Commonwealth legislation

AD/ROBIN/15 - Lateral Console Panel

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This airworthiness directive requires inspection and modification of Robin ATL aeroplanes (serial numbers up to 89, with a few exclusions) per ROBIN SA Service Bulletin No. 7 to stop the lateral console panel contacting and potentially jamming the rudder pedals. Affected owners/operators must arrange the work promptly — grounding aircraft if contact is found — and bear the cost and operational disruption to meet the short compliance deadlines.

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Current sections

Direct links to the current provisions in AD/ROBIN/15 - Lateral Console Panel.

AD/ROBIN/15 - Lateral Console Panel

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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 Robin Aviation Series Aeroplanes

AD/ROBIN/15 Lateral Console Panel 7/92

Applicability: ATL, all types, to S/No 89 inclusive, except S/No 22, 28, 53, 71 and 82. Requirement: Action in accordance with ROBIN SA SB No 7.

Note: DGAC AD 91-018(A) refers.

Compliance: Unless already accomplished; prior to further flight after 30 June 1992 if contact is evident, if no contact is evident accomplish modification prior to 31 July 1992.

Background: The DGAC requires an inspection and modification in order to prevent contact between the rudder pedals and the lateral console panel which could lead to the rudder pedals jamming.

Source text

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