Document ID: chunk:federal_register_of_legislation:F2006B10348:body:0
Version: federal_register_of_legislation:F2006B10348
Segment Type: other
Provision Reference: 
Character Range: 0–764

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

 Hiller UH-12 Series Helicopters

AD/HILLER 12/19 Main Rotor Blades - Inspection 11/71

 Applicability: All models.

 Requirement: 1. Carry out a visual inspection for cracks in the main rotor blades P/No. 53100.

            Note: This inspection may be performed and certified by the pilot.

            2. Inspect blades P/N 53100 for cracks using an approved dye penetrant method.

            Note: Any blades found defective shall be removed from service before further flight.

 Compliance: For Para. 1 - Before further flight.

            For Para. 2 - Within 10 hours' time in service after 16 Nov. 1971.