AD/ELECT/47 - Propeller De-Ice Terminal Clamp Assembly

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

Legislation au F2006B09422 Not in force Legislative Instrument

Legislation content

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 107 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Electrical Equipment

 

AD/ELECT/47 Propeller De-Ice Terminal Clamp Assembly 1/86

Applicability: B.F. Goodrich propeller de-icer terminal clamp assembly P/No 3E1883-2 fitted to Hartzell HC-B3TN and HC-B4TN series propellers.

 

Requirement: Inspect the terminal clamp assembly for cracks according to the requirements of B.F. Goodrich SB No E-85-71.

 

Compliance: Prior to issue of the next maintenance release after 31 January 1986.

 

Background: Overstressing of the terminal clamp assembly during maintenance may cause cracking around the attachment holes. Complete failure may lead to the separation of the terminal clamp assembly from the propeller with the possibility of striking the aircraft fuselage.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.