AD/SD3-60/3 - Elevator Tab Linkage - Inspection and Modification
1AD/SD3-60/3 - Elevator Tab Linkage - Inspection and Modification
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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 Short SD3-60 Series Aeroplanes
AD/SD3-60/3 Elevator Tab Linkage - Inspection and Modification 1/84
Applicability: All model SD3-60 aircraft with S/Nos SH 3601 to SH 3623. Requirement: 1. Shorts S.B. SD360-55-A02.
- Shorts S.B. SD360-55-02 modification 7448.
Compliance: 1. Within 60 hours ("A" Check) time in service after 12 December 1983 and thereafter at intervals not exceeding 60 hours ("A" check) until modified.
- Before 31 March 1984.
Background: Analysis shows that in the event of elevator tab disconnect there could be an unacceptable level of vibration.