Document ID: chunk:federal_register_of_legislation:F2006B07735:body:0
Version: federal_register_of_legislation:F2006B07735
Segment Type: other
Provision Reference: 
Character Range: 0–2219

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

 Beagle B121 (Pup) Series Aeroplanes

 AD Name AD Number

 Fuel Tank Modification - CANCELLED AD/BEA 121/1

 Rudder Control Torque Tubes AD/BEA 121/2

 Engine Bearers AD/BEA 121/3

 Dual Throttle Control AD/BEA 121/4

 Rudder Control Lever Assembly P/N BE 45.10193 AD/BEA 121/5 Amdt 1

 Fuel Tank Non-Return Valves AD/BEA 121/6

 Elevator Torque Tubes AD/BEA 121/7 Amdt 1

 Rudder Control Torque Tubes AD/BEA 121/8 Amdt 3

 Bonding Points AD/BEA 121/9

 Rudder Drain Hole AD/BEA 121/10

 Fuel Tanks AD/BEA 121/11

 Front Seat Restraint Installation AD/BEA 121/12

 Internal Door Lock Operating Handle AD/BEA 121/13

 Fuselage/Mainplane Attachments AD/BEA 121/14 Amdt 3

 Flap Actuating Lever Assemblies AD/BEA 121/15

 Fuselage/Mainplane Attachments AD/BEA 121/16 Amdt 1

 Nosewheel Steering Mechanism AD/BEA 121/17

 Rudder Control Lever AD/BEA 121/18

 Rudder Pedal Anchorages AD/BEA 121/19

 Throttle Cable Assembly AD/BEA 121/20

 Nose Undercarriage and Rudder Control System AD/BEA 121/21

 Wing Spar Web AD/BEA 121/22 Amdt 1

 Engine Mounting Structure AD/BEA 121/23

 Fuselage Angle, Diaphragm and Flange at Tailplane Spar Attachments AD/BEA 121/24

 Control Rod End Fittings AD/BEA 121/25

 Rudder Control Tube Bolt AD/BEA 121/26

 Control Column Handgrips AD/BEA 121/27 Amdt 2

 Wing to Fuselage Main Spar Attachment Fitting AD/BEA 121/28

 Aircraft Fatigue Life AD/BEA 121/29

 Brake Torque Tube Assembly AD/BEA 121/30

 Main Spar Doubler at Main Landing Gear Attachment and Wing to Fuselage  AD/BEA 121/31 Amdt 1