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Airworthiness Directive

AD 2012-21-05 77 FR 64693 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2012-25664
Amendment
39-17221
Published
2012-10-23
Effective
2012-11-27
Models covered
1
Last live check
2026-09-30

Printed from https://aircraftdirectives.com/ad/2012-21-05 · 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

2012-21-05

FR doc 2012-25664 · 77 FR 64693

AD 2012-21-05Published 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 replacement of the incorrect gauge wiring with the correct wiring required by type design and the aircraft's circuit protection.

Full official abstract

We are adopting a new airworthiness directive (AD) for certain Hawker Beechcraft Corporation Model G58 airplanes. This AD was prompted by notification from Hawker Beechcraft Corporation that certain affected aircraft were produced with the incorrect gauge wiring installed. This AD requires replacement of the incorrect gauge wiring with the correct wiring required by type design and the aircraft's circuit protection. 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