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Airworthiness Directive

AD 2011-27-04 76 FR 81790 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2011-33344
Amendment
39-16905
Published
2011-12-29
Effective
2011-12-29
Models covered
1
Last live check
2026-09-30

Printed from https://aircraftdirectives.com/ad/2011-27-04 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.

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AD

2011-27-04

FR doc 2011-33344 · 76 FR 81790

AD 2011-27-04Published 2011-12-29Effective 2011-12-29

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires assuring the airspeed indicator(s) and/or airspeed limitations placard(s) have the correct minimum control speed (V<INF>MC</INF>) markings for the STCs installed.

1 correction to this AD FAA · 2012-03-05

Correction published 2012-03-05

Issued by
Federal Aviation Administration
Published
2012-03-05
Document
Federal Register 2012-5290 · Final rule; correction

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.

A correction restates part of an AD that was published incorrectly. It is not an additional requirement and it does not change the AD number or its effective date.

Source: Federal Register document 2012-5290, retrieved 2026-08-16

Read this correction on Federal Register (opens in a new tab)
Full official abstract

We are adopting a new airworthiness directive (AD) for all Hawker Beechcraft Corporation Models 95-C55, D55, E55, 58, and 58A airplanes equipped with a certain STC. This AD requires assuring the airspeed indicator(s) and/or airspeed limitations placard(s) have the correct minimum control speed (V<INF>MC</INF>) markings for the STCs installed. This AD was prompted by information that suggests the affected airplane models with a certain STC installed may not have the appropriate V<INF>MC</INF> markings on the airspeed indicator(s). We are issuing this AD to correct the unsafe condition on these products.

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View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab)

Applies to 1 model in our index