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Old 9th Jan 2014, 18:35
  #961 (permalink)  
 
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Just thinking...The engines sucking in fuel via the inletport of the prime pump.....transfer pumps delivering the fuel from the main tank to the supplytank. Assuming the transfer fuel lines exits situated somewhere on/near the bottom of the supply tank...the fuel flow generated by the transferpumps is way larger than the suction flow to the engine. Is this creating some swirl effect in the supply tank.....when you suddenly stop the supply from the transfer pumps; the swirl will continue for a couple more minutes, creating static pressure drop at the exit of the fuel transfer line, and thus continue pulling fuel from the main tank. The swirl effect slows in time and after some minutes the static pressure drop ceases to exist and the engine starts sucking from the supply tank........
So I think a lot of sucking is involved

so if you did a similar check without switching on the transfer pumps at the beginning of the sequence....no swirl created,.... the supply tanks would start emptying rightaway. (assuming the main tank Qty level is below the overflow channels)
Yellowbird, I think thats the first plausible explanation since I started this long debate with my simple question... Thanks!

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Old 9th Jan 2014, 18:52
  #962 (permalink)  

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Sucking fuel for 15 minutes from the main tank to the supply through all that pipeage simply by the pressure difference caused by a swirl that can be reproduced by making a cup of tea …. if only we'd known about this effect before archimedes invented his screw
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Old 9th Jan 2014, 21:09
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. if only we'd known about this effect before archimedes invented his screw*
Are you really that old Sid?

Yep, because I question things*
That's a good thing, so do I, that's the main reason why I decided to disagree with you on this issue....and await your condescending reply to it........and you didn't disappoint me.
(also looking forward to your reply on this one)
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Old 9th Jan 2014, 21:42
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Phoinix; We had exactly the same; 159 till 139 after XFER pumps OFF, sucking at it for almost 15' before supply tank indication dropped."
So, a 20kg decrease in that time....I observed the exact same behaveour in two out of two checks I did in our company. Only difference: we started at appr. 240kg in the main tank decreasing to appr 220 before the supply tank quantities started to decrease.(in about the same amount of time)
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Old 9th Jan 2014, 22:04
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that's the main reason why I decided to disagree with you on this issue....
Interesting, surely in a discussion you either agree or disagree about something based on your own reasoning, knowledge, experience ... you don't decide to disagree.



p.s. Remember what Viper said about arrogance?

Viper
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Old 9th Jan 2014, 22:22
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.. you don't*decide*to disagree.
Sid, thanks, point taken......my only excuse is that english is not my native language, but I assume all native speakers already figured that out when reading my posts.

p.s. Remember what Viper said about arrogance?
You're right again......Viper rules.. I'll try to remember that.
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Old 9th Jan 2014, 23:11
  #967 (permalink)  

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I must have missed that Y135, I guess we agree to disagree.
Perhaps there will be some more investigation into this phenomena
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Old 10th Jan 2014, 16:13
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Yellowbird, I think thats the first plausible explanation since I started this long debate with my simple question... Thanks!
Very easy way to find out!

With transfer pumps off, Run the supply tanks down until red fuel warning.
Shut down the engines.
Turn on both transfer pumps, when supply tanks start filling, turn off transfer pumps and monitor the supply tank levels.
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Old 10th Jan 2014, 16:49
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PC,

yep...could be, but I'm not sure whether the suction of a running engine is needed to create this phenomena.
I'm not even sure if this actually is the explanation..........I just can't think of anything else.
To be honest, I know I have a creative imagination, but I would never have predicted this effect (if it's true) to continue for this long.
I think that the boys and girls from Donauwerth might have addressed the "couple of minutes" note in the ASB a little further.
I was about to shut down the thing after more than 10 minutes wittnessing the Main tank qty go down, thinking I must have done something wrong.

Still, I'm almost certain now that this is exactly what happens.

Last edited by yellowbird135; 10th Jan 2014 at 16:53. Reason: another typo
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Old 10th Jan 2014, 20:08
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Donauwörth
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Old 10th Jan 2014, 22:56
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6 pumps, 4 nrv, 3(4) fuel tanks - still no consensus on how it works - uphill swirl syphoning, I see! certifiable !
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Old 12th Jan 2014, 13:04
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Factory Training

Having read most of the posts regarding this tragic accident there seems to be a great deal of poor understanding of the fuel system.

May respectfully suggest that all crew go on a FACTORY training course ensuring that they fully and correctly understand the systems they are operating.
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Old 12th Jan 2014, 14:26
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..cont from other thread.

I thought you might have been on about transfer pump failures/turned off, with a check valve failure.
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Old 12th Jan 2014, 14:44
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Normal flight ops......use of transfer pumps with low main tank fuel levels.

Last edited by Robin400; 12th Jan 2014 at 14:47. Reason: addition to text
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Old 12th Jan 2014, 15:33
  #975 (permalink)  

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brought over from other thread..

AnFI
SS - The irony of your post is staggering - the first accident in the AAIB report, you point to, is a double engine stoppage of a twin cause by fuel exhaustion - given that that may also be the case here (and other complete power loss events) it is tempting to conclude that the mathematical assumptions concerning the safety of TWIN ENGINED helicopters is FLAWED - is the rarety of full power loss in twins actually 10^-9 per hour ?
Anfi, Sorry, I didn't produce the AAIB Bulletin

Umm, if you care to read the first incident all the way to the end, you'll get to the bit that says, "no action was taken to select an alternative fuel source for the engines after their power loss."

Single or twin, if the crew don't switch tanks, the engine will stop
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Old 12th Jan 2014, 15:49
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SS

Agree SS

more complexity - more room for human error - more human errors

if you have 2 FCL then it is possible to retard the wrong one - if you don't it is not possible....

It is clear that if an 'internet room' full of experts can't work out how a fuel system works that it is probably too complicated - if a system is prone to human failure then it's not totally 'Kosher' to blame pilot's - it's a whole system deal

Stats don't support the theory
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Old 12th Jan 2014, 16:29
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I'm really surprised to hear that the fuel system (airframe) is considered complicated, I can imagine people having difficulties (before anyone starts asking......myself included) with the engine fuel system. But a bladder divided in 1 large, 2 small reservoirs, a couple of impeller pumps........how complicated can it be?
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Old 12th Jan 2014, 17:14
  #978 (permalink)  

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Human factor wise, how is the fuel system being considered complicated?
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Old 12th Jan 2014, 17:49
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yellowbird
I'm really surprised to hear that the fuel system (airframe) is considered complicated, I can imagine people having difficulties (before anyone starts asking......myself included) with the engine fuel system. But a bladder divided in 1 large, 2 small reservoirs, a couple of impeller pumps........how complicated can it be?
Doesn't look over-complicated to me, either. Clearly, without pilot intervention fuel should be automatically pumped and supplied to both engines until all fuel exhausted, other than in a leak or other malfunction when maybe one should shut down automatically.

I thought these are diaphragm not impeller pumps? I'm sure I read that and would seem to me to be the better choice with these low fuel flow rates.
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Old 12th Jan 2014, 17:50
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Fuel system complexity

I total agree that the fuel system is not complicated.

How the system is managed with fuel levels below the weir is where l guess a certain procedure is required.

I have asked how you manage the TRANSFER PUMPS to ensure that one is submerged in fuel with the change in pitch attitude with no reply.

My understanding is the one pump may be above the fuel and switched off.



I thought these are diaphragm not impeller pumps? This is what worries me, if you operated a 135 you should know. Do you not do a tech refresher course.

Last edited by Robin400; 12th Jan 2014 at 18:00.
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