Document ID: chunk:federal_register_of_legislation:F2006B10453:body:0:p2
Version: federal_register_of_legislation:F2006B10453
Segment Type: other
Provision Reference: 
Character Range: 2967–5069

those locations identified in the original service bulletin; Revision 1 requires inspections at additional locations.

 British Aerospace BAe 125 Series Aeroplanes

 AD/HS 125/170 (continued)

5.        For Model Hawker 800 aircraft identified as Group C aircraft in Raytheon Service Bulletin SB 51-3421, Revision 1, dated November 2001, including Appendix 1, dated December 2000, excluding Service Bulletin/Kit Drawing Report Fax: Inspect in accordance with above referenced service bulletin. Inspection before the effective date of this Directive in accordance with the original issue of above referenced service bulletin, including Appendix 1, is acceptable for compliance with the inspection requirement only for those locations identified in the original service bulletin; Revision 1 requires inspections at additional locations.

           For any discrepant bolt (any Ravenstone Jackson DHS bolt or any bolt that cannot be identified) found during any inspection required by this Directive, before further flight, perform an ultrasonic inspection to determine if the bolt is broken. Replace any broken bolt with a new bolt before further flight, in accordance with the applicable service bulletin.

           Note: FAA AD 2003-06-06 Amdt 39-13093 refers.

 Compliance: 1. Within 12 months after 10 July 2003.

2.        Within 18 months after 10 July 2003.

3.        Within 12 months after 10 July 2003.

4.        Within 18 months after 10 July 2003.

5.        Within 12 months after 10 July 2003.

           This Airworthiness Directive becomes effective on 10 July 2003.

           Background: This Directive requires a one-time inspection to identify the bolts installed at certain locations in the wing or fuselage. The actions required by this Directive are intended to prevent failure of certain attachment bolts due to manufacturing discrepancies, whic h could result in reduced structural integrity of the aircraft.

 David Villiers
 Delegate of the Civil Aviation Safety Authority 9 May 2003

 The above AD is notified in the Commonwealth of Australia Gazette on 18 June 2003.