Document ID: chunk:federal_register_of_legislation:F2006B09513:body:0
Version: federal_register_of_legislation:F2006B09513
Segment Type: other
Provision Reference: 
Character Range: 0–954

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-120/26 Wing-to-Fuselage Fittings 3/99
 Applicability: All Model EMB-120 aircraft that have accumulated more than 4,000 flight cycles. Requirement:               Perform a detailed visual inspection in accordance with Embraer Service Bulletin
            120-57-0034 Revision 1. Results of the inspection to be forwarded to Embraer.

            Note: CTA AD 1999-01-01 Amdt 39-845 refers.

 Compliance: Unless already accomplished, within 400 flight cycles after 25 March 1999.

            This Airworthiness Directive becomes effective on 25 March 1999.

            Background: The CTA received reports of cracks in the fuselage attachment area of the wing-to- fuselage fittings on two aircraft, and requires an evaluation of the "Brasilia" fleet.