1AD/LEARJET 35/18 - Horizontal Stabiliser Hinge Pin Bushing Installation - 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 35/18 Horizontal Stabiliser Hinge Pin Bushing

Installation - Inspection

12/81

 

Applicability: All models 35 & 36 with S/Nos. referenced in Gates Learjet Service Bulletin No.

35/36-27-13 or with S/Nos. referenced in subsequent issues of that Service Bulletin.

 

Document: Gates Learjet SB 35/36-27-13.

 

Compliance: Within 100 hours time in service after 31 December, 1981.

 

Background:  The horizontal stabiliser hinge pin bushings may move out of their mating fittings during normal service.