Document ID: chunk:federal_register_of_legislation:F2006B03129:body:0:p2
Version: federal_register_of_legislation:F2006B03129
Segment Type: other
Provision Reference: 
Character Range: 3014–5616

in Appendix 1 of FAA AD 2000-02-22, or if any discrepancy is detected during any operational check, repair in accordance with procedures specified in approved maintenance data.

5.        Repeat Requirement 3 operational checks if any discrepancies have been corrected under Requirement 4 during compliance with Requirement 3 or 6.

6.        Repeat and successfully accomplish operational checks required by Requirement 3.

                               Terminating Action

              Accomplishment of Requirement 1 and 2, or installation of an additional locking system during production in accordance with production equivalent PRR 81000- 39, is terminating action for the inspections and tests required by Requirement 3 of AD/B747/277.

           Note: FAA AD 2000-02-22 Amendment 39-11540 refers.

           Compliance: For Requirement 1: Within 36 months time in service from 13 July 2000 (the effective date of original issue of this Directive).

           For Requirement 2: Prior to or concurrent with Requirement 1 compliance.

           For Requirement 3: Within 3,000 flight hours after accomplishment of Requirement 1 or within 1,000 flight hours from 13 July 2000 (the effective date of original issue of this Directive), whichever occurred later.

           For Requirement 4: Prior to further flight. For Requirement 5: Prior to further flight.
           For Requirement 6: At intervals not exceeding 3,000 flight hours time in service. This Amendment becomes effective on 5 September 2002.

Boeing 747 Series Aeroplanes

 AD/B747/230 Amdt 1 (continued)

           Background: This amendment introduces a requirement to repeat operational checks after maintenance, and terminating action for part of AD/B747/277. This Directive was issued after a safety review revealed that in- flight deployment of a thrust reverser could result in significant reduction of aircraft controllability. Therefore this Directive includes actions to ensure the integrity of the fail safe features of the thrust reverser system is maintained by preventing failure modes which could result in inadvertent deployment of a thrust reverser during flight. This amendment does not add aircraft or require more work on aircraft modified in accordance with the original issue of the service bulletin.

           The original issue of this Airworthiness Directive became effective on 13 July 2000.

 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.