AD/EMB-110/22 - Rudder Pedal Assembly, Main Bearing Attachment - Inspection and Modification

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

Legislation au F2006B09463 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

 


Embraer EMB-110 (Bandeirante) Series Aeroplanes

 

AD/EMB-110/22 Rudder Pedal Assembly, Main Bearing

Attachment - Inspection and Modification

Applicability: All model EMB-110 with S/Nos. 110001 to 110385. Document:  Embraer SB No. 110-27-058.

Note: Brazilian AD 82-11-02 refers.


3/83

 

Compliance: Within 25 hours time in service after 21 January, 1983 and thereafter at intervals not exceeding 100 hours time in service until modified in accordance with Section II of the requirement document.

 

Background: Manufacturer reports that a bearing was displaced from its housing flange rendering the rudder control inoperative.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.