AD/APU/1 - Turbine Blade Containment Ring - Installation
1AD/APU/1 - Turbine Blade Containment Ring - Installation
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 107 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text Auxiliary Power Units
AD/APU/1 Turbine Blade Containment Ring - Installation NK
Applicability: Airesearch Model No
GTCP85-98D with Serial No. prior to 28008.
-98W with Serial No. prior to 30734.
-99 with Serial No. prior to 14744.
-115 with Serial No. prior to 18801.
-115C with Serial No. prior to 35975.
Document: Airesearch SB No. 49-1790.
Compliance: Before installation in an aircraft following next reconditioning or hot end repair after 30 November 1971.