# Proposed AD FAA-2006-24084: Raytheon Model Hawker 800XP Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2006-11-07
- Products: Raytheon
- Product type: Aircraft
- Action: Notice of proposed rulemaking (NPRM).
- Published: March 7, 2006, 71 FR 11343
- Comments due: April 21, 2006
- Became: [AD 2006-11-07](https://openairdocs.org/ad/2006-11-07)
- Docket: FAA-2006-24084 (https://www.regulations.gov/docket/FAA-2006-24084, where comments are filed)
- Project: 2006-NM-017-AD
- FR document: E6-3219
- Official PDF: https://openairdocs.org/files/sha256/df/4e/df4e719aae5f63a5d044ca33bef042e4496193ebaeb529a4cbf258c4eadcb0da (from https://www.govinfo.gov/content/pkg/FR-2006-03-07/pdf/E6-3219.pdf)
- Federal Register: https://www.federalregister.gov/documents/2006/03/07/E6-3219/airworthiness-directives-raytheon-model-hawker-800xp-airplanes
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/5B50A10A20632AFD8625712A005E4CCA.0001
- Page: https://openairdocs.org/proposed/FAA-2006-24084

## Summary

The FAA proposes to adopt a new airworthiness directive (AD) for certain Raytheon Model Hawker 800XP airplanes. This proposed AD would require inspecting certain bus bars in the DA-A panel to ensure that the bus bars match the panel configuration and clearance is adequate between the bus bars and adjacent components, and performing corrective action if necessary. This proposed AD results from two reports of inadequate clearance between the bus bars in the DA-A panel. We are proposing this AD to prevent insufficient electrical isolation for the electrical bus configuration and inability of the flightcrew to isolate the bus bars in an emergency situation involving a dual generator failure, which could result in extra loads on the main ship batteries and consequent loss of power to the main essential bus.

## Notices in this docket

- Mar 7, 2006: Notice of proposed rulemaking (NPRM). (first notice), FR document E6-3219, comments due Apr 21, 2006 (https://www.federalregister.gov/documents/2006/03/07/E6-3219/airworthiness-directives-raytheon-model-hawker-800xp-airplanes)

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