AD/TB10/7 - Battery Tray Installation

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

Legislation au F2006B07309 In force Legislative Instrument

Legislation content

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Aerospatiale (Socata) TB9 and TB10 (Tobago) Series Aeroplanes

 

AD/TB10/7 Battery Tray Installation 10/85

Applicability: All models TB9 and TB10 series with S/nos up to 441 but excluding S/nos 343, 382, 414, 423, 425 to 429 and 434 to 438.

 

Requirement: Inspect and modify the battery tray installation in accordance with the requirements detailed in Socata Service Letter No. 18 under description paragraph 1. Pay particular attention to surrounding fuselage structure for signs of electrolyte spillage and subsequent damage.

 

Note: French AD 85-130-(A) refers.

 

Compliance: Within 50 hours time in service after 31 October 1985.

 

Background:  The battery tray installation may be such that electrolyte spillage from the battery could cause fuselage structural damage due to corrosion.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.