AD/DC4/1 - Vacuum System - Modification

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

Legislation au F2006B08814 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

 


Douglas DC4 Series Aeroplanes

 

AD/DC4/1 Vacuum System - Modification NK

Applicability: All models.

 

Requirement: Rework the vacuum system in accordance with either of the following modifications:

 

  1. Replace the present oil separator with a Genesco No. 40081 separator.

 

The new separator incorporates a pressure relief valve and can be dismantled for cleaning; or

 

2.    Install a fusible plug in the side of the vacuum pump discharge port at right angles to the axis of the discharge port boss.

 

Note: Some pumps incorporate a plugged hole in the discharge port which may be enlarged to a 3/8 in. NPT tapped hole to accommodate the fusible plug. This plug should employ an AN-840-8D fitting with a binary eutectic mixture of 68 per cent tin and 32 per cent cadmium which has a melting point of 351oF (See Figure 1). The 3/8 in. fusible plug is intended for pumps model 3P211 and 3P485. For smaller pumps a modified AN-840-6D fitting should be used.

 

or FAA AD 49-46-1; or ANO 105.1.16.0.1.1.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.