AD/TB10/13 - Aircraft Wiring/Support Bracket Clearance

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

Legislation au F2006B07280 Not 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/TB10/13 Aircraft Wiring/Support Bracket Clearance 2/90

Applicability: All Socata TB10 aircraft.

 

Requirement:  Inspect the aircraft to ensure that adequate clearance exists between the folded edge of the terminal block support bracket behind the LH firewall door (assy P/N TB10- 23-020-104) and the adjacent terminal board wiring. Modify aircraft if necessary.

 

Compliance: Within 100 hours time in service after 22 February 1990.

 

Background:  One instance has been reported where the terminal block support bracket behind the LH firewall door chaffed through 3 live wires of the adjacent terminal board wiring.

 

It is considered that this condition could exist on other aircraft of this type. Therefore, to prevent a potentially serious situation, inspection (and modification as necessary) is required.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Interactions

Authorises

All Versions

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.