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#2
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![]() "Bertie the Bunyip" wrote Another factor is the distance travelled. It makes no sense to go to 410 on a 200 mile trip. Having said that, the ideal fuel burn profile is close to straight up and straight down on short trips. No level cruise. IOW, you keep climbing until you intercept the descent profile and then come down. Yep, I've been on flights like that. Kinda' strange. What percentage of power are the engines normally running, on the "coming down" portion of a flight like that? -- Jim in NC |
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"Morgans" wrote in
: "Bertie the Bunyip" wrote Another factor is the distance travelled. It makes no sense to go to 410 on a 200 mile trip. Having said that, the ideal fuel burn profile is close to straight up and straight down on short trips. No level cruise. IOW, you keep climbing until you intercept the descent profile and then come down. Yep, I've been on flights like that. Kinda' strange. What percentage of power are the engines normally running, on the "coming down" portion of a flight like that? Idle, Right back to the stop is the ideal as far as you can safely do it. You're supposed ot have the power up to stabilised approach power by about 1,000', bu tit's almost impossible not to touch the taps before then because of ATC. Bertie |
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Morgans writes:
What percentage of power are the engines normally running, on the "coming down" portion of a flight like that? Flight idle. |
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Mxsmanic wrote in
: Morgans writes: What percentage of power are the engines normally running, on the "coming down" portion of a flight like that? Flight idle. And what's that, wannabe boi? Bertie |
#6
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![]() AFAIK the new Bus has one of F430 as well. You can fly right up to the service ceiling but the max allowable FL goes down with weight. THe buffet margins become tighter when you are heavy and the max allowable altitude goes down accordingly,. As you burn fuel you can go up in steps, so on a long trip you might originally be limited to say, FL330 and then after an hour or two your limit may rise enough that you can get to 350 and then again to 370 and so on until you either get to max or its time to come down. The performance computer (integrated into the FMS) gives you a constant readout of the limit. I see.. that actually explains what I saw on a Cathay flight across the Pacific last year. It appeared to level off at 35 but when I checked 6-7 hrs or so later (on the moving map) we were at 40. At the time I thought the climb rate beyond 35 must be very slow but I think its to do with weight as you explained. Also, it's not so clever to go up another 4,000 feet if you're going to have another 100 knots on your nose! A typical rule of thumb tradeoff for wind/altitude is about 7knots per 1,000 feet, though this isn't hard and fast.We have tables for it or you can put some projected winds into the FMS and ask the computer to do it for you. Another factor is the distance travelled. It makes no sense to go to 410 on a 200 mile trip. Having said that, the ideal fuel burn profile is close to straight up and straight down on short trips. No level cruise. IOW, you keep climbing until you intercept the descent profile and then come down. Bertie |
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#8
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![]() "Bertie the Bunyip" wrote in message .. . wrote in news:c3217254-afdf-40c0-b87a- : Out of curiosity I was wondering which civilian passenger airplanes snip Also, it's not so clever to go up another 4,000 feet if you're going to have another 100 knots on your nose! A typical rule of thumb tradeoff for wind/altitude is about 7knots per 1,000 feet, though this isn't hard and fast.We have tables for it or you can put some projected winds into the FMS and ask the computer to do it for you. In the Lear we sometimes found you could climb out of the headwind. With the 100kts on the nose at FL350, we could go to FL430 and get out of half of it.(Westbound Winter) Another factor is the distance travelled. It makes no sense to go to 410 on a 200 mile trip. Having said that, the ideal fuel burn profile is close to straight up and straight down on short trips. No level cruise. IOW, you keep climbing until you intercept the descent profile and then come down. The old Lears, did exactly that. They had enough thrust to go direct to FL450 at gross, and burned so much fuel it was worth while to get high and keep it there until you had to come down. Rule of thumb was trip distance in tens of miles times 2 for the cruise altitude. 200nm=40,000, we would file for 41. Al G |
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"Al G" wrote in
: "Bertie the Bunyip" wrote in message .. . wrote in news:c3217254-afdf-40c0-b87a- : Out of curiosity I was wondering which civilian passenger airplanes snip Also, it's not so clever to go up another 4,000 feet if you're going to have another 100 knots on your nose! A typical rule of thumb tradeoff for wind/altitude is about 7knots per 1,000 feet, though this isn't hard and fast.We have tables for it or you can put some projected winds into the FMS and ask the computer to do it for you. In the Lear we sometimes found you could climb out of the headwind. With the 100kts on the nose at FL350, we could go to FL430 and get out of half of it.(Westbound Winter) Yeah, we hardly ever get on top of a jetstream unless it;s very low. Alos, we'd be wary of even trying in case we hit the cold side CAt near our margin. Another factor is the distance travelled. It makes no sense to go to 410 on a 200 mile trip. Having said that, the ideal fuel burn profile is close to straight up and straight down on short trips. No level cruise. IOW, you keep climbing until you intercept the descent profile and then come down. The old Lears, did exactly that. They had enough thrust to go direct to FL450 at gross, and burned so much fuel it was worth while to get high and keep it there until you had to come down. Rule of thumb was trip distance in tens of miles times 2 for the cruise altitude. 200nm=40,000, we would file for 41. More importantly, you had the buffet margins. We could also go to that altitude if power were the issue, but at max gross, we're limited to about 350 initially. |
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