Document ID: chunk:federal_register_of_legislation:F2006B10318:body:0
Version: federal_register_of_legislation:F2006B10318
Segment Type: other
Provision Reference: 
Character Range: 0–1180

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

 Grob G115 Series Aeroplanes

AD/GROB 115/11 Aileron Control Rod 7/98

 Applicability: Model G115 and G115A, all serial numbers.

            Requirement: Replace aileron control rods no. 1 (part number 115-4400/4401) with modified aileron control rods no. 1 (part number 115-4410/4411) in accordance with Grob Service Bulletin (SB)1078-14.

            Note 1: LBA AD 90-229 refers.

            Note 2: Aileron control rods (part number 115-4400/4401) removed from aircraft or in storage should be rendered unserviceable or destroyed.

            Compliance: Unless already accomplished, replace within 20 hours time in service after 18 June 1998.

            This airworthiness directive becomes effective on 18 June 1998.

            Background: Application of high control forces can distort the aileron control rod no. 1 (part number 115-4400/4401), interfering with proper control of the aircraft. This directive requires installation of a modified control rod with an additional stop to prevent damage during operation.