Document ID: chunk:federal_register_of_legislation:F2006B11164:body:0:p2
Version: federal_register_of_legislation:F2006B11164
Segment Type: other
Provision Reference: 
Character Range: 2956–4172

for the requirements of Item 1 of requirements.

            Note 3: Compliance with Bombardier (Learjet) Service Bulletin (SB) A45-30-2 is terminating action for this Directive.

 Compliance: Effective 13 June 2002.

               1. Prior to 15 June 2002.

              2.        Within 25 hours Time in Service (TIS) from the effective date of this Directive.

              3.         Within 25 hours Time in Service (TIS) from the effective date of this Directive.

            4.        Within 25 hours Time in Service (TIS) from the effective date of this Directive. This Airworthiness Directive becomes effective on 13 June 2002.
            Background: Failure of the splitter contained with the anti-ice manifold has led to blocking of the anti-ice system ducts. This degrades the anti-ice capacity of the aeroplane. This Directive introduces a temporary flight manual change to not allow operation of the aeroplane in icing conditions until replacement of the manifold and a check of the anti-ice system ducts for blockage is carried out.

 James Coyne
 Delegate of the Civil Aviation Safety Authority 3 May 2002

 The above AD is notified in the Commonwealth of Australia Gazette on 22 May 2002.