[Federal Register Volume 67, Number 36 (Friday, February 22, 2002)]
[Corrections]
[Page 8337]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: C2-2946]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2001-CE-38-AD; Amendment 39-12638; AD 2002-02-10]
RIN 2120-AA64


Airworthiness Directives; Pilatus Britten-Norman Limited BN-2, 
BN-2A, BN-2B, and BN-2T Series Airplanes

Correction

    In rule document 02-2946 beginning on page 6388 in the issue of 
Tuesday, February 12, 2002 make the following correction:


Sec. 39.13  [Corrected]

    On page 6389, in Sec.  39.13(d), in the table, the second column, 
under the heading ``Compliance'', the last sentence ``Replace 
thereafter prior to further bulletin), flight after any loose rivet, 
structural accomplish the damage, or crack is found.'' should read 
``Replace thereafter prior to further flight after any loose rivet, 
structural damage, or crack is found.''

[FR Doc. C2-2946 Filed 2-21-02; 8:45 am]
BILLING CODE 1505-01-D