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Airworthiness Directive

AD 2012-21-06 77 FR 64695 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2012-25670
Amendment
39-17222
Published
2012-10-23
Effective
2012-11-27
Models covered
1
Last live check
2026-10-03

Printed from https://aircraftdirectives.com/ad/2012-21-06 · 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

2012-21-06

FR doc 2012-25670 · 77 FR 64695

AD 2012-21-06Published 2012-10-23Effective 2012-11-27

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 replacing incorrect gauge wires in certain electrical power wiring bundles, inspecting associated wiring bundles and components for heat damage, and taking all necessary corrective actions.

Full official abstract

We are adopting a new airworthiness directive (AD) for certain Hawker Beechcraft Corporation Model C90GTi (King Air) airplanes. This AD was prompted by reports of incorrect gauge wires used in certain wiring bundles for the cockpit electrical power for backlighting and instrument panel components. This AD requires replacing incorrect gauge wires in certain electrical power wiring bundles, inspecting associated wiring bundles and components for heat damage, and taking all necessary corrective actions. We are issuing this AD to correct the unsafe condition on these products.

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All Beechcraft King Air 90 directives

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Applies to 1 model in our index