C0-24901. Airworthiness Directives; General Electric Company CF6-50 Series Turbofan Engines
[Federal Register Volume 65, Number 200 (Monday, October 16, 2000)]
[Corrections]
[Page 61216]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: C0-24901]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2000-NE-38-AD; Amendment 39-11913; AD 2000-20-02]
Airworthiness 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. C0-24901 Filed 10-13-00; 8:45 am]
BILLING CODE 1505-01-D
Document Information
- Published:
- 10/16/2000
- Department:
- Federal Aviation Administration
- Entry Type:
- Correction
- Document Number:
- C0-24901
- Pages:
- 61216-61216 (1 pages)
- Docket Numbers:
- Docket No. 2000-NE-38-AD, Amendment 39-11913, AD 2000-20-02
- PDF File:
-
c0-24901.pdf
- CFR: (1)
- 14 CFR 39.13