Commonwealth legislation

AD/GROB 115/6 - Elevator - Lever

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

The directive mandates immediate and recurring dye‑penetrant inspections of the elevator lever on Grob G115/G115A/G115B aircraft (per the manufacturer’s service bulletin) to detect cracks and preserve airworthiness. It falls on operators/maintenance providers, who bear inspection and any repair costs, and imposes short‑term downtime and ongoing 100‑hour inspection intervals, while procedural and remedial details are delegated to the referenced service bulletin.

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AD/GROB 115/6 - Elevator - Lever

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source 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.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.