AD/BEECH 56/1 Amdt 2 - Rudder Spar and Hinges
1AD/BEECH 56/1 Amdt 2 - Rudder Spar and Hinges
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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 Beechcraft 56TC (Turbo Baron) Series Aeroplanes
AD/BEECH 56/1
Amdt 2
Rudder Spar and Hinges 5/68
Applicability: Model 56TC with S/Nos. TG-1 to TG-51.
Requirement: Action in accordance with Beechcraft SB 67-34, Rev. 1.
Compliance: Inspect for cracking within 100 hours’ time in service from 16 May 1968 and thereafter at intervals not exceeding 100 hours’ time in service until modified. Modify and inspect for alignment within 300 hours’ time in service from 16 May 1968.