Airworthiness Directive

AD 2008-13-17 73 FR 37783 Active

Federal Aviation Administration · 14 CFR part 39

FR document
E8-14090
Amendment
39-15580
Published
2008-07-02
Effective
2008-08-06
Models covered
2
Last live check
2026-10-02
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.
AD

2008-13-17

FR doc E8-14090 · 73 FR 37783

AD 2008-13-17Published 2008-07-02Effective 2008-08-06

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 you to replace certain circuit breaker toggle switches with improved design circuit breaker toggle switches.

Full official abstract

The FAA adopts a new airworthiness directive (AD) for certain Hawker Beechcraft Corporation F33 series and Models G33, V35B, A36, A36TC, B36TC, 95-B55, D55, E55, A56TC, 58, 58P, 58TC, G58, and 77 airplanes. This AD requires you to replace certain circuit breaker toggle switches with improved design circuit breaker toggle switches. This AD results from reports of certain circuit breaker toggle switches used in various electrical systems throughout the affected airplanes overheating. We are issuing this AD to prevent failure of the circuit breaker toggle switch, which could result in smoke in the cockpit and the inability to turn off the switch.

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Applies to 2 models in our index