Commonwealth legislation

Airworthiness Directives 2004 - Revocation and Remaking - DHC-2 (Beaver) Series Aeroplanes

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This instrument revokes a list of Airworthiness Directives (ADs) that apply to DHC‑2 (Beaver) series aeroplanes and re‑issues each AD as a separate, identical instrument under CASA subregulation 39.001(1). It affects owners, operators and maintenance organisations of DHC‑2 aircraft because the re‑made ADs continue to impose mandatory inspections, modifications and placard requirements; those parties bear the compliance costs and CASA (through its delegate) remains the decision‑maker enforcing the same obligations.

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Airworthiness Directives 2004 - Revocation and Remaking - DHC-2 (Beaver) 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

DHC-2 (Beaver) Series Aeroplanes

AD Name AD Number

Fuel Tanks Inspection and No Smoking Placards AD/DHC-2/1

Hydraulic Control Unit - Selector Lever Hub Inspection AD/DHC-2/2

Rudder Pedal Assembly - Modification AD/DHC-2/3

Undercarriage Legs - Anti-Corrosion Treatment AD/DHC-2/4

CANCELLED AD/DHC-2/5

Safety Harness Inertia Reel - Installation AD/DHC-2/6

Aileron Differential Mount - Modification AD/DHC-2/7

Beaver Wing - Prevention of Flutter - Inspection AD/DHC-2/8

Superseded by AD/DHC-2/10 - CANCELLED AD/DHC-2/9

Lift Strut and Lift Strut Attachment Fittings AD/DHC-2/10 Amdt 8

Aileron Hinge Arm - Inspection AD/DHC-2/11

Left and Right Wing Intermediate Rib Assembly Stations 15.50, 29.00 and AD/DHC-2/12 Amdt 2

Wing - Inspection and Modification AD/DHC-2/13

Main Undercarriage Lower Forward Attachment - Modification AD/DHC-2/14

Main Undercarriage Lower Forward Bolt Attachment - Inspection AD/DHC-2/15 Amdt 1

Aileron Centre Hinge Bracket - Inspection AD/DHC-2/16

Fin Rear Attachment - Inspection AD/DHC-2/17

Tailplane Rear Spar - Inspection and Modification AD/DHC-2/18

Aileron Control Cables - Inspection AD/DHC-2/19 Amdt 1

Control Column Torque Tubes - Inspection AD/DHC-2/20

Flight Controls, Elevator Root Rib - Inspection AD/DHC-2/21

Aileron Centre Hinge Bracket AD/DHC-2/22 Amdt 1

Stabilising Fins AD/DHC-2/23 Amdt 1

Wing Strut Assembly Lower Attachment Fittings AD/DHC-2/24 Amdt 3

Horizontal Stabiliser Attachment Brackets AD/DHC-2/25

Passenger Seats and Passenger Seat Attachment Fittings AD/DHC-2/26

Horizontal Stabiliser Front Spar AD/DHC-2/27 Amdt 2

Wing Strut Lower Steel End-Fitting AD/DHC-2/28

Elevator Mass Balance Weight AD/DHC-2/29

Front Fuselage Struts at Windshield AD/DHC-2/30 Amdt 1

Fuselage Station 228 Bulkhead AD/DHC-2/31

Magneto Cannon Plug AD/DHC-2/32

Exhaust Collector Ring Segments AD/DHC-2/33

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.

1 Airworthiness Directives 2004 - Revocation and Remaking - DHC-2 (Beaver) Series Aeroplanes