Commonwealth legislation

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

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This instrument, signed by a CASA delegate under subregulation 39.001(1), revokes a set of Airworthiness Directives (ADs) for Brantly B‑2 helicopters and re‑issues each AD as a separate instrument in the identical form of the latest published versions. It affects owners, operators and maintenance providers for Brantly B‑2 helicopters, who must continue to comply with those ADs. The delegate (CASA) decides the administrative reissue; operators bear compliance, inspection and record‑keeping costs imposed by the remade ADs.

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

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.

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Superseded by AD/B-2/23 AD/B-2/15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

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.

1 Airworthiness Directives 2004 - Revocation and Remaking - Brantly B-2 Series Helicopters