Document ID: chunk:federal_register_of_legislation:F2006B07353:body:0
Version: federal_register_of_legislation:F2006B07353
Segment Type: other
Provision Reference: 
Character Range: 0–793

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

 Aerospatiale (Socata) TB20 (Trinidad) Series Aeroplanes

AD/TB20/7 Stabilator Control Rod Ends 4/87 DM

 Applicability: All models with S/Nos 1 to 709, except S/Nos 652, 653, 661, 664, 665, 672, 691, 701
            to 706.

 Requirement: Action in accordance with Socata S.B. No. 29.

            Note: Bureau Veritas AD 87-003(A) refers.

            Compliance: Within 25 hours time-in-service after 6 February 1987 and thereafter at each scheduled inspection for Maintenance Release issue until modified.

            Background: The manufacturer reports instances of stabilator operating rod ends with excessive play due to loose rivets.