AD/EMB-110/23 - Trim Tab Control Systems - Inspection and Modification

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

Legislation au F2006B09464 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-110/23 Trim Tab Control Systems - Inspection

and Modification

Applicability: All models EMB-110 with S/Nos. 110001 to 110364 and 110366 to 110384. Document:               Embraer SB No. 110-27-062 Parts I and II.

Note: Brazilian AD 82-11-03 refers.

Compliance: PART 1: Within 25 hours time in service after 25 January 1983.


3/83

 

PART II: Within 125 hours time in service or one month, whichever occurs first, after 25 January, 1983.

 

Background: Investigation by the manufacturer revealed that the attaching nuts of the actuating rod ends of the trim cab systems may become loose.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.