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Your best fuel/cost savings tips

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Old 20th Sep 2018, 14:29
  #41 (permalink)  
 
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Gotta love being stuck behind the locos in Europe. If they are in front you are snookered. They do a lovely fully managed descent CDA at 250kts and in sight of the field then ask for a short base and final and the rest of us are on the speedbrake. No doubt pat themselves on the back for all that fuel they saved and what wonderful airman they are. Seems airmanship and a bit of respect for other operators sharing the sky has long left this industry. Instead its a bunch of lemmings who are to scared to take the fuel they require to do the job properly. One day you might actually take the time to compare the fuel flow on a high speed descent at IDLE power with your 250kt version.
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Old 20th Sep 2018, 20:22
  #42 (permalink)  
 
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Originally Posted by MCDU2
Seems airmanship and a bit of respect for other operators sharing the sky has long left this industry. Instead its a bunch of lemmings who are to scared to take the fuel they require to do the job properly.
Playing a bit of a devil's advocate here, so... What is the optimum descend speed? Vmo, Vmo-5, Vmo-10? Supposedly I'm no. 3 for a straight in approach to XYZ airfield, and I have planned to fly at 340 kts, but now I'm stuck behind this slow guy doing 300 and I have to use speedbrake, bunch of idiots in front of me scared of the barber pole... How does it work in this case, where is the point where the speed becomes too slow?

Hat, coat...

PS: I agree we are all in the same airspace, but people with a lot of information about operating costs (much more than it's available to an average pilot) have come up with a cost index that keeps the boat afloat, and it might be different for another airline operating same aircraft type. It's then ATC's job to adjust the speeds to keep the flow going, sometimes the slow guys have to speed and and sometimes the fast guys need to slow down.
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Old 21st Sep 2018, 06:07
  #43 (permalink)  
 
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Originally Posted by Skyjob
On similar narrow body you can save up to 50-70kg if you land using idle reverse thrust which can sometimes only be achieved by wasting those 15kgs saved through use of lower flaps. (Slow it down +15kgs, ability for landing with idle reverse -70kgs, saving 55kgs!)
On the A320 family using flaps 3 or flaps full is only about +-3/6kts on the VAPP. Does not make a big difference for the landing roll. Using autobrake low with flaps 3 and reverse idle works very nicely unless you operate on short runways I guess.
The green procedure recommends Flaps 3. I’m pretty convinced they take the potential extra fuel burn of using more reverse thrust into considerations.


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Old 21st Sep 2018, 06:16
  #44 (permalink)  
 
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"Low power to save engine life and then full thrust if you are going to get a continuous climb.
High thrust on ground can cause much higher temps than in flight and temp = $$$."


Can someone explain this. Non jet driver here. I thought the EGT would be lowest at sea level due to highest air density and that EGT climbs as you climb in altitude.
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Old 21st Sep 2018, 06:39
  #45 (permalink)  
 
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Originally Posted by tdracer
Several years ago, we were investigating a particular Asian airline that had horrible time-on-wing for their 737/CFM56 engines. Mainly sort haul, they were running out of EGT margin in ~3,000 hours - at a time when the typical operator was in the range of 15,000-20,000 hour time on wing.
Come to find out, they were using max TO every single takeoff - never a derate of any kind. At around a million dollars to overhaul an engine, you'd have to save a whole lot of of fuel to justify an extra two million dollars/year in engine maintenance...
Treble that cost. Depends also on hour to cycle ratio and operating environment, which being in Asia can be vastly lower than a benign environment. A ME3 engine for example, could operate for probably half the time as Euro-loco, which should go to the LLP limiter at 20K cycles (if operated at ~1.5 FH : 1 FC).
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Old 23rd Sep 2018, 06:54
  #46 (permalink)  
 
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Originally Posted by nomorecatering
"Low power to save engine life and then full thrust if you are going to get a continuous climb.
High thrust on ground can cause much higher temps than in flight and temp = $$$."


Can someone explain this. Non jet driver here. I thought the EGT would be lowest at sea level due to highest air density and that EGT climbs as you climb in altitude.
The higher you go, the less air there is, which means less fuel can be burnt, which means the fire in the can isn't as big, which means the EGT reduces.
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Old 23rd Sep 2018, 15:51
  #47 (permalink)  
 
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Originally Posted by GlenQuagmire
You could save a bit of fuel and a lot of localised pollution if you used towbots to take aircraft from the gate and towed them almost to the hold point so that they minimised taxiing and waiting about with the engines running. Nice autonomous towbots ensuring you only have three minutes from startup to takeoff. Heahrow would love it!


Wasn’t that trialled somewhere in Germany? Not auto bots, but towing to the holding point. It would only really work with towbarless tugs, otherwise there would be too much faffing about at the holding point. Also the tugs would need a separate route back to the apron, since I don’t think they would be able to pass alongside aircraft on a normal width taxiway?

A system called Wheel Tug has also been invented; electric traction motors in the nose wheels, powered by the APU.
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Old 25th Sep 2018, 22:23
  #48 (permalink)  
 
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Originally Posted by MCDU2
One day you might actually take the time to compare the fuel flow on a high speed descent at IDLE power with your 250kt version.
The difference (savings) come from starting descent earlier (i.e. setting thrust to idle earlier) in a low speed descent. Since for a higher speed descent your calculated TOD will be further away than for a low speed one, you'll have cruise power for some minutes longer.
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Old 26th Sep 2018, 00:09
  #49 (permalink)  
 
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Originally Posted by Escape Path
The difference (savings) come from starting descent earlier (i.e. setting thrust to idle earlier) in a low speed descent. Since for a higher speed descent your calculated TOD will be further away than for a low speed one, you'll have cruise power for some minutes longer.
Just to clarify for anyone who may have had the same misreading as me initially, that's further away from the airplane before the decent starts, not further away from the airport
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