High Pressure Turbine - Stage 1 Disc Rim Bolt Holes and Stage 2 Disc Rim and Inner Bolt Holes

Airworthiness Directive number
29 Amdt 1
Airworthiness Directives issue number
13/1994
ID
5233
Series name
General Electric Turbine Engines - CF6 Series
Series number
AD/CF6/
Series order
5
File name
CF6-029.pdf
Folder name
CF6
Group title
TURBINE
Groups
TURBINE
Group description
Turbine engines
Authority
CASA
Online version available at: https://www.casa.gov.au//index.php/aircraft/airworthiness/airworthiness-directives/high-pressure-turbine-stage-1-disc-rim-bolt-holes-and-stage-2-disc-rim-and-inner-bolt-holes
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