Document ID: chunk:federal_register_of_legislation:F2006B06038:body:0:p2
Version: federal_register_of_legislation:F2006B06038
Segment Type: other
Provision Reference: 
Character Range: 3122–4218

and contacting the module's metal case. This causes the electrical short circuit and electrical arcing.

            The following electrical system components are potentially affected by this condition: engine start; strobe light; left/right taxi light; liquid crystal display (LCD) dimming; dual flasher (recognition light); left/right pitot heat; avionics dimming (Bezel buttons for radios); prop heat; left/right fuel pump; position light landing light; instrument panel light dimming; ice light; vent defog (vent blower); hi/low blower; stall heat and dimmer switch lighting (overhead switch panel switches).

            If not corrected, short circuit failure and electrical arcing of the electronic control modules could result in loss of the electrical systems components or burning of wiring insulation and cause smoke in the cockpit. This condition could lead to the inability to properly control the aeroplane.

 James Coyne
 Delegate of the Civil Aviation Safety Authority 1 April 2004

 The above AD is notified in the Commonwealth of Australia Gazette on 21 April 2004.