Document ID: chunk:federal_register_of_legislation:F2006B01839:body:0
Version: federal_register_of_legislation:F2006B01839
Segment Type: other
Provision Reference: 
Character Range: 0–796

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

 Agusta A109 Series Helicopters

AD/A109/9 Engine Mount Installation 6/87

 Applicability: All models A109A and A109AII up to and including S/N 7361 except S/N 7359. Requirement:               Action in accordance with Bollettino Tecnico 109-61 Part I and Part II.
            Compliance: Within 100 hours' time in service after 4 June 1987 or at the next scheduled inspection for Maintenance Release issue after 4 June 1987, whichever is later.

            Note: RAI AD 87-43/109-42 refers.

            Background: Chafing of an oil scavenge line against a mount leg has initiated corrosion which has in one case penetrated through the tubing.