Document ID: chunk:federal_register_of_legislation:F2006B06972:body:0
Version: federal_register_of_legislation:F2006B06972
Segment Type: other
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Character Range: 0–786

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

 SAAB SF340 Series Aeroplanes

AD/SF340/43 Power Lever Placard  7/94 DM

 Applicability: All SAAB SF 340A S/N 004 through 159 and SF 340B S/N 160 through 379. Requirement:               Action in accordance with SAAB Service Bulletin 340-76-033.
            Note: FAA AD 94-09-09 amdt 39-8898 refers.

 Compliance: Unless previously carried out within 14 days from 16 May 1994.

            Background:  Advice has been received of a recent event overseas where during descent all engine power was lost after both propellers overspeed possibly due to an inadvertent crew selection of the power levers to a position below 'flight idle'.