Document ID: chunk:federal_register_of_legislation:F2006B10325:body:0
Version: federal_register_of_legislation:F2006B10325
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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 115/6 Elevator - Lever 5/95 DM

Applicability: All Grob G115, G115A and G115B.

            Requirement: Carry out a dye penetrant inspection of the elevator lever (P/N 115-3571) for cracks in accordance with Grob G115 Service Bulletin TM 1078-29.

Note: LBA AD 93-135 Grob refers.

 Compliance: Initially inspect within 5 hours time in service from 29 March 1995.

            Re-inspect at intervals not to exceed 100 hours time in service.

            Background: A report has been received of cracks in the elevator lever. Precautionary inspections will ensure that the airworthiness of the aircraft is maintained.