Document ID: chunk:federal_register_of_legislation:F2006B11102:body:0
Version: federal_register_of_legislation:F2006B11102
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Gates Learjet 35 and 36 Series Aeroplanes

 AD/LEARJET 35/23
 Amdt 2

     Flap System and Flap Sector Mounting Brackets

 1/87

 Applicability: All models Learjet with serial numbers listed in Requirement Document. Requirement:              Modify in accordance with Gates Learjet SB AMK 86-4.
            Compliance: Unless already accomplished, within 100 hours time in service or at the next inspection for Maintenance Release issue after 31 January 1987 whichever is later.

            Background: This Directive was initially issued due to cracking of the flap sector mounting brackets. A repetitive inspection was later included because of further cracking after inspection. This amendment now requires modification using steel sector mounting brackets and deletes the repetitive inspection.