A-320 Single Engine Taxi out Myth Busters
#51
reddog,
Is there any data to support the actual savings of fuel at the heavier weights? Is there a published report where two planes at identical weights travel the same taxi route and show the difference between fuel used? What I see in ATL during my commutes is a lot of high power settings during breakaway, acceleration and during uphill taxi segments. Then there's the high power settings during crossbleed start. I've never seen an actual side by side comparison.
Carl
Is there any data to support the actual savings of fuel at the heavier weights? Is there a published report where two planes at identical weights travel the same taxi route and show the difference between fuel used? What I see in ATL during my commutes is a lot of high power settings during breakaway, acceleration and during uphill taxi segments. Then there's the high power settings during crossbleed start. I've never seen an actual side by side comparison.
Carl
Everyone is waiting on your to go all latin on me.
#52
#53
I'll admit to being a solid C physics student, but I do understand momentum. This is what I was saying in the other thread, I'm not seeing the savings taxi out as two in idle has to be about the same as one at a higher setting.
TSquare says Delta looked at it 15 years ago, and we're wrong. So I guess there are figures somewhere.
TSquare says Delta looked at it 15 years ago, and we're wrong. So I guess there are figures somewhere.
#54
I'll admit to being a solid C physics student, but I do understand angular momentum. This is what I was saying in the other thread, I'm not seeing the savings taxi out as two in idle has to be about the same as one at a higher setting.
TSquare says Delta looked at it 15 years ago, and we're wrong. So I guess there are figures somewhere.
TSquare says Delta looked at it 15 years ago, and we're wrong. So I guess there are figures somewhere.
If your captains are taxiing it right, breakaway thrust at single engine is basically the same as two engines on the 757. It doesn't take more than idle thrust to keep going in the 757 at anytime single engine unless it's a steep hill.
#55
#56
Carl
#57
Gets Weekends Off
Joined APC: Nov 2005
Posts: 758
Spirit std is s.e.taxi. In the four years I've been a babybus Cpt, I can't remember more than a few times that a second engine was necessary to taxi. In fact, one turning in a 319 loaded up with 145 pax, and fuel for FLL LGA takes little more than idle thrust to break away and gives a nice ten or so knot taxi which requires very little braking. We use the APU to start #2 which eliminates the crossbleed problem.
Funny thing, I always assumed that s.e.taxi was a NWA thing because Jeff Carlson started it at Spirit.
Truthfully, I started using it mostly because they load so little fuel up, I hated to burn that "six hundred pounds for momma and the kids" up just sitting around on taxi out. Then I discovered that it really made things easier.
Funny thing, I always assumed that s.e.taxi was a NWA thing because Jeff Carlson started it at Spirit.
Truthfully, I started using it mostly because they load so little fuel up, I hated to burn that "six hundred pounds for momma and the kids" up just sitting around on taxi out. Then I discovered that it really made things easier.
#58
Gets Weekends Off
Joined APC: May 2005
Position: B777/CA retired
Posts: 1,502
At AWA we used single engine taxi somewhat, but after fuel spiked over the last couple of years there has been a real big push for single engine taxi. We did it a lot on the 757 because we were Brake release fuel limited on some of our flights to Hawaii (we had some 240k GTOW jets with full loads). I did not think much of the idea (our previous PH discouraged SE taxi over 205K) but after flight ops engineering talked to Boeing they said it was OK up to Max TOW. I never had an issue with breakaway thrust, especially since we have gone to all concrete taxiways in PHX.
On the Airbus standard procedure is SE taxi. I would think there might be an issue in ATL because you have some pretty good slopes on those taxiways. But for us in PHX, PHL or most other places it works just great. I like having fuel in my tanks without carrying a lot of unecessary extra fuel. Sitting # 25 in JFK saves a lot of gas.
One thing about shutting down the APU and cross bleeding the other engine start - if it is warm out there is more airflow and less fuel burned by running the APU bleed.
On the Airbus standard procedure is SE taxi. I would think there might be an issue in ATL because you have some pretty good slopes on those taxiways. But for us in PHX, PHL or most other places it works just great. I like having fuel in my tanks without carrying a lot of unecessary extra fuel. Sitting # 25 in JFK saves a lot of gas.
One thing about shutting down the APU and cross bleeding the other engine start - if it is warm out there is more airflow and less fuel burned by running the APU bleed.
#59
Gets Weekends Off
Joined APC: Jul 2006
Posts: 2,918
Until AA management actually shares profit sharing with us and stops stealing from us to enrich their own coffers, they can shove their S.E. taxi where it's dark and gloomy.
Two engine taxi out with APU for takeoff, two engine taxi in and APU stays on at all times at the gate. Safety first, crew/pax comfort second, fuel savings = FUPM!!
#60
Gets Weekends Off
Thread Starter
Joined APC: Feb 2006
Position: A320 CA
Posts: 973
I'll admit to being a solid C physics student, but I do understand momentum. This is what I was saying in the other thread, I'm not seeing the savings taxi out as two in idle has to be about the same as one at a higher setting.
TSquare says Delta looked at it 15 years ago, and we're wrong. So I guess there are figures somewhere.
TSquare says Delta looked at it 15 years ago, and we're wrong. So I guess there are figures somewhere.
Never took physics...and I'm just a dumb rotor head.
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