AD/BEECH 90/68 - Elevator Spar Web and Hinge Points - Inspection
1AD/BEECH 90/68 - Elevator Spar Web and Hinge Points - Inspection
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
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Beechcraft 90 and 65-90 (King Air) Series Aeroplanes
AD/BEECH 90/68 Elevator Spar Web and Hinge Points - Inspection
3/83
Applicability: Models 65-90 and 65-A90 with S/Nos. LJ-1 thru LJ-317 and B90 with S/Nos. LJ-318 thru LJ-501, except those aeroplanes having reinforced elevators as per Beechcraft SI No. 0333-131 Rev. II, or P/No. 50-610000-349 LH and -350 RH Aluminium Elevators (reference Kit Nos. 90-4061S, 90-4062S and 90-4062-1S).
Document: 1. Beechcraft SI No. 0450-133, Rev. 1.
- Beechcraft SI No. 0423-133.
Note: FAA AD 82-23-02 Amendment 39-4484 refers.
Compliance: 1. Unless already accomplished, within 200 hours’ time in service for those aeroplanes models 65-90 and models 65-A90 not fitted with elevator overhang balance horns per Beechcraft Kit 90-4029 which have achieved 2000 hours’ time in service, and thereafter at intervals not exceeding 500 hours’ time in service.
- Unless already accomplished, within 100 hours’ time in service for those aeroplanes models B90 and Models 65-A90 fitted with elevator overhang balance horns per Beechcraft Kit No. 90-4029 which have achieved 500 hours’ time in service and thereafter at intervals not exceeding 200 hours’ time in service.
Background: AD/BEECH 90/23 and AD/BEECH 90/53 have been consolidated into this AD and are now cancelled.