Document ID: chunk:federal_register_of_legislation:F2006B09510:body:0
Version: federal_register_of_legislation:F2006B09510
Segment Type: other
Provision Reference: 
Character Range: 0–877

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

 Embraer EMB-120 (Brasilia) Series Aeroplanes

AD/EMB-120/22 Wing and Empennage Leading Edge 1/98

 Applicability: All models EMB-120 aircraft.

 Requirement: Inspect in accordance with Embraer Alert Service Bulletin 120-51-A004.

            Note: CTA AD 97-09-07 Amdt 39-802 refers.

 Compliance: Unless already accomplished, within 75 hours time in service after 1 January 1998.

            This airworthiness directive becomes effective on 1 January 1998.

            Background: An occurrence was reported of delaminations in the wing leading edge top layer, immediately behind the ice boot upper edge. This Directive requires a visual inspection for erosion, delamination and condition of sealing and anti-static paint.