AD/X-TS/3 - Canard Rear Spar Reinforcement
1AD/X-TS/3 - Canard Rear Spar Reinforcement
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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 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.