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Police helicopter crashes onto Glasgow pub

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Old 11th Jan 2014, 21:15
  #1681 (permalink)  
 
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One pipe and one transfer pump (low fuel level) to two supply tanks, is a risky game.
http://www.airbushelicopters.com/sit...uel_system.pdf

There are two pumps and two pipes in parallel circuit. I'd expect the pump capacities vs pipe bores and fuel demand to have been considered for all the possible failure conditions...that's first year mech eng stuff. Looks like a perfectly sound system to me, assuming that there is a strainer/filter before the tanks, which there is bound to be.
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Old 11th Jan 2014, 21:17
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Bearing in mind this threads title, doesn't all this fuel system talk need to be on a different thread?
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Old 11th Jan 2014, 23:17
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Pie Chaser
Airbus know very well how much fuel was in each tank at point of impact.
I very much doubt that is even possible. Unless you are saying there is a known failure mode that would have produced such a tragedy from that precise amount? That would be tantamount to criminal negligence were that not widely publicised beforehand. Non of our EC135 contributors (or BO105-similar system?) has yet offered such an explanation?

I suspect the final determination may be a little more prosaic? But that's just my opinion!

Last edited by Tandemrotor; 11th Jan 2014 at 23:28.
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Old 11th Jan 2014, 23:36
  #1684 (permalink)  

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PC;
There is a report coming out very shortly, so let's just hope everything will become much clearer and a design change will be made.
It's not the January Bulletin you mean by 'a report coming out very shortly' is it?

http://www.aaib.gov.uk/cms_resources...l%201-2014.pdf
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Old 12th Jan 2014, 08:45
  #1685 (permalink)  
 
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There are two pumps and two pipes in parallel circuit

Thanks for the link. There is only one red pipe from the main tank prior to splitting into two before entering the supply tanks.

That is NOT two independent supplys. A rupture of the red pipe will result in loss of feed to BOTH supply tanks.
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Old 12th Jan 2014, 08:59
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Robin, I think that's a simplified schematic as the positioning of NRVs was discussed earlier in this thread by those with knowledge of type. There have to be flex couplings if solid pipes are used and bulkhead mounts, so I think we can assume a lot has been left out of the schematic for clarity.

However, the truth is that this accident was unexpected (aren't all?). We have an experienced and well-respected pilot and a major operator with a good safety record, crewed/manned by responsible people rather than a couple of champagne Charlies or "A-Listers" in the back making whoopee. The weather was excellent, viz good. This accident was never meant to happen so we can expect the unexpected.
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Old 12th Jan 2014, 11:27
  #1687 (permalink)  

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The schematic is simple yet portrays the system well.
Transfer hoses come from the trans pumps and are connected to each other, and in turn to the supply tanks. It seems to me that if there is a leak or failure anywhere in the flexible transfer hose, the fuel will end up being circulated within the main tank and perhaps not be able to top up the supply tanks fast enough to prevent them emptying.

The check valve is integral to the transfer pump unit.

But of course, if this was to have happened the engines wouldn't have stopped at the same time and the fuel warnings and gauge would have indicated something to the crew.(therefore this part of the thread is imho better off being in the 135 thread)
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Old 12th Jan 2014, 11:38
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Sid

But of course, if this was to have happened the engines wouldn't have stopped at the same time
We do not know that both engines stopped at the same time.
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Old 12th Jan 2014, 12:27
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Sid --
It seems to me that if there is a leak or failure anywhere in the flexible transfer hose, the fuel will end up being circulated within the main tank and perhaps not be able to top up the supply tanks fast enough to prevent them emptying.
I'd bet that's the sort of defect they would have been looking for in any case would have been found by now, with a directive to check/repair all a/c in service. The only directive we are aware of is a fuel indication issue - i.e. an instrumentation issue, not a safety issue per se.
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Old 12th Jan 2014, 12:45
  #1690 (permalink)  

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Chop;
Sid
But of course, if this was to have happened the engines wouldn't have stopped at the same time
We do not know that both engines stopped at the same time.
It's a statement of fact based on the system, not a speculation. That's why there's an 'if'

Back to the big question, how do you get to a point a metre above a roof in a vertical descent with the transmission system stationary? We do not know if this incident had anything whatsoever to do with fuel, and personally I still don't think it is.
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Old 12th Jan 2014, 12:54
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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, 13:05
  #1692 (permalink)  

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...... Or you could tell us where we are all going wrong
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Old 12th Jan 2014, 13:43
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Not a Clue

From the posts you all seem unable to have a consistent and accurate understanding.
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Old 12th Jan 2014, 13:48
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Not a Clue
From the posts you all seem unable to have a consistent and accurate understanding.
So You have it? I'm waiting for explanation!

skadi
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Old 12th Jan 2014, 13:56
  #1695 (permalink)  
 
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You tell me please

How do you opertate the transfer pumps ( with a low fuel level ) transiting from hover to cruise and back to hover.?
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Old 12th Jan 2014, 14:05
  #1696 (permalink)  
 
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You tell me please
How do you opertate the transfer pumps ( with a low fuel level ) transiting from hover to cruise and back to hover.?
Please read my post #1429.

skadi
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Old 12th Jan 2014, 14:06
  #1697 (permalink)  

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How about keeping system issues to the 135 thread?

p.s. I think Robin is talking check valves
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Old 12th Jan 2014, 14:12
  #1698 (permalink)  
 
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Not nrv valves Transfer pumps.
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Old 12th Jan 2014, 14:13
  #1699 (permalink)  
 
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Gone to 135 posts. Out.
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Old 12th Jan 2014, 14:56
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irony...

Originally Posted by SilsoeSid
It's not the January Bulletin you mean by 'a report coming out very shortly' is it?

http://www.aaib.gov.uk/cms_resources...l%201-2014.pdf
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 ?
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