AD/GROB 115/11 - Aileron Control Rod

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B10318 In force Legislative Instrument

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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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.