Document ID: chunk:federal_register_of_legislation:F2006B11148:body:0
Version: federal_register_of_legislation:F2006B11148
Segment Type: other
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Character Range: 0–799

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

 Gates Learjet 24 & 25 Series Aeroplanes

 AD/LEARJET/30
 Amdt 2

     Flap System and Flap Sector Mounting Brackets

 1/87

 Applicability: All model Learjet with S/Nos. listed in requirement documents. Requirement: Modify in accordance with Gates Learjet SB AMK 86-4.
            Compliance: 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 originally issued due to cracking in the flap sector mounting brackets. This amendment replaces the aluminium brackets with steel items and terminates any further requirement.