Commonwealth legislation

AD/CESSNA 207/20 - Fuel Flow Stabilisation Placard

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Commonwealth

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legislative instrument

Plain English Summary

2/10 complexity

This AD requires owners/operators of Cessna 207 (s/n 20700001–20700530) to install a fuel‑flow stabilisation placard and follow Cessna’s Service Instruction Letter procedures to recognise/eliminate excessive fuel vapour and to restart the engine after inflight power interruptions. Compliance is mandatory within 100 flight hours after 31 Oct 1979; implementation costs and method rely on the manufacturer’s SIL and are borne by operators.

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AD/CESSNA 207/20 - Fuel Flow Stabilisation Placard

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source Cessna 207 Series Aeroplanes

AD/CESSNA 207/20 Fuel Flow Stabilisation Placard 10/79

Applicability: Model 207 with S/Nos 20700001 to 20700530.

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.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.