Document ID: chunk:federal_register_of_legislation:F2006B02912:body:0:p2
Version: federal_register_of_legislation:F2006B02912
Segment Type: other
Provision Reference: 
Character Range: 2934–4727

be installed:

5.         Hydraulic accumulators with P/N's referred to in Requirements 2 and 4 may not be installed on any aircraft as a replacement part.

            Alternative Means of Compliance:

            Inspections and replacements accomplished before the effective date of this Directive per BSASB 737-32-1334, dated 11 May 2000, are considered acceptable for compliance with the corresponding actions required by Requirements 1 and 2.

            Inspections and replacements accomplished before the effective date of this Directive per BSASB 737-78-1068, dated 8 June 2000, are considered acceptable for compliance with the corresponding action required by Requirements 3 and 4.

            Note 3: FAA AD 2003-11-03 Amdt 39-13162 refers.

            Compliance: For Requirements 1, 2, 3 and 4: Within 18 months or prior to exceeding 6,000 flight hours from the effective date of this Directive, whichever occurs sooner.

            For Requirement 5: From the effective date of this Directive.

            This Airworthiness Directive becomes effective on 4 September 2003.

            Background: This Directive requires one-time inspections to determine the part numbers of hydraulic accumulators installed in various areas of the aeroplane and follow-on corrective actions as necessary. These actions are intended to prevent high-velocity separation of a barrel, piston or end cap from a hydraulic accumulator. Such separation could result in injury to personnel, loss of cabin pressurisation, loss of affected hydraulic systems or damage to plumbing, electrical installations or structural members.

 Jim Coyne
 Delegate of the Civil Aviation Safety Authority 25 July 2003

 The above AD is notified in the Commonwealth of Australia Gazette on 13 August 2003.