Document ID: chunk:federal_register_of_legislation:F2006B11321:body:0
Version: federal_register_of_legislation:F2006B11321
Segment Type: other
Provision Reference: 
Character Range: 0–713

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

 Aerospatiale Rallye Series Aeroplanes

AD/MSR/22 Rear Fuselage Structure - Inspection 6/76

 Applicability: All models.

             Requirement: 1. Remove the fuselage tail-cone and fin dorsal fairing and, with the aid of a torch, visually inspect the fuselage internal and external stringers for corrosion.

             2. If corrosion is detected remove the empennage components and perform a detailed visual inspection of the rear fuselage structure for corrosion damage.

 Compliance: Before 15 July 1976 and thereafter at intervals not exceeding 3 years.