Document ID: chunk:federal_register_of_legislation:F2006B05198:body:0
Version: federal_register_of_legislation:F2006B05198
Segment Type: other
Provision Reference: 
Character Range: 0–851

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Cessna 205 (210-5) Series Aeroplanes

AD/CESSNA 205/14 Fuel Flow Stabilisation Placard 10/79

 Applicability: Model 205 with S/Nos. 205-0001 to 205-0555 (with SK205-5 installed) and 205-0556
            to 205-0577.

 Requirement: Action in accordance with Cessna SIL No. SE79-25, Supplement No. 1.

            Note: FAA AD 79-15-01, Amendment 39-3517 refers.

 Compliance: Within 100 hours time in service after 31 October 1979.

            Background: The manufacturer has made placards and instructions available to aid in the recognition and elimination of excessive vapour from the aircraft fuel system. In the event of inflight power interruptions engine restart procedures are also detailed.