Back to publication catalog

Published 2012-03-05 · Federal Register document 2012-5290

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

Publication 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.

Why this record is shown

Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:39.502075+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2012-08bffa249ae9a205
Source row
results[64]
Raw source SHA-256
08bffa249ae9a2053bbfc0d74663d089914e83fb91f9bc4c8409ea28239f6875

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition
2011-27-04
Effective date printed in this edition
Unknown

This correction is a separate source edition; it is not counted as a new adopted rule.

No adopted-clause structure was recorded for this source edition. Read the complete text; no applicability conclusion has been inferred.

No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.

Find all recorded historical references to AD 2011-27-04 · 0 printed reference observations in this pinned collection.

These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.

Why these observations are shown

They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.

Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 24f4f3dafcf97b231b0feb67a687ad17d55a92a31cbf8a60f7b32eb4e657f520. Source manifest: c78c1c054cf1ed7cda9b3623866ed14b36897a418943be15b4c46bc9aafb2f29.

Official source · 2012-03-05

Publication text

This is the complete recorded text of this dated publication.

Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.

Read the complete official publication text
[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]


-----------------------------------------------------------------------

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.

-----------------------------------------------------------------------

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: [email protected].

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


Why this text is shown

The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T03:04:14.904312+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

Open the captured official edition

Source SHA-256
31cea7c8510a480e054cccc523864d6cbaa30335b07f89eb537b8e464922b9e8
Text SHA-256
24f4f3dafcf97b231b0feb67a687ad17d55a92a31cbf8a60f7b32eb4e657f520

Return to the full metadata catalog · Search complete publication text · Explore retained publication text and evidence

Coverage and limits

These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.

The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.