Document ID: chunk:federal_register_of_legislation:F2006B03149:body:0:p2
Version: federal_register_of_legislation:F2006B03149
Segment Type: other
Provision Reference: 
Character Range: 2985–4280

repetitive inspections and functional tests required by Requirement 1 of AD/B747/277.

              Accomplishment of the requirements of this Directive is also terminating action for the repetitive inspections and functional tests required by Requirement 1 of AD/B747/277.

           Note: FAA AD 2001-12-21 Amendment 39-11799, and 94-15-05 Amendment 39-8976 refer.

           Compliance:  For Requirement 1: Prior to issue of Certificate of Airworthiness. For Requirement 2: Prior to issue of Certificate of Airworthiness. For Requirement 3: Prior to further flight.
           For Requirement 4: At intervals not exceeding 4000 hours time- in-service. This Amendment becomes effective on 5 September 2002.
           Background: This amendment includes a number of editorial and technical changes to better represent the requirements of FAA AD 2000-12-21. This Directive was issued to prevent inadvertent deployment of the thrust reverser during flight and consequent reduced controllability of the aeroplane.

           The original issue of this Airworthiness Directive became effective on 9 August 2001.

 Eugene Paul Holzapfel
 Delegate of the Civil Aviation Safety Authority 25 July 2002

 The above AD is notified in the Commonwealth of Australia Gazette on 14 August 2002.