Document ID: chunk:federal_register_of_legislation:F2006B06913:body:0
Version: federal_register_of_legislation:F2006B06913
Segment Type: other
Provision Reference: 
Character Range: 0–929

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

 Short SD3-60 Series Aeroplanes

 AD/SD3-60/8
 Amdt 2

                                      Elevator Torque Shaft Assembly 6/85 DM

 Applicability:  All Models SD-360 aircraft. Requirement: 1. Shorts SB SD360-27-A06 Rev 1.
            2. Shorts SB SD360-27-06.

             Compliance: 1. Prior to 14 March 1985 and thereafter at intervals not exceeding 60 hours time in service or pre-first flight following parking in severe wind gust conditions.

            2. Prior to 15 August 1985.

            Background: This Directive was issued after loss of elevator control on a SD3-30 aircraft. Rev 1 extended the inspection area and introduced a repetitive inspection. Rev 2 introduces mandatory modification to reinforce the attachment of the elevator torque shaft housings.