AD/GROB 115/6 - Elevator - Lever
1AD/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
Image unavailable in extracted text 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.