Airworthiness Directives 2004 - Revocation and Remaking - Brantly B-2 Series Helicopters (Cth)

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Superseded by AD/B-2/23  AD/B-2/15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