Document ID: chunk:federal_register_of_legislation:F2006B09472:body:0
Version: federal_register_of_legislation:F2006B09472
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Embraer EMB-110 (Bandeirante) Series Aeroplanes

 AD/EMB-110/30
 Amdt 1

 Flap Control and Protection Unit - Modification 4/85

 Applicability: All models equipped with multiposition flap control switch. Document: Embraer SB 110-27-073 R1.
            Note: Brazilian AD 84-01-01 refers.

            Compliance: Part I: Within 100 hours time in service after 31 March 1984. Part II: Within 250 hours time in service after 30 April 1985.
             Background: a. Inadvertent flap extension due to short circuit in flap system control and protection unit have been reported.

             b. Amendment 1 includes a further modification to prevent tripping the Flap control circuit breaker when the fire extinguishing system is actuated.