AD/BEECH 95/21 - Fuselage Bulkheads FS 257.6 & FS 271.92
1AD/BEECH 95/21 - Fuselage Bulkheads FS 257.6 & FS 271.92
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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 95 (Travelair) Series Aeroplanes
AD/BEECH 95/21 Fuselage Bulkheads FS 257.6 & FS 271.92 4/79
Applicability: All models 95, B95, B95A, D95A and E95 with S/Nos TD-2 to TD-721. Requirement: Action in accordance with Beechcraft SI No 0990.
Compliance: Initially inspect within 100 hours’ time in service after 30 April 1979 and thereafter at intervals not exceeding 500 hours’ time in service or 1 year, whichever occurs first.
Background: Cracks may develop in the subject bulkheads in the areas of the horizontal stabilator attachments.