Document ID: chunk:federal_register_of_legislation:F2006B04152:body:0
Version: federal_register_of_legislation:F2006B04152
Segment Type: other
Provision Reference: 
Character Range: 0–929

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

 Beechcraft 65 and 70 (Queen Air) Series Aeroplanes

 AD/BEECH 65/56 Cabin, Baggage and Pilot Compartment
 Side Windows - Inspection Applicability: All models 65-88 with S/Nos. LP-1 to LP-26, LP-28 and LP-30 to LP-47. Document:               Beechcraft SI No. 0711-110, Rev. 111.
            Note: FAA AD 81-12-01 Amdt. 39-4126 refers.

8/81

            Compliance: Unless already accomplished, initially inspect within 50 hours' time in service after 7 July 1981 and thereafter at intervals not exceeding 300 hours' time in service or 1 year, whichever occurs first, until windows are replaced in accordance with Beechcraft SI No. 0711-110, Rev. 111.

            Background: In service window failures have occurred both in Australia and overseas in similar type aeroplanes.