AD/CESSNA 210/53 - Oxygen Indicator Lights - Modification

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

Legislation au F2006B08102 Not 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

 


Cessna 210 Series Aeroplanes

 

AD/CESSNA 210/53 Oxygen Indicator Lights - Modification 12/81

Applicability: All P210 Series with a solid state chemical oxygen system installed.

 

Requirement: Install a press to test system in the oxygen indicator light circuits so that the indicator lights can be tested prior to each flight.

 

Compliance: Within 200 hours time in service or before the aircraft is cleared to operate to 23,000 feet maximum altitude after additional supplementary oxygen is installed to comply with ANO 20.4

 

Background: The chemical oxygen system in Cessna aircraft has been reviewed by the Flying Operations Branch and additional supplementary oxygen is considered necessary to meet the requirements of ANO 20.4. The addition of the press to test system for the oxygen indicator lights is considered a satisfactory method for meeting the requirement of ANO 20.4 para. 4.1.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.