[Federal Register Volume 69, Number 54 (Friday, March 19, 2004)]
[Corrections]
[Page 13127]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: C4-4372]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2000-CE-09-AD; Amendment 39-13496; AD 2001-13-18 R1]
RIN 2120-AA64
Airworthiness Directives; Raytheon Aircraft Corporation Beech
Models 45 (YT-34), A45 (T-34A, B-45), and D45 (T-34B) Airplanes
Correction
In rule document 04-4372 beginning on page 9526 in the issue of
Monday, March 1, 2004, make the following correction:
Sec. 39.13 [Corrected]
On page 9528, in 39.13, the table is corrected in part to read as
follows:
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Action When In accordance with
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* * * * *.............. * *
(2) Modify each airspeed All actions required Not Applicable.
indicator glass by within 10 hours
accomplishing the time-in-service
following: (TIS) after July 9,
1999 (the effective
date of AD 99-12-
02), unless already
accomplished.
(i) Place a red radial line
on each indicator glass at
175 miles per hour (mph)
(152 knots).
(ii) Place a white slippage
index mark between each
airspeed indicator glass
and case to visually verify
that the glass has not
rotated.
(3) Mark the outside surface All actions required Not Applicable.
of the ``g'' meters with within 10 hours
lines of approximately \1/ time-in-service
16\-inch by \3/16\-inch, as (TIS) after July 9,
follows: 1999 (the effective
date of AD 99-12-
02), unless already
accomplished.
* * * * *.............. * *
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[FR Doc. C4-4372 Filed 3-18-04; 8:45 am]
BILLING CODE 1505-01-D