Document ID: chunk:federal_register_of_legislation:F2006B07864:body:0:p1
Version: federal_register_of_legislation:F2006B07864
Segment Type: other
Provision Reference: 
Character Range: 1–3528

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

 Fairchild (Swearingen) SA226 and SA227 Series Aeroplanes

 AD Name AD Number

 Frame Splices - Inspection AD/SWSA226/1

 Stabiliser Skin Attachment Screws - Inspection - CANCELLED AD/SWSA226/2

 Superseded by DCA/SWSA226/17 - CANCELLED AD/SWSA226/3

 CANCELLED - Incorporated into AD/SWSA226/21 Amdt1 - CANCELLED AD/SWSA226/4 Amdt 1

 Wing Centre Section Improved Venting - Modification AD/SWSA226/5

 Trim Tab Actuator Rods - Inspection AD/SWSA226/6

 Fuel Line and Heat Shroud - Inspection AD/SWSA226/7

 Front (Pilot) Seat Restraint Installation - Modification AD/SWSA226/8

 Main Landing Gear Uplock Roller - Inspection and Modification AD/SWSA226/9

 Engine Windmilling Limits Placard - Installation AD/SWSA226/10

 Rudder - Inspection AD/SWSA226/11

 Rudder Bellcranks - Inspection AD/SWSA226/12

 Aileron Tab - Inspection and Modification AD/SWSA226/13

 Aileron Control System - Modification AD/SWSA226/14

 Main Landing Gear Door Hinge Angles - Inspection and Replacement AD/SWSA226/15

 Aileron Balance Weight Attachment Bolts - Inspection AD/SWSA226/16

 Wing - Modification and Fail Safe Structural Inspection - CANCELLED AD/SWSA226/17 Amdt 4

 Stabiliser Trim Disconnect Controls - Modification AD/SWSA226/18

 Horizontal Stabiliser Bar - Inspection - CANCELLED AD/SWSA226/19

 Horizontal Stabiliser Rear Spar - Inspection and Modification - CANCELLED AD/SWSA226/20

 Fuselage - Fail Safe Structural Inspection - CANCELLED AD/SWSA226/21 Amdt 1

 Elevator Quadrant - Inspection AD/SWSA226/22 Amdt 1

 Fuel and Hyraulic Lines Inspection AD/SWSA226/23

 Nose Wheel Steering - Deactivation AD/SWSA226/24

 Fuel Line - Inspection - CANCELLED AD/SWSA226/25

 Landing Gear Actuator Rod End AD/SWSA226/26 Amdt 1

 Wing Main Spar - Inspection for Manufacturing Defects AD/SWSA226/27

 Crew and Cargo Door Latch Assemblies/Receptacles - Life Limitation -  AD/SWSA226/28 Amdt 5

 Nose Baggage Compartment Door - Modification AD/SWSA226/29

 Cargo And Passenger Doors, Latching Mechanisms - Inspection - CANCELLED AD/SWSA226/30 Amdt 2

 Aileron Control Cable Installation - Inspection AD/SWSA226/31

 Rudder Pedal Links AD/SWSA226/32 Amdt 1

 Elevator Mass Balance Weights - Inspection AD/SWSA226/33

 Fuselage Skin and Aft Belly Fairing - Inspection AD/SWSA226/34

 Aileron Static Rebalance - Incorporation AD/SWSA226/35

 Elevator Return Spring And Attachment AD/SWSA226/36 Amdt 2

 Fuselage, Lower L.H. Cargo Area Belt Frames - Inspection and Modification AD/SWSA226/37

 Elevator Return Spring Location - Modification AD/SWSA226/38 Amdt 1

 Main Landing Gear Door Actuating Mechanism - Modification AD/SWSA226/39

 Prohibition of Flight into Known Icing Conditions - Placard AD/SWSA226/40

 Flight Control, Control Column - Modification AD/SWSA226/41

 Prohibition of Flight into Known Icing Conditions - Placard AD/SWSA226/42