Document ID: chunk:federal_register_of_legislation:F2006B07610:body:0
Version: federal_register_of_legislation:F2006B07610
Segment Type: other
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Character Range: 0–792

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Eagle X-TS Series Aeroplanes

AD/X-TS/3 Canard Rear Spar Reinforcement 2/2000 TX

 Applicability: Models X-TS 150 and 150B serial numbers 001 to 003 and 005 to 030 inclusive. Requirement:               Modify the canard rear spar bracket in accordance with Eagle Service Bulletin 1074. Compliance:               Within 100 hours time in service after the effective date of this directive.
            This Airworthiness Directive becomes effective on 24 December 1999.

            Background: This Directive is issued to provide additional strength to the canard rear spar bracket, to enable the aircraft to meet certification requirements.