Document Details
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Correction
In rule document 05-4826 beginning on page 12120 in the issue of Friday, March 11, 2005, make the following corrections:
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