Document ID: chunk:federal_register_of_legislation:F2006B04327:body:0
Version: federal_register_of_legislation:F2006B04327
Segment Type: other
Provision Reference: 
Character Range: 0–1211

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

 Bell Helicopter Textron 204 Series Helicopters

AD/BELL 204/21 Main Rotor Blades - Inspection NK

            Applicability: All models 204B with main rotor blades P/Nos. 204-012-001 (all dash numbers) and 204-011-250 (all dash numbers) which have achieved 600 hours' time in service.

 Requirement: To detect cracks in the main rotor blades, perform the following:

              1. Visually inspect the upper surface of each blade in the area of the spare particularly between stations 110 and 165.

2.    Cone each blade by inserting a wooden wedge between the mast and the static stop and raise the tip of the blade sufficiently to eliminate blade droop and obtain approx. 6 ins. (15 cms) blade cone at the tip; and

3.    Visually inspect the undersurface of each blade particularly in the area of the spare between stations 110 and 165.

            Note: Refer to the Maintenance Manual Section 1, Page 1-23 and 1-24 Section II, Page 2-6, Para 2-7B for inspection requirements.

 Compliance: At each daily or overnight inspection after 11 November 1975.