A320 PTU Inhibition - FCOM
Hey everyone! It has come to my attention recently during One Engine Taxi procedures how the PTU seems to be inhibited after the ENG 1 start, but then starts running before the Y ELEC PUMP is turned ON.
I remember reading older FCOMs from years ago, and seeing a few "PTU Running conditions" eg. Park BRK not ON, etc.... Somehow, it appears these diagrams have now disappeared from newer FCOMs (MSNs 7500-10500) yet the same conditions pro PTU operations have remained. Does anyone really know why this information could have been removed from the manuals? And more importantly, does the PTU still run under the same conditions as it did before? This is ALL I could find on my FCOM. Can't`upload pictures yet so had to copy the text!
Thanks in advance! I'm really looking forward to learning more of the A320, since I've only flied it for a few months now. |
I dont know why Airbus removed the PTU diagram you mentioned however the information can be found in the Landing Gear chapter in the tables that show interaction between landing gear and other systems.
i.e PTU will run ( if more the 500 PSI pressure diff) 1. Both engine masters off, or 2. Both engine masters on, or 3. Nose wheel not in the towing position and park brake off. The above applies to “on ground”. |
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