What it does
This instrument is an Airworthiness Directive (AD) issued by the Civil Aviation Safety Authority (CASA), identified as AD/BAe 146/141, State of Design Airworthiness Directives, number 18/2010. Mechanically, it does three things.
First, it requires operators and maintainers of British Aerospace BAe 146 and Avro 146-RJ aircraft, all series, to determine whether a set of United Kingdom Civil Aviation Authority (UK CAA) ADs listed in Table 1 are applicable to their aircraft. The Directive’s Requirement 1 states, “Determine the applicability of the UK CAA Airworthiness Directives (AD) listed in Table 1.” This is an affirmative obligation to undertake an applicability assessment against each listed AD.
Second, where an AD in Table 1 is applicable and has not already been accomplished, the operator or maintainer must perform the actions required by that UK CAA AD or by a later EASA-approved revision. The Directive’s Requirement 2 reads, “If it is determined that a UK CAA AD listed in Table 1 is applicable and has not been previously accomplished, perform the actions required by that AD or later EASA-approved revision.” That is, CASA makes compliance with the State of Design ADs mandatory for Australian-registered aircraft to the extent they apply.
Third, the Directive explicitly recognises EASA-approved Alternative Methods of Compliance (AMOC) in the form of service bulletins. It states, “Service Bulletins approved by EASA as Alternative Methods of Compliance (AMOC) to the ADs listed in Table 1 are considered acceptable for compliance with the equivalent requirements of this Airworthiness Directive.” Thus CASA permits EASA-sanctioned alternative technical solutions, rather than mandating strict verbatim adherence to each UK CAA AD text.
The Directive attaches Table 1, which lists a series of UK CAA AD reference numbers, the associated service bulletin references where supplied, and short titles describing the subject matter. Examples include ADs concerning bolts on the wing rear spar, inspection of spars for corrosion and cracking, inspection for micro-biological contamination, inspection of wing stringers for machining errors, ERMA terminals, elevator hinge bracket ribs, oxygen system pipe material, bleed air system housings, fire resistance coupling in the engine bay, and a range of other items. The instrument also includes a practical compliance schedule: if a certificate of airworthiness has not yet been issued for an aircraft, the required actions must be completed before issuing that certificate; if the certificate has been issued, the required actions must be completed before further flight after 60 days from the Directive’s effective date. The Directive records an effective date of 24 September 2010 and is signed on behalf of CASA by a delegate, Charles Lenarcic, dated 7 September 2010. Finally, the Background statement in the Directive records CASA’s view that the listed UK CAA ADs required once-only actions with compliance dates that had already passed, and that CASA issued the Directive to “ensure compliance with all State of Design ADs.” The Background also notes that some ADs may not be applicable to any aircraft presently registered in Australia because of manufacture date or configuration.