Document ID: chunk:federal_register_of_legislation:F2006B11100:body:0
Version: federal_register_of_legislation:F2006B11100
Segment Type: other
Provision Reference: 
Character Range: 0–942

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 35/21
 Amdt 1

 Engine Hydraulic Line Interference - Inspection

 10/83

            Applicability: All model 35 and 36 series aircraft as detailed in Gates Learjet Service Bulletins 35/36-29-1 and 35/36-29-2.

 Document: 1. Gates Learjet SB 35/36-29-1.

            Note: FAA AD 83-08-3 refers.

            2. Gates Learjet SB 35/36-29-2.

 Compliance: Requirement Document No. 1: Within 100 hours time in service after 30 April 1983.

            Requirement Document No. 2: Within 100 hours time in service after 30 September 1983.

            Background:  This directive has been raised in issue to include a further manufacturers SB related to interference between hydraulic lines and adjacent components in the tailcone area.