
Work on the condenser path is almost completed and the Stress Testing has not shown any pre-existing weaknesses in the structure of the gears and wings.
CANDU-ISMR/5 Installation = 100%
Aircraft Gantry (Cockpit+Quarters>Refueling Bay) = 100%
Fuel Bladders (Remaining space) = 100%
Wing Replacement = 100%
Wing Coolant Condensor Path Installation = 75%
Gear Reinforcement = 100%
Ground Stress Test = 30%