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

Cabin Interior Liner in Areas of Emergency Exit Door - Inspection             AD/LEARJET 35/17

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

Stall Warning Accelerometer  AD/LEARJET 35/19 Amdt 1

Engine Firewall Sealing  AD/LEARJET 35/20

Engine Hydraulic Line Interference - Inspection  AD/LEARJET 35/21 Amdt 1

Aileron Trim Tab Balance Weight - Replacement  AD/LEARJET 35/22

Flap System and Flap Sector Mounting Brackets  AD/LEARJET 35/23 Amdt 2

Battery Vent System  AD/LEARJET 35/24 Amdt 2

Flap Attachment Fittings  AD/LEARJET 35/25

Forward Engine Mounts  AD/LEARJET 35/26

Fluorescent Lighting Inverters  AD/LEARJET 35/27 Amdt 1

Crew Oxygen Plumbing and Map Light Wire Protection  AD/LEARJET 35/28

Retirement Life - Fatigue Critical Components  AD/LEARJET 35/29

Flight Management Systems  AD/LEARJET 35/30

Emergency Brake Handle  AD/LEARJET 35/31

Tip Tank Flapper Valves  AD/LEARJET 35/32

Outflow/Safety Valve  AD/LEARJET 35/33

Auxiliary Cabin Heater Wiring  AD/LEARJET 35/34 Amdt 1

Mach Limit  AD/LEARJET 35/35

Spoiler Actuators  AD/LEARJET 35/36

Emergency Procedures - AFM Amendment  AD/LEARJET 35/37

Main Landing Gear Tyre  AD/LEARJET 35/38

Forward Engine Beam Shear Web  AD/LEARJET 35/39