Document ID: chunk:federal_register_of_legislation:F2006B07775:body:0
Version: federal_register_of_legislation:F2006B07775
Segment Type: other
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Character Range: 0–2422

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

 Brantly B-2 Series Helicopters

 AD Name AD Number

 Tail Rotor Guard and Skid Assembly P/N B2-416 - Modification AD/B-2/1

 Tail Rotor Drive - Modification AD/B-2/2

 Tail Rotor Drive - Inspection AD/B-2/3

 Tail Rotor Drive - Modification AD/B-2/4

 Tail Cone Reinforcement AD/B-2/5

 Overunning Clutch - Modification and Cockpit Placard Amendment AD/B-2/6

 Main Rotor Blade Dampers - Installation AD/B-2/7

 Tail Cone Reinforcement AD/B-2/8

 Main Transmission Mount - Reinforcement AD/B-2/9

 Rotor Blade Hinge - Modification AD/B-2/10

 Tail Rotor Blade Retaining Nut - Safetying AD/B-2/11

 Main Transmission Forward Mount - Rework AD/B-2/12

 Tail Rotor Guard - Inspection AD/B-2/13

 Rod End Bearings (Old Type KAHR. HE3SFN) on Forward End of U/C Drag  AD/B-2/14

 Superseded by AD/B-2/23 AD/B-2/15

 Centrifugal Clutch - Inspection Cockpit Placard - Installation AD/B-2/16

 Elimination of Carburettor Manifold From Oil System AD/B-2/17

 Seat Safety Bracket - Installation AD/B-2/18

 Transmission Mount Lugs - Reinforcement AD/B-2/19

 Increased Tail Rotor Control - Modification AD/B-2/20

 Conversion of Fuel Pump Model RD 7790D3 and E to G AD/B-2/21

 Seat Back Adjustment Wire - Removal AD/B-2/22

 Main Rotor Blades - Inspection and Replacement AD/B-2/23

 Rudder Control Post Upper Attachment - Modification AD/B-2/24

 Tail Rotor Blade - Inspection AD/B-2/25

 Main Rotor Mast Upper Bearing - Replacement AD/B-2/26

 Tail Rotor Blades Strike Indicators - Installation AD/B-2/27

 Tail Rotor Blade Spar - Inspection AD/B-2/28 Amdt 1

 Tail Rotor Drive Shaft - Inspection and Corrosion Proofing AD/B-2/29 Amdt 1

 Retirement Life - Critical Components AD/B-2/30 Amdt 3

 Main Rotor Mast - Inspection AD/B-2/31