AD/CT58/4 - Compressor Stator Vanes
1AD/CT58/4 - Compressor Stator Vanes
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text General Electric Turbine Engines - CT58 Series
AD/CT58/4 Compressor Stator Vanes 9/85
Applicability: All CT58-100-1 and CT58-110-1 as detailed in General Electric SB (CT 58) 72-108 (CEB No. 180).
Document: General Electric SB (CT 58) 72-108 (CEB No. 180); or AD/GE-T/8.
Compliance: Before installation in an aircraft following next complete overhaul after 8 March 1968.