Airworthiness Directives; Hawker Beechcraft Corporation (Type Certificate No. A00010WI Previously Held by Raytheon Aircraft Company) Model 390 Airplanes
airworthiness · Rule · Final rule. · Published 2010-05-17 · Effective 2010-06-21 · 75 FR 27422
Document
Document number
2010-10717
Federal Register citation
75 FR 27422
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Hawker Beechcraft Corporation (Type Certificate No. A00010WI Previously Held by Raytheon
Publication date
2010-05-17
Effective date
2010-06-21
FAA docket
Docket No. FAA-2010-0158
Abstract
We are adopting a new airworthiness directive (AD) for certain Hawker Beechcraft Corporation Model 390 airplanes. This AD requires you to inspect the essential bus lightning strike protection for proper installation of metal oxide varistor (MOV) and spark gap wiring. This AD also requires you to rework the wiring as necessary to achieve the required lightning strike/surge protection. This AD results from a report that the wires to the MOV and spark gap were swapped. We are issuing this AD to detect and correct improper installation of the MOV and spark gap wiring, which could result in overload of the MOV in a lightning strike and allow electrical energy to continue to the essential bus and disable equipment that receives power from the essential bus. The disabled equipment could include the autopilot, anti-skid system, hydraulic indicator, spoiler system, pilot primary flight display, audio panel, or the <greek-i>1 air data computer. This failure could lead to a significant increase in pilot workload during adverse operating conditions.