Document ID: chunk:federal_register_of_legislation:F2006B10449:body:0:p2
Version: federal_register_of_legislation:F2006B10449
Segment Type: other
Provision Reference: 
Character Range: 2939–4575

in accordance with this Airworthiness Directive. Accomplishment of the actions specified in both Raytheon Service Bulletin SB 21-3377, Revision 1, dated July 2000; and Raytheon Service Bulletin SB 21-3414, Revision 1, dated July 2000, is terminating action for the requirements of this Airworthiness Directive.
 COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

            Note: FAA AD 2001-13-05 refers.

            Compliance: For Requirement 1 and 2: Within 100 hours time-in-service or, two months after the effective date of this Airworthiness Directive, whichever occurs first.

            This Airworthiness Directive becomes effective on 10 April 2002.

            Background: The manufacturer reported that air conditioning clamps and connecting sleeves that connect the water separator and turbine discharge duct have come loose. Should either of these ducts become disconnected, it will result in loss of air supply to maintain adequate cabin pressure. Loss of adequate cabin pressure at high altitude would require emergency procedures to be used, such as use of oxygen, auxiliary pressurisation, or emergency descent. This Airworthiness Directive therefore requires the replacement of existing clamps, bedding tapes and sleeves with new improved components that will prevent clamp slippage and subsequent duct disconnection.

 Eugene Paul Holzapfel
 Delegate of the Civil Aviation Safety Authority 28 March 2002

 The above AD is notified in the Commonwealth of Australia Gazette on 10 April 2002.