[Docket No. 2003-CE-28-AD; Amendment 39-13382; AD 2003-24-13]

ACTION: Final rule; correction.

SUMMARY: This document makes a correction to Airworthiness Directive (AD) 2003-24-13, which was published in the Federal Register on December 4, 2003 (68 FR 67789), and applies to certain Cessna Aircraft Company (Cessna) Models 172R, 172S, 182S, 182T, T182T, 206H, and T206H airplanes that are equipped with a Honeywell KAP 140 autopilot computer system installed on the center instrument control panel near the throttle. We inadvertently duplicated affected airplane serial numbers and included a serial number that should not be affected by this AD in the applicability section. This action corrects the applicability section of AD 2003-24-13, Amendment 39-13382.

EFFECTIVE DATE: The effective date of this AD remains January 20, 2004.

Correction of Publication
    Accordingly, the publication of December 4, 2003 (68 FR 67789), of Amendment 39-13382; AD 2003-24-13, which was the subject of FR Doc. 03-30075, is corrected as follows:

Sec. 39.13  [Corrected]

    On page 67791, in section 39.13 [Amended], 2., replace paragraph (c) of the AD with the following text:

What Airplanes Are Affected by This AD?
   (c)    This AD affects the following airplane models and serial numbers that are:
    (1)    equipped with a KAP 140 autopilot computer system, part number (P/N) 065-00176-2602, P/N 065-00176-5402, or P/N 065-00176-7702; and
    (2)    certificated in any category;

------------------------------------------------------------------------
               Model                             Serial No.
------------------------------------------------------------------------
172R..............................  17280001 through 17281073, 17281075
                                     through 17281127, and 17281130
172S..............................  172S8001 through 172S9195, 172S9197,
                                     172S9198, and 172S9200 through
                                     172S9203
182S..............................  18280001 through 18280944
182T..............................  18280945 through 18281064, 18281067
                                     through 18281145,18281147 through
                                     18281163, 18281165 through
                                     18281167, and 18281172
T182T.............................  T18208001 through T18208109, and
                                     T18208111 throughT18208177
206H..............................  20608001 through 20608183, 20608185,
                                     20608187, and 20608188
T206H.............................  T20608001 through T20608039,
                                     T20608041 through T20608367,
                                     T20608369 through T20608379,
                                     T20608381, T20608382, and
                                     T20608385''
------------------------------------------------------------------------

    Action is taken herein to correct this reference in AD 2003-24-13 and to add this AD correction to Sec. 39.13 of the Federal Aviation Regulations (14 CFR 39.13).