What it does
Mechanically, this Airworthiness Directive (AD/CF6/78, reference 21/2010) makes the United States Federal Aviation Administration (FAA) Airworthiness Directives listed in Table 1 of the instrument an enforceable compliance obligation for General Electric CF6 series engines on aircraft on the Australian register, subject to an applicability determination. The Directive requires two discrete acts by the responsible person or organisation: first, determine whether each FAA AD listed in Table 1 applies to the particular engine/airframe combination; second, if an FAA AD in Table 1 is applicable and has not previously been accomplished, perform the actions required by that FAA AD. The Directive accepts Service Bulletins that have been approved by the FAA as Alternative Methods of Compliance (AMOC) to the listed FAA ADs as acceptable means of compliance with the equivalent requirements of the CASA Directive.
The Directive lists four FAA ADs in Table 1 with their effective dates and titles: 90-12-06 (25/06/1990) , Low Pressure Turbine; 96-16-07 (28/08/1996) , Rear Right Hand Mount Link; 2005-26-06 (26/01/2006) , Low Pressure Turbine (LPT) stage 2 interstage seal assemblies; and 2007-21-06 (15/11/2007) , Electronic Control Unit (ECU). The Directive becomes effective 8 November 2010 and states compliance timings: if a certificate of airworthiness has not yet been issued for the aircraft, compliance must occur before issue of the certificate; if a certificate has issued, compliance must occur before further flight after 8 November 2010. The Directive also advises where to access FAA ADs (Note 1: http://rgl.faa.gov) and contains a background paragraph stating CASA’s view that the listed FAA ADs require once-only actions with past compliance dates and may be applicable when an aircraft enters the Australian register.
The instrument’s stated objective, in CASA’s words, is to "ensure compliance with all State of Design ADs." That stated purpose appears in the background paragraph. The Directive operationalises that objective by directly importing a set of State-of-Design (FAA) ADs into an Australian regulatory requirement for CF6 engines, subject to applicability analysis, and by recognising FAA-approved AMOCs as acceptable compliance methods. The text explicitly acknowledges that, due to date of manufacture or configuration and modification status, some of the FAA ADs may not be applicable to particular aircraft on the Australian register.