# Airworthiness Directives; Hawker Beechcraft Corporation Model 390 Airplanes
> **Rule** · Final rule. · Published 2008-07-30 · Effective 2008-09-03 · 73 FR 44142
## Document
- **Document number:** E8-17329
- **Category:** airworthiness
- **Manufacturer:** Hawker Beechcraft Corporation Model 390
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 73 FR 44142
- **Publication date:** 2008-07-30
- **Effective date:** 2008-09-03
- **FAA docket:** Docket No. FAA-2008-0353
## Abstract

We are adopting a new airworthiness directive (AD) for certain Hawker Beechcraft Corporation Model 390 airplanes. This AD requires you to repetitively do a post-flight check (owner/operator holding at least a private pilot certificate checking for residual heat in the angle-of- attack (AOA) probes or an appropriately-rated mechanic doing a maintenance manual operational test of the heat of the AOA probes) after every flight and replace or modify (upload software) the stall warning AOA transmitters. This AD results from reports of the potential for unannunciated loss of the heating function in the left-hand (LH) and right-hand (RH) stall warning AOA transmitters of Model 390 airplanes. We are issuing this AD to correct potentially inadequate stall warning with loss of stick pusher function.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2008/07/30/E8-17329/airworthiness-directives-hawker-beechcraft-corporation-model-390-airplanes)
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