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