Commonwealth legislation

AD/B767/1 Amdt 1 - Fuel Quantity System - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

4/10 complexity

This directive requires operators of Boeing 767s fitted with FQIS processor P/N S345T002-41 to carry out an initial inspection by 31 December 1983 (if not already done) and recurring inspections per Boeing Alert Service Bulletin 767-28A5 Rev. 2, which the AD incorporates. Operators fund and arrange inspections/repairs. The measure, superseding earlier compliance, aims to prevent engine power loss from erroneous fuel quantity indications.

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Current sections

Direct links to the current provisions in AD/B767/1 Amdt 1 - Fuel Quantity System - Inspection.

AD/B767/1 Amdt 1 - Fuel Quantity System - Inspection

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

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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.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.

1 AD/B767/1 Amdt 1 - Fuel Quantity System - Inspection