X97-40619. Advisory Circular 20-128A, Design Considerations for Minimizing Hazards Caused by Uncontained Turbine Engine and Auxiliary Power Unit Rotor Failure

[Federal Register Volume 62, Number 118 (Thursday, June 19, 1997)]
[Corrections]
[Page 33459]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: X97-40619]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration


Advisory Circular 20-128A, Design Considerations for Minimizing 
Hazards Caused by Uncontained Turbine Engine and Auxiliary Power Unit 
Rotor Failure

Correction

    In notice document 97-15310 appearing on page 31860 in the issue of 
Wednesday, June 11, 1997, make the following correction:
    On page 31860, in the first column, in the HOW TO OBTAIN COPIES 
section, in the seventh line, the fax number ``301-5394'' should read 
``301-386-5394''.
BILLING CODE 1505-01-D