Airworthiness Directives 2004 - Revocation and Remaking - Dhc-3 (Otter) Series Aeroplanes (Cth)
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
DHC-3 (Otter) Series Aeroplanes
AD Name AD Number
Rudder Quadrant, Rudder Pedal Linkage, Tail Wheel Assembly and Rear AD/DHC-3/1
Rear Cargo Door AD/DHC-3/2
Main Undercarriage Compression Strut AD/DHC-3/3
Cargo Door Handles AD/DHC-3/4
Booster Pump, Fuselage Former Cap Strips, Rear Cabin Seats AD/DHC-3/5
Rudder Control AD/DHC-3/6
Engine Breather Drain Box AD/DHC-3/7
With Skin Riveting and Flap Hydraulic System AD/DHC-3/8
Tailplane Trim Indicator AD/DHC-3/9
Exhaust System AD/DHC-3/10
Elevator Quadrant, Inboard Nose Flaps, Empennage, Aileron Centre Hinge AD/DHC-3/11
Flap Hydraulic Jack AD/DHC-3/12
Propeller Counterweight Bearing Shafts AD/DHC-3/13
Tailplane Fork Attachment Fitting AD/DHC-3/14
Engine Driven Fuel Pump AD/DHC-3/15
Flap Control Rod Sub-Assembly AD/DHC-3/16
Engine Cooling AD/DHC-3/17
Wing Strut Spar AD/DHC-3/18
Fuel Line Chafing AD/DHC-3/19
Mixture Control Lever Quadrant AD/DHC-3/20
Rudder Pedal Support AD/DHC-3/21
Elevator Tab Control Arm AD/DHC-3/22
VNE Placard AD/DHC-3/23
Main Landing Gear Fuselage Attachment Bolts AD/DHC-3/24
Wing Strut and Attachments - Retirement Lives AD/DHC-3/25
Tailplane Hinge Bolts AD/DHC-3/26
Front Seat Restraint Installation AD/DHC-3/27
Front Fuselage - Windshield Post AD/DHC-3/28
Engine Mounting Frame AD/DHC-3/29
Elevator Connecting Rod AD/DHC-3/30
Control Column Cracking AD/DHC-3/31
Utility Seat Forward Leg Positive Lock Installation AD/DHC-3/32 Amdt 1
Wing Strut to Fuselage Tie Bar AD/DHC-3/33
Tailplane Main Rib Forward Flange and Forward Lower Flange AD/DHC-3/34 Amdt 1
Electrical System AD/DHC-3/35
Fire Detection and Extinguishing System AD/DHC-3/36
Magneto Cannon Plug AD/DHC-3/37
Electrically Heated Engine Pneumatic Lines AD/DHC-3/38
Elevator Servo Tab AD/DHC-3/39
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