Post by jardx on Oct 12, 2019 17:41:02 GMT
I posted in the Douglas forum about a similar fuel feed logic error that I saw while attempting to conduct realistic operations of the fuel system in the DC-9.
1. I did match model version to panel version
2. No, I did not mess with the aircraft cfg or air file
3. Yes, I am using the most current core gauge/panel/model files
4. Yes, I read Mark's Handling Notes
I saw something in the same neighborhood with the B707-700 with the CFM engines with a fuel load that required fuel in the center tank, not sure about the other B707 models.
If you use one boost pump per main tank (for at the bare min engine start) then turn the second boost pump on with at least one main crossfeed valve open to assure positive fuel feed in the event of engine or boost pump failures, you get tank to engine feed.
When you attempt to burn out of the center only, open the 1 through 4 crossfeeds turn on the center tank boost pumps turn off mains 1 and 4 I saw the feed come from number 2 and 3 main tanks only.
In the fuel management document it was stated that this config of the fuel system should yield a feed from the center tank only as the pressure output from the center pumps is greater then the main pumps there for overriding the feed from mains 2 and 3.
"3. Main tanks boost pumps 1 and 4: off; Main tanks boost pumps 2 and 3:on; central tank boost
pump: on; 1, 2, 3 and 4 crossfeed selectors: open.
This is the setup for using the central tank fuel. Notice the main boost pumps 1 and 4 are turned
off and the central tank boost pumps are on. This way fuel will be supplied from the central
tank to engines 1 and 4. A smaller quantity will also go to engines 2 and 3. This mode is used
after takeoff, when a certain amount of fuel from the main tanks has already been used
(14,000lb recommended)"
pump: on; 1, 2, 3 and 4 crossfeed selectors: open.
This is the setup for using the central tank fuel. Notice the main boost pumps 1 and 4 are turned
off and the central tank boost pumps are on. This way fuel will be supplied from the central
tank to engines 1 and 4. A smaller quantity will also go to engines 2 and 3. This mode is used
after takeoff, when a certain amount of fuel from the main tanks has already been used
(14,000lb recommended)"
I did not get this result.
As a test I turned all main pumps off to see if the feed logic would shift to the center tank, it did not instead it started feeding from number 2 main tank only.
With all this in mind I wanted to test/check the crossfeed and boost pump operation by purposely starving an engine, in this case number 3, of fuel by keeping the boost pumps off in tank 3 and closing the number 3 crossfeed valve. As expected after closing the number 3 crossfeed valve engine 3 shutdown.
I re configed for a tank to engine feed for number 3 restarted number 3 then recycled all main boost pumps and finally got a center tank only feed with no main boost pumps on, center tank pumps on, and all main crossfeed valves open.
So my conclusions from this experience are either there is a coding error in the fuel system, the fuel tutorial document needs to be reworded as the present text is misleading or in the case of the DC-9 you simply can not use only one boost pump in the tanks even though the panel manual states that you can.
As with the DC-9 fuel system post/thread I am simply throwing this observation out there. I know that more then likely nobody has the time to fix it if there is indeed a bug in the coding of the fuel feed logic and I know that these models and panels have been published for 10+ years with no one else seeing this behavior.
So maybe this post was made in case anyone saw this behavior and was wondering if they were crazy.
Jared