Document ID: chunk:federal_register_of_legislation:F2006B06849:body:0
Version: federal_register_of_legislation:F2006B06849
Segment Type: other
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Character Range: 0–820

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

 Short SD3-30 Series Aeroplanes

AD/SD3-30/5 Aileron, Pilots Handwheel Stop - Modification 1/82

            Applicability: SD 3-30 aircraft with S/Nos. SH 3002 to SH 3067 fitted with PT6A-45R engines (SB SD3-71-11), and S/Nos. SH 3068 to SH 3071, SH 3073, SH 3075, SH 3077 and SH
            3078.

 Document: Shorts SB No. SD3-27-23.

            (Modification No. 6255).

 Compliance: Unless already accomplished, within 400 hours time in service after 31 January 1981.

            Background:  During flight testing after fitting PT6A-45R engines, it was found that in some low weight configurations the aircraft was marginally below the required VMCL rate of roll.