Airworthiness directives: Raytheon Correction,

[Federal Register: March 19, 2004 (Volume 69, Number 54)]

[CORRECTIONS]

[Page 13127]

From the Federal Register Online via GPO Access [wais.access.gpo.gov]

[DOCID:fr19mr04-107]

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:

Action

When

In accordance with

* *

* * *.............. * * (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. * *

* * *.............. * *

[FR Doc. C4-4372 Filed 3-18-04; 8:45 am]

BILLING CODE 1505-01-D