AD/GENERAL/22 - Engine Oil Tank - Modification

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

Legislation au F2006B10268 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

 


Aircraft - General

 

AD/GENERAL/22 Engine Oil Tank - Modification NK

Applicability: All aeroplanes fitted with hydraulically operated feathering propellers which draw their feathering oil supply from the engine oil tank.

 

Requirement: 1. Modify engine oil tanks by reworking the engine oil supply standpipe in such a manner that, in the event of exhaustion of the engine oil supply, sufficient oil will be retained in the tank to enable the propeller to be feathered. This reserve supply shall be available only to the feathering pump; or

 

Note: In some installations incorporating a hopper in the oil tank, there is a possibility of an increase in the height of the standpipe causing a restriction of the flow of oil from tank to hopper leading to oil starvation under cold starting conditions and overheating of oil under high power. In such cases, it will be necessary also to modify the neck of the hopper to ensure that restriction of oil flow cannot take place.

 

2. ANO 105.1.0.1.49; or

 

3. AD/DC3/22.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.