Airworthiness directives: General Electric Co.; correction,

FR, October 16, 2000Rules › Federal Aviation Administration

Linked as:

Text




Federal Register: October 16, 2000 (Volume 65, Number 200)CORRECTIONSPage 61216From the Federal Register Online via GPO Access [wais.access.gpo.gov]

DOCID:fr16oc00-146

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

Docket No. 2000-NE-38-AD; Amendment 39-11913; AD 2000-20-02Airworthiness Directives; General Electric Company CF6-50 Series Turbofan Engines

Correction

In rule document 00-24901, beginning on page 58645, in the issue of Monday, October 2, 2000, make the following correction:

Sec. 39.13 [Corrected]

1.On page 58646, in the second column, under the heading Initial Inspection of Stage 2 LPT Nozzle Lock Assemblies, in paragraph (a), the fourth line, ``information'' should read ``Information''.

2. On page 58646, in the third column, under the heading Repetitive Inspection of Stage 2 LPT Nozzle Lock Assemblies, in paragraph (c), the fourth line, ``information'' should read `` Information''.

3. On page 58646, in the third column, in paragraph (d), the second line, ``place'' should read ``replace''.

FR Doc. C0-24901Filed10-13-00; 8:45 amBILLING CODE 1505-01-D

Sponsored links




ver las páginas en versión mobile | web

ver las páginas en versión mobile | web

© Copyright 2012, vLex. All Rights Reserved.

Contents in vLex United States

Explore vLex

For Professionals

For Partners

Company