AD/LEARJET 35/1 - Primary Control System Stop Bolts - Inspection and Replacement
1AD/LEARJET 35/1 - Primary Control System Stop Bolts - Inspection and Replacement
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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 35/1 Primary Control System Stop Bolts - Inspection and Replacement
Applicability: All model 35 with S/Nos. 35-001 to 35-039.
All model 36 with S/Nos. 36-001 to 36-016.
Document: Gates Learjet SB 35/36-27-3.
Compliance: Within 300 hours time in service after 30 April 1976.
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