Document ID: chunk:federal_register_of_legislation:F2006B07879:body:0
Version: federal_register_of_legislation:F2006B07879
Segment Type: other
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Character Range: 0–3083

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