AD/B747/398 State of Design Airworthiness Directives 1 (Cth)
AIRWORTHINESS DIRECTIVE
For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.001(1) of CASR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.
Boeing 747 Series Aeroplanes
| AD/B747/398 | State of Design Airworthiness Directives - 1 | 14/2009 |
Applicability: | Boeing 747-400 aircraft and 747 aircraft with General Electric CF6-80 or Rolls-Royce engines. | ||
Requirement: | 1. Determine the applicability of the FAA Airworthiness Directives (AD) listed in Table 1. | ||
| 2. If it is determined that an FAA AD listed in Table 1 is applicable and has not been previously accomplished, perform the actions required by that AD or later FAA-approved revision. | |||
| Table 1 | |||
FAA AD | Effective Date | Title | |
2007-04-10 | 23 March 2007 | Decompression panels | |
2005-05-20 | 17 April 2006 | Flight-deck door electronic equipment | |
2002-23-15 | 11 December 2002 | Lower lobe panel | |
2000-11-08 | 6 July 2000 | Fuel nozzles | |
96-11-03 | 26 June 1996 | Fuel line | |
96-08-05 | 23 May 1996 | Strut fuel tubes and couplings | |
96-03-10 | 20 February 1996 | Forward engine strut | |
95-13-06 | 28 July 1995 | Nacelle strut and wing structure | |
95-02-13 | 17 March 1995 | Fire extinguishers in engine nacelles | |
94-22-08 | 15 December 1994 | Engine strut skin | |
93-18-07 | 3 November 1993 | Fire extinguisher discharge tubes | |
92-14-07 | 20 August 1992 | Fire extinguisher tubes | |
92-13-08 | 5 August 1992 | Drain masts | |
| FAA AD | Effective Date | Title | |
| 92-06-01 | 13 April 1992 | Fuel tubes | |
| 92-04-05 | 26 March 1992 | APU pneumatic duct restraint | |
| 91-13-11 | 22 July 1991 | Wire bundles | |
| Note 1: FAA ADs may be accessed via the internet at the following URL:
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Compliance: | If a certificate of airworthiness has not been issued for the aircraft - before issue of the certificate of airworthiness. If a certificate of airworthiness has been issued for the aircraft – before further flight after 60 days from the effective date of this Directive. | ||
| This Airworthiness Directive becomes effective on 30 July 2010. | |||
Background: | The FAA ADs listed in Table 1 of this Directive require once-only actions for which the compliance date has passed. CASA has determined that these ADs may be applicable to some Australian aircraft. This Directive is issued to ensure compliance with all State of Design ADs. | ||
| CASA appreciates that, due to date of aircraft manufacture or aircraft configuration and modification status, some of the ADs listed in Table 1 will not be applicable to any aircraft presently registered in Australia. | |||
David Punshon
Delegate of the Civil Aviation Safety Authority
14 July 2010
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