Document ID: chunk:federal_register_of_legislation:F2006B07872:body:0:p1
Version: federal_register_of_legislation:F2006B07872
Segment Type: other
Provision Reference: 
Character Range: 1–3389

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

 Fokker F50 (F27 Mk 50) Series Aeroplanes

 AD Name AD Number

 Central Windshield Post Connection to Pressure Bulkhead AD/F50/1

 Aircraft Flight Manual and Minimum Equipment List Amendment AD/F50/2

 Wing Structure - Skin Splice WS 7915 AD/F50/3 Amdt 1

 Fire Sensing Element (Fire Wire) Bonding AD/F50/4

 Cabin Pressure Control System AD/F50/5

 Control Cables in Accessory Compartment AD/F50/6

 Dorsal Fin Gutter AD/F50/7

 Passenger Entrance Door Coamings AD/F50/8

 Door External Handles AD/F50/9

 Outboard Nacelle Ventilation Air Inlets AD/F50/10

 Wing Centre Section Cable Tray Blanking Plate AD/F50/11

 Engine Anti-Ice Control Unit AD/F50/12

 Accessory Bay Ventilation Air Outlet AD/F50/13

 Outer Wing End Rib Access Panel AD/F50/14 Amdt 1

 Engine Air Intake Seal AD/F50/15

 Flap Power Drive Unit AD/F50/16 Amdt 1

 Fuel Collector Tank Supply Line AD/F50/17

 Door Mechanism Gearbox Cover AD/F50/18

 Engine Controls AD/F50/19

 Engine Tailpipe Assembly AD/F50/20 Amdt 1

 Forward Fuselage - Stringers and Frame 5775 AD/F50/21

 Elevator Trim Cable Pulley Bracket and Mounting AD/F50/22

 Elevator Control Rod Ends AD/F50/23

 Engine Control Rod Clearance AD/F50/24

 Radio Magnetic Indicators Wiring Change AD/F50/25

 Forward Passenger Door Frame to Torsion Box Connection AD/F50/26 Amdt 1

 Windshield - Post Link Support Bracket- Forward Pressure Bulkhead AD/F50/27

 Stringer 18 Between Stations 4875 and 5325 AD/F50/28

 Elevator and Tab Pulley Bracket - Frame 3100 AD/F50/29

 Fuselage Upper Girder Connection at Frame Sta. 3415 AD/F50/30

 Accessory Compartment Cable Covers AD/F50/31

 Electrical Power - Terminal Block and Contactor Torque Values AD/F50/32 Amdt 1

 Landing Gear - Extension/Retraction Control AD/F50/33 Amdt 1

 Electrical Power - AC Emergency Inverter AD/F50/34

 Emergency Inverter Circuitry - CANCELLED AD/F50/35

 Alternate Brake System Cables AD/F50/36

 Auto Flight Idle Stop Mechanism AD/F50/37

 Auto Flight Idle Stop Mechanism Modification AD/F50/38

 Elevator Torque Tube Bearing Plate Bolts AD/F50/39

 Fire Wire Connector Replacement AD/F50/40

 Outboard Flap Drive AD/F50/41

 External Power Connection Relay Fitment AD/F50/42 Amdt 1

 Fuselage - Flight Compartment Window Frames -1 AD/F50/43

 Fuselage - Flight Compartment Window Frames -2 AD/F50/44

 Fuselage Power Supply Box Surround Structure AD/F50/45

 Forward Fuselage Skin Dimples AD/F50/46

 Nose Landing Gear Retraction Mechanism AD/F50/47

 RH Nacelle Aft Cone Fairing Fork-End Assemblies AD/F50/48

 Windshield Wiper Rotary Selector Switch Replacement AD/F50/49

 Windshield Wiper System AD/F50/50

 Auto Feather Control Unit AD/F50/51

 Cockpit Window Post Attach Angles