1Airworthiness Directives 2004 - Revocation and Remaking - Beagle B121 (Pup) Series Aeroplanes

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.

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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