COMMONWEALTH OF AUSTRALIA (Civil Aviation Safety Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
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 39.1 (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 717 Series Aeroplanes
AD/B717/11 Safe-Life Structure and Principal Structural
Elements
11/2003
Applicability: All Model 717-200 aircraft.
Requirement: Action in accordance with the technical requirements if FAA AD 2003-17-01 Amdt.
39-13274.
Note: Boeing Report No. MDC-96K9063 Revision 3 refers.
Compliance: Within 180 days after 30 October 2003, unless already accomplished. This Airworthiness Directive becomes effective on 30 October 2003.
Background: The FAA requires a revision of the Airworthiness Limitations Section of the Instructions for Continued Airworthiness to incorporate new removal limits for certain components of the flap system and to reduce the interval of inspections for fatigue cracking of certain principal structural elements.
David Villiers
Delegate of the Civil Aviation Safety Authority 10 September 2003
The above AD is notified in the Commonwealth of Australia Gazette on 8 October 2003.
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