Commonwealth legislation

AD/CESSNA 206/29 - Fuel Flow Stabilisation Placard

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This Airworthiness Directive requires owners/operators of specified Cessna 206, U206 and P206 aircraft (listed by serial number) to fit a fuel‑flow stabilisation placard and follow Cessna Service Instruction Letter SE79‑25 Supplement No.1 addressing fuel vapour and engine‑restart procedures. The work must be done within 100 hours' time in service after 31 October 1979. It changes operating and maintenance obligations for the affected aircraft to reduce in‑flight power interruptions linked to fuel vapour, by mandating placarding and procedural compliance.

JSON API

Deep dive

Want the full deep dive?

Zoe can write the in-depth analysis on top of the summary above: how it works, who it affects and what each part actually does.

Current sections

Direct links to the current provisions in AD/CESSNA 206/29 - Fuel Flow Stabilisation Placard.

AD/CESSNA 206/29 - Fuel Flow Stabilisation Placard

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 206 Series Aeroplanes

AD/CESSNA 206/29 Fuel Flow Stabilisation Placard 10/79

Applicability: Model 206 with S/Nos. 206-0001 to 206-0136 (with SK206-2 Installed) and 206-

0138 to 206-0275.

Model U206 with S/Nos. U206-0276 to U206-04287, 04289, 04290, 04292 to 04335,

04337 to 04389, 04391 to 04787, 04789 to 04894, 04896 to 04906, 04908 to 04911,

04913 to 04958, 04960 to 04963, 04965 to 04973, 04975 to 04977, 04980 to 04985,

04987 to 04990, 04992, 04993, 04995 to 04998, 05000 to 05018, 05020 to 05058,

05060, 05061, 05063, 05066, 05069, 05071 to 05073, 05075, 05077, 05078, 05083,

05085, 05086, 05088, 05095, 05097, 05100, 05102, 05105, 05107 and 05110.

Model P206 with S/Nos. P206-0001 to P20600647.

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.

1 AD/CESSNA 206/29 - Fuel Flow Stabilisation Placard