AD/TB20/11 - Hydraulic Brake Line Clearance

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

Legislation au F2006B07314 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

 


Aerospatiale (Socata) TB20 (Trinidad) Series Aeroplanes

 

AD/TB20/11 Hydraulic Brake Line Clearance 11/87

Applicability: All model TB20 and TB21 up to S/No 755 inclusive, except S/Nos 630, 631, 634, 636, 643, 648, 649, 656, 657, 658, 659, 661, 662, 663, 664, 750, 751, 752 and 753.

 

Requirement: Action in accordance with Aerospatiale Socata SB No 33.

 

Note: Bureau Veritas AD 87-118(A) refers.

 

Compliance: Within 100 hours time in service or at the next scheduled inspection for maintenance release issue after 30 October 1987 whichever is the earlier.

 

Background: The manufacturer has reported instances of the cockpit hydraulic brake lines being damaged by the aileron and rudder control rods.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.