AD/AMD 20/23 - Supplementary Structural Inspection Program
1AD/AMD 20/23 - Supplementary Structural Inspection Program
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text AMD Fan Jet Falcon (Falcon 20/Mystere-Falcon 200) Series Aeroplanes
AD/AMD 20/23 Supplementary Structural Inspection Program 10/91
Applicability: All models.
Requirement: Action in accordance with the Technical Requirements of DGAC AD 90-089-020 (B), dated 28 April 1990.
Note: Dassault Aviation Service Bulletin FJF/00/26 (DA/FJF/730), revision 1 dated 12 December 1990, refers.
Compliance: As specified in the Requirement Document with effective date 3 October 1991 for Australian registered aircraft.
Background: Compliance with the SSIP is required in order to extend the operating life of the airframe to the lesser of 40 000 flights or 60 000 flight hours.