Airworthiness Directives 2004 - Revocation and Remaking - Gates Learjet 35 and 36 Series Aeroplanes (Cth)

Airworthiness Directives 2004

I, DAVID ALAN VILLIERS, delegate of the Civil Aviation Safety Authority, acting under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998:

(a) revoke the Airworthiness Directives mentioned in Schedule 1; and

(b) make, as separate instruments, each Airworthiness Directive mentioned in Schedule 1 and attached.

David Villiers Delegate of the Civil Aviation Safety Authority

20 December 2004

Note: Each attached Airworthiness Directive is being re-made in exactly the same form as appears in the latest published edition of the Directive.

Schedule 1 Revocation and Remaking of Airworthiness Directives

Gates Learjet 35 and 36 Series Aeroplanes

AD Name AD Number

Primary Control System Stop Bolts - Inspection and Replacement AD/LEARJET 35/1

Spoiler Centre Hinge Brackets - Inspection AD/LEARJET 35/2

Lower Cabin Door Jambs - Inspection AD/LEARJET 35/3

Upper Wing Skin Fasteners - Inspection AD/LEARJET 35/4

Angle of Attack Indicator - Modification AD/LEARJET 35/5

Wing to Fuselage Attachment - Modification AD/LEARJET 35/6

Spoileron Computer - Modification AD/LEARJET 35/7

Refrigeration System Condenser Fan - Inspection and Replacement AD/LEARJET 35/8

Secondary Yaw Damper Servo Cable Clamp Bolt - Inspection AD/LEARJET 35/9

Cabin Altitude Pressure Limiter - Installation AD/LEARJET 35/10

Elevator Control System - Modification AD/LEARJET 35/11

Upper Cabin Door Locking Mechanism - Modification AD/LEARJET 35/12

Upper Cabin Door Lock Mechanism Bolts - Modification AD/LEARJET 35/13

Tailcone Service Area - Inspection AD/LEARJET 35/14 Amdt 1

Automatic Flight Control Systems - Inspection and Modification AD/LEARJET 35/15

Maximum Operating Airspeed (VMO) - Reduction and Terminating Modification AD/LEARJET 35/16