AD/HS 748/17 - Engine Subframe Eye Bolt

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B10551 In force Legislative Instrument

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


British Aerospace (Hawker Siddeley) HS 748 Series Aeroplanes

 

AD/HS 748/17 Engine Subframe Eye Bolt 5/95

Applicability: All HS748 Aircraft.

 

Requirement: 1. On both left and right engine subframe assemblies inspect the installation of the eye bolt (P/N 14b.0.3975) into the “Y” plate (P/N 14a.0.3975) in accordance with British Aerospace Mandatory Service Bulletin (MSB) 54/31.

 

2. Rectify any deficient eye bolt installations in accordance with British Aerospace MSB 54/31.

 

Note: CAA (UK) AD 009-08-88 refers.

 

Compliance: 1. Inspect before 11 May 1995.

 

2. Rectify, if required, within 60 days of the Requirement 1 inspection.

 

Background: An in-service failure of an eye bolt revealed the possibility of incorrect bedding of the eye bolt head to the sub-frame “Y” plate.

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.