AD/LEARJET 35/21 Amdt 1 - Engine Hydraulic Line Interference - Inspection
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text 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.
- 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.