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Evaluation of Coking Propensity of Aviation Lubricants Using the Single Phase Flow Technique
ARP5996C
WIRE, THERMOCOUPLE, FLUOROPOLYMER INSULATED, EXTRUDED TFE NICKEL/CHROMIUM (KP); NICKEL/ALUMINUM/MANGANESE (KN) THERMOCOUPLE EXTENSION, 260 °C
AS5419/5A
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