Document ID: chunk:federal_register_of_legislation:F2006B07711:body:0:p1
Version: federal_register_of_legislation:F2006B07711
Segment Type: other
Provision Reference: 
Character Range: 1–3476

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

 Airparts (NZ) Ltd. FU 24 Series Aeroplanes

 AD Name AD Number

 Elevator Control Cables and Pulleys - Inspection AD/FU24/1 Amdt 2

 Structural Component - Corrosion - Inspection AD/FU24/2 Amdt 1

 CANCELLED AD/FU24/3

 Elevator Balance Horn Attachment - Modification - CANCELLED AD/FU24/4

 Elevator Trim Tab Brackets - Modification AD/FU24/5

 Elevator Lower Pulley Station 337 - 340 - Modification - CANCELLED AD/FU24/6

 Wing Spar - Inspection - CANCELLED AD/FU24/7 Amdt 2

 Aileron Rib Assembly - Modification - CANCELLED AD/FU24/8

 Auxiliary Fuel Pump Switch - Modification - CANCELLED AD/FU24/9

 Fuel Sump Corrosion - Inspection AD/FU24/10

 Fin Rib and Skin Cracking - Inspection AD/FU24/11

 Rudder Lowr Rib - Inspection AD/FU24/12

 Fuel Tank Vent System - Modification - CANCELLED AD/FU24/13

 Hopper and Spray Tank Installation - Modification AD/FU24/14

 Main Landing Gear Axle Socket - Inspection AD/FU24/15

 Rudder Top Hinge Rivnuts - Modification - CANCELLED AD/FU24/16

 Aileron Mass Balance Arms - Modification AD/FU24/17

 Fuselage Skin Panels - Inspection - CANCELLED AD/FU24/18

 Engine Mounts and Firewalls AD/FU24/19

 CANCELLED AD/FU24/20

 CANCELLED AD/FU24/21

 CANCELLED AD/FU24/22

 CANCELLED AD/FU24/23

 CANCELLED AD/FU24/24

 CANCELLED AD/FU24/25

 CANCELLED AD/FU24/26

 CANCELLED AD/FU24/27

 CANCELLED AD/FU24/28

 CANCELLED AD/FU24/29

 CANCELLED AD/FU24/30

 Elevator Hinge and Attachment Fittings AD/FU24/31 Amdt 1

 CANCELLED AD/FU24/32

 CANCELLED AD/FU24/33

 CANCELLED AD/FU24/34

 CANCELLED AD/FU24/35

 Fuselage Structure - Modification AD/FU24/36

 Elevator Horn Assembly - Inspection AD/FU24/37

 Main Landing Gear Lower Torque Link - Modification AD/FU24/38

 Cleveland Wheel and Brake Assembly - Inspection AD/FU24/39

 Cockpit Ventilators - Modification AD/FU24/40

 Pilot Restraint Installation - Modification AD/FU24/41

 Installation of No Step Placard AD/FU24/42

 Installation of Crash Axes AD/FU24/43

 Part 1. Wing Spar Modification, and Part 2. Wing Spar Inspection AD/FU24/44

 Fuel Quantity Indication - Modification AD/FU24/45

 Brake Torque Plates - Inspection and Modification AD/FU24/46

 Cockpit Bulkhead - Modification AD/FU24/47

 Tailplane Mass Balance Weight and Control Horn - Inspection and Modification AD/FU24/48

 Centre Wing, Outboard Rear Fitting - Inspection and Modification AD/FU24/49

 Control Column Grip - Inspection AD/FU24/50

 Fin Forward Attachment Fitting AD/FU24/51 Amdt 2

 Fuel Line - Modification AD/FU24/52

 Flap Control Torque Tube - Inspection AD/FU24/53 Amdt 1

 L.H. Rudder Pedal - Inspection AD/FU24/54

 Oil Pressure Gauge Line - Fitment of Restrictor AD/FU24/55

 Engine Controls - Inspection and Modification AD/FU24/56

 Shoulder Harness Inertia Reel Installation Tension Clip