COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Bell Helicopter Textron 204 Series Helicopters
AIRWORTHINESS DIRECTIVE
For the reasons set out in the background section, the CASA delegate whose signature appears below revokes Airworthiness Directive (AD) AD/BELL 204/22 and issues the following AD under subregulation 39.1 (1) of CAR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.
AD/BELL 204/22
Amdt 1
Main Rotor Blades Removal From Service 8/2000
Applicability: All Models.
Requirement: The main rotor blades with the serial numbers listed below are to be removed from service.
A2-03642 | A2-03643 | A2-03646 | A2-27872 | A2-27961 |
A2-27963 | A2-27967 | A2-27968 | A-27982 | A2-28015 |
A2-28016 | A2-28019 | A2-28020 | A2-28023 | A2-28195 |
A2-28198 | A2-28211 | A2-29315 | A2-29325 |
|
A2-29334 | A2-29915 | A2-29919 | A2-29920 |
|
Note: FAA AD 76-02-06 refers.
Compliance: Before further flight after 16 January 1976.
This Amendment becomes effective on 10 August 2000.
Background: This directive was issued initially to remove certain MR blades from service.
Amendment 1 is issued to reference the country of manufacture AD. It also follows the re-introduction of the AD Series after sixteen years.
The original issue of this Airworthiness Directive became effective on 16 January 1976.
David Alan Villiers
Delegate of the Civil Aviation Safety Authority 6 July 2000
The above AD is notified in the Commonwealth of Australia Gazette on 12 July 2000.