Document ID: chunk:federal_register_of_legislation:F2006B07740:body:0:p1
Version: federal_register_of_legislation:F2006B07740
Segment Type: other
Provision Reference: 
Character Range: 1–3168

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

 Beechcraft 200 (Super King Air) Series Aeroplanes

 AD Name AD Number

 Strobe Light Bonding Straps AD/BEECH 200/1

 Flap Gearbox AD/BEECH 200/2

 Propeller Secondary Low Pitch Stop System AD/BEECH 200/3 Amdt 1

 Nacelle Fuel Vent Float Valve AD/BEECH 200/4

 Generator Leads AD/BEECH 200/5

 Wing Tip Fuel Filler Anti-Siphon Door Assembly AD/BEECH 200/6

 Rudder Push Rod Assembly AD/BEECH 200/7

 Seat Locking Pins AD/BEECH 200/8

 Cabin Door Instruction Plate - CANCELLED AD/BEECH 200/9

 Wing Deicer Lines AD/BEECH 200/10

 DC Power Panel Harness AD/BEECH 200/11

 Vertical Stabiliser AD/BEECH 200/12 Amdt 2

 Aft Cowling Door Forward Latch Pin AD/BEECH 200/13 Amdt 1

 Fuselage Structure - CANCELLED AD/BEECH 200/14

 Aileron Control System AD/BEECH 200/15

 Rudder Control System AD/BEECH 200/16

 Nacelle Wheel Well Fender Installation AD/BEECH 200/17

 Aft Wing Spar and Lower Cabin Structure - CANCELLED AD/BEECH 200/18

 Main Landing Gear Torque Tubes AD/BEECH 200/19

 Cabin Door Pins - Fatigue Life Limitation AD/BEECH 200/20 Amdt 3

 Fuselage Fatigue Life Limitation AD/BEECH 200/21 Amdt 11

 Cabin Door Latch Hooks and Lock Pins - CANCELLED AD/BEECH 200/22 Amdt 1

 Inboard Aileron Hinge Arms AD/BEECH 200/23 Amdt 1

 Fuselage Clip Installation AD/BEECH 200/24

 Flap Safety Switch Linkage AD/BEECH 200/25

 Flight Controls AD/BEECH 200/26 Amdt 1

 Engine Hose Assembly AD/BEECH 200/27

 Forward R.H. Cabin Service Panel Retainer AD/BEECH 200/28

 Fuselage Avionics Compartment Floor AD/BEECH 200/29 Amdt 1

 Wing Panel to Centre Section, Attach Fittings, Bolts and Nuts AD/BEECH 200/30 Amdt 3

 Elevator Control Horn Attachment AD/BEECH 200/31 Amdt 1

 Left Hand Rudder Cable Installation AD/BEECH 200/32

 Pilot and Co-Pilot Seat Back Pan AD/BEECH 200/33

 Oxygen System AD/BEECH 200/34

 Wing Fatigue Life Limitation AD/BEECH 200/35 Amdt 6

 Horizontal Stabiliser Forward Spar Web Rivets AD/BEECH 200/36 Amdt 1

 Nacelle Fuel Tank Probe AD/BEECH 200/37

 Wing Front Spars AD/BEECH 200/38 Amdt 4

 Outboard Wing Attachment Bolts and Nuts - CANCELLED AD/BEECH 200/39 Amdt 4

 Fuselage Windows - CANCELLED AD/BEECH 200/40

 Fuel Boost Pumps AD/BEECH 200/41 Amdt 2

 Engine Fuel Drain Connections AD/BEECH 200/42 Amdt 1

 Centre Section Upper Wing Skins AD/BEECH 200/43 Amdt 5

 Rear Fuselage, Stabilisers and Fin Sealing and Draining AD/BEECH 200/44 Amdt 1

 Nose Gear Lower Shock Absorber Assembly AD/BEECH 200/45 Amdt 2

 Elevator Trim Tab System AD/BEECH