1Airworthiness Directives 2004 - Revocation and Remaking - Agusta A109 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.

Image unavailable in extracted text

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

Agusta A109 Series Helicopters

AD Name AD Number

Main Rotor Blade AD/A109/1 Amdt 3

Tail Rotor Blade Root Fitting AD/A109/2 Amdt 3

Passenger and Pilots Door Emergency Release Mechanism AD/A109/3 Amdt 1

Retirement Lives - Fatigue Critical Components - CANCELLED AD/A109/4 Amdt 3

MLG Actuator Bracket Assembly Attachment Bolts - CANCELLED AD/A109/5 Amdt 1

Swashplate Bearing AD/A109/6

Superflexit Fuel Tanks AD/A109/7

Tail Rotor Blades AD/A109/8 Amdt 1

Engine Mount Installation AD/A109/9

Nose Landing Gear Actuator AD/A109/10

Emergency Float Assembly P/N 109-0715-01 AD/A109/11

Main Landing Gear Stiffening Struts AD/A109/12

Electrical Connectors P/N MS3456W14S-5S AD/A109/13

Main Landing Gear Wheels AD/A109/14

Modification of Overhead Console Relay Boards AD/A109/15

Main Rotor Blades AD/A109/16 Amdt 3

Main Gearbox Gleason Crown Bolts AD/A109/17 Amdt 1

Upper Transmission Mount Fitting AD/A109/18 Amdt 3

Tail Rotor Hub AD/A109/19 Amdt 2

Main Rotor Hydraulic Actuators AD/A109/20

Aircruiser Emergency Floats AD/A109/21

Sliding Doors Emergency Exit Panel AD/A109/22

Tail Boom and Vertical Fin Modification AD/A109/23

Main Rotor Blade - Trailing Edge AD/A109/24

Main Rotor Pitch Change Link Spherical Bearing AD/A109/25 Amdt 1

Hydraulic System Return Line AD/A109/26

Tail Rotor Blades P/N 109-8132-01-107 AD/A109/27

Tail Rotor Blade Grip Assemblies AD/A109/28