AD/CESSNA 310/40 - Pre-Certification Requirements - Modifications

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Legislation au F2006B08168 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 310 Series Aeroplanes

 

AD/CESSNA 310/40  Pre-Certification Requirements - Modifications


9/75

 

Applicability: All model 310R.

 

Requirement: Modify the aircraft in accordance with the requirements of ANO 101.22 in respect of the following:

 

  1. Install a placard in the cabin specifying the periods during which smoking is prohibited.

 

2.    (a) Install fuelling equipment bonding points at each fuel filling point.

 

(b) Install and identify external earthing points for the attachment of ground connections on each main under- carriage assembly or on the nose gear.

 

3.    Modify the turn co-ordinator failure warning system to continuously monitor the instrument power supply, to a scheme approved by the Secretary.

 

4.    Modify the aircraft external electrical power system to prevent a power supply of reversed polarity or phase sequence being connected to the aircraft electrical system, to a scheme approved by the Secretary.

 

Compliance: Before 30 September 1975.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.