Document ID: chunk:federal_register_of_legislation:F2006B08090:body:0
Version: federal_register_of_legislation:F2006B08090
Segment Type: other
Provision Reference: 
Character Range: 0–1256

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

 Cessna 210 Series Aeroplanes

                             AD/CESSNA 210/41 Fuel Flow Stabilisation Placard - Installation

10/79

Applicability: Model 210 with S/Nos. 21057841 to 58220 (with SK205-5 installed) 58221 to 58351
(with SK206-2 installed), 58352 to 63013, 63015 to 63086, 63088 to 63228, 63230 to
            63287, 63289 to 63298, 63300 to 63324, 63326 to 63389, 63391 to 63393, 63396 to
            63399, 63401, 63403 to 63407, 63412, 63413, 63419, 63424 and 63426. Model T210
            with S/Nos. T210-0001 to T210-0454. Model P210 with S/Nos. P21000001 to 00255, 00257 to 00273, 00275 to 00279, 00281 to 00283, 00287, 00290 and 00292.

            Document: 1. Cessna SIL No. SE79-25, Supplement No. 1 or 2. FAA AD 79-15-01, Amendment 39-3517.
 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.