Document ID: chunk:federal_register_of_legislation:F2006B03932:body:0
Version: federal_register_of_legislation:F2006B03932
Segment Type: other
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Character Range: 0–938

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Beechcraft 400 Series Aeroplanes

 AD/BEECH 400/5 Main Circuit Breaker Panel 1/94

DM

            Applicability: Model 400A aircraft with serials numbers RK-45 and RK-49 through RK-77 inclusive.

            Requirement: Action in accordance with Beechcraft Mandatory Service Bulletin 2520 dated August 1993 and Beechcraft Service Communique 400-101 dated July 1993.

            Note: FAA AD 93-20-01 Amdt 39-8708 refers.

 Compliance: Within 25 hours' time in service from 17 November 1993.

            Background:  Beechcraft have advised of anomalies in the main circuit breaker panel wiring and that there is a possibility for an electrical short to occur. Compliance with this Directive will decrease the probability of an electrical short causing fire and smoke in the cockpit.