Document ID: chunk:federal_register_of_legislation:F2006B03279:body:0
Version: federal_register_of_legislation:F2006B03279
Segment Type: other
Provision Reference: 
Character Range: 0–1009

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Boeing 767 Series Aeroplanes

 AD/B767/1
 Amdt 1

 Fuel Quantity System - Inspection 12/83

 Applicability: All models equipped with FQIS processor P/N. S345T002-41. Document:  Boeing Alert Service Bulletin 767-28A5 Rev. 2.
            Note: FAA AD 83-15-05 AMDT. 39-4696 refers.

 Compliance: Unless already accomplished, initial inspection on or before 31st December 1983.
            Subsequent inspections as per requirement document.

            Note: Compliance with the original issue of this directive does not constitute compliance with this AD/B767/1 AMDT 1.

            Background: To prevent loss of engine power due to fuel exhaustion resulting from erroneous fuel quantity indication. This directive is raised in issue to include the latest revision status of Boeing S.B. 767-28A5 which modifies certain aspects of the inspection procedure.