Document ID: chunk:federal_register_of_legislation:F2006B10785:body:0
Version: federal_register_of_legislation:F2006B10785
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Israel Aircraft Industries 1123 and 1124 (Westwind) Series Aeroplanes

AD/IAI-W/10 Emergency Lighting System 8/85

 Applicability: As detailed in Requirement Document.

            Requirement: Inspect and Modify the emergency lighting system components according to Accomplishment Instructions Parts 1 and 2 contained in IAI Westwind S.B. 1124-33-010.

 Compliance: Within 150 hours time in service after 31 August 1985. Background: The aircraft manufacturer advises that:
a)        the inertial switch may not be aligned with the longitudinal axis of the aircraft; and

b)        the possibility exists for an inadvertent battery pack short circuit to surrounding structure.