[Federal Register Volume 77, Number 43 (Monday, March 5, 2012)]
[Rules and Regulations]
[Page 12991]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2012-5290]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2011-1420; Directorate Identifier 2011-CE-035-AD; 
Amendment 39-16905; AD 2011-27-04]
RIN 2120-AA64


Airworthiness Directives; Hawker Beechcraft Corporation Airplanes 
Equipped With a Certain Supplemental Type Certificate (STC)

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; correction.

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SUMMARY: The FAA is correcting an airworthiness directive (AD) that 
published in the Federal Register. That AD applies to all Hawker 
Beechcraft Corporation Models 95-C55, D55, E55, 58, and 58A airplanes 
equipped with a certain STC. The description of the affected STCs in 
the first sentence of the SUPPLEMENTARY INFORMATION, Discussion 
section, is incorrect. This document corrects that error. In all other 
respects, the original document remains the same.

DATES: This final rule is effective March 5, 2012. The effective date 
for AD 2011-27-04 (76 FR 81790, December 29, 2011) remains December 29, 
2011.

ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov; or in person at the Docket Management Facility 
between 9 a.m. and 5 p.m., Monday through Friday, except Federal 
holidays. The AD docket contains this AD, the regulatory evaluation, 
any comments received, and other information. The address for the 
Docket Office (phone: 800-647-5527) is Document Management Facility, 
U.S. Department of Transportation, Docket Operations, M-30, West 
Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE., 
Washington, DC 20590.

FOR FURTHER INFORMATION CONTACT: Eric B. Potter, Aerospace Engineer, 
Atlanta Aircraft Certification Office, FAA, 1701 Columbia Avenue, 
College Park, Georgia 30337; phone: (404) 474-5583; fax: (404) 474-
5606; email: <a href="/cdn-cgi/l/email-protection#6d081f040e431d021919081f2d0b0c0c430a021b"><span class="__cf_email__" data-cfemail="d5b0a7bcb6fba5baa1a1b0a795b3b4b4fbb2baa3">[email protected]</span></a>.

SUPPLEMENTARY INFORMATION: Airworthiness Directive 2011-27-04, 
amendment 39-16905 (76 FR 81790, December 29, 2011), currently requires 
assuring the airspeed indicator(s) and/or airspeed limitations 
placard(s) have the correct minimum control speed (V<INF>MC</INF>) 
markings for all Hawker Beechcraft Corporation Models 95-C55, D55, E55, 
58, and 58A airplanes equipped with a certain STC.
    As published, the description of the affected STCs in the first 
sentence of the SUPPLEMENTARY INFORMATION, Discussion section, is 
incorrect.
    No other part of the preamble or regulatory information has been 
changed; therefore, only the changed portion of the preamble to the 
final rule is being published in the Federal Register.
    The effective date of this AD remains December 29, 2011.

Correction of Non-Regulatory Text

    In the Federal Register of December 29, 2011, AD 2011-27-04; 
Amendment 39-16905 is corrected as follows:
    On page 81790, in the third column, on line 2 under the heading 
SUPPLEMENTARY INFORMATION, Discussion, correct ``, we found that STC 
SA1762SO (installation of vortex generators) and STC SA4016NM (Foxstar 
Baron modification of winglets and different engines and propellers) 
were installed.'' to read ``, we found that STC SA1762SO (Foxstar Baron 
modification of winglets and different engines and propellers) and STC 
SA4016NM (installation of vortex generators) were installed.''

    Issued in Kansas City, Missouri, on February 23, 2012.
John Colomy,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2012-5290 Filed 3-2-12; 8:45 am]
BILLING CODE 4910-13-P


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