Document ID: chunk:federal_register_of_legislation:F2006B04316:body:0
Version: federal_register_of_legislation:F2006B04316
Segment Type: other
Provision Reference: 
Character Range: 0–767

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

 Beechcraft 99 Series Aeroplanes

AD/BEECH 99/6 Wing Structural Fatigue Limitations 12/96

 Applicability: All model 99 aircraft.

            Requirement: Inspect and retire the wing structural components in accordance with the Beechcraft 99 Airliner Series Continued Airworthiness Program Inspection Manual P/N 98- 30131 Rev. A1, Sections 57-10 and 57-20.

            Note: FAA AD 92-15-13 refers.

 Compliance: This Directive takes effect 7 November 1996.

            Background:  This Directive requires life limited components to be retired to prevent fatigue failure of the wing spar and associated structure.