Document ID: chunk:federal_register_of_legislation:F2006B09350:body:0
Version: federal_register_of_legislation:F2006B09350
Segment Type: other
Provision Reference: 
Character Range: 0–803

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

 Eurocopter AS 350 (Ecureuil) Series Helicopters

AD/ECUREUIL/45 Tail Rotor Pitch Control Lever Expansion Pin 9/91

                                                          DM

 Applicability: All AS350 Helicopters versions B, B1, B2 and D.

            Requirement: Action in accordance with the Technical Requirements of DGAC TAD T91-137-059 (B).

            Note: Aerospatiale TSB 01-33 refers.

 Compliance: A specified in the requirement document with revised effective date of 10 July 1991.

            Background: One lug of the tail rotor gearbox control lever hinge yoke failed through incorrect assembly of the bushes on the expansion pin.