AD/ELECT/65 - Marathon Power Technologies PC-250 Static Inverter

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

Legislation au F2006B09440 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/65 Marathon Power Technologies PC-250 Static Inverter


10/94

 

Applicability: Marathon Power Technologies PC-250 series static inverters, where installed to provide a source of emergency or standby electrical power.

 

Note: These inverters are known to be installed in, but not limited to, the following aircraft models:

 

Hawker 800 and BAe 125 Series 800 prior to Constructors Number 258248

 

DH/BH/HS/BAe 125 Series 1 to 700 post modification 252740

 

Requirement: Action in accordance with Marathon Power Technologies Service Bulletin 111692- 014 Revision 1 dated 15 March 1993.

 

Note: CAA(UK) AD 005-05-94 refers.

 

Compliance: Prior to 15 March 1995.

 

Background: The CAA(UK) has reported that PC-250 static inverters have failed because of moisture ingress. Compliance with this Directive will ensure that the inverters are protected from moisture ingress.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.