What it does
Mechanically, this instrument is an amendment to an existing Civil Aviation Safety Authority (CASA) airworthiness directive concerning the nacelle strut attach pin/bolt, dual side brace, and underwing midspar fitting on specified Boeing 747 series aeroplanes. The directive requires operators to carry out the technical actions set out in FAA Airworthiness Directive (AD) 2005-19-09, Amendment 39-14274. The text explicitly authorises that corrective actions (repairs or repeat inspections) which are approved on an FAA form 8100-9 and which have been approved by the Manager, Seattle Aircraft Certification Office (ACO) or that Manager’s delegate as an Alternative Method of Compliance (AMOC) to FAA AD 2005-19-09, may be carried out by operators without the need to obtain an exclusion from CASA from this airworthiness directive [Requirement].
Applicability is limited to specific Boeing 747 models, as identified in Boeing Service Bulletin 747-54A2218 Revision 1 dated 24 February 2005, or later FAA-approved revision. The amendment becomes effective on 12 February 2009 and the original AD became effective on 24 November 2005 [Applicability; Compliance; This Amendment becomes effective on 12 February 2009; The original issue ... 24 November 2005].
The official rationale provided in the text is that the FAA received reports of corroded, migrated, and rotated bearings for dual side braces in inboard and outboard engine mounting struts, a fractured retainer for an eccentric bushing on a dual side brace side link, and wear and damage to the underwing midspar fitting on the outboard strut. The directive’s stated safety purpose is to prevent loss of a dual side brace or underwing midspar fitting load path, which could lead to load and motion transfer to other parts of a strut and potential separation of a strut and engine from the aircraft during flight [Background].