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Anybody know if a 800XP with API winglets can carry 1600lb payload over a 2000nm trip (no wind) at intermediate cruise speed and still land with sufficient reserves?
Thanks...
Yes.
BOW of 16,400 LBS, 1,600 LBS payload makes you 18,000 ZFW. Add 10,000 lbs of fuel (max) and you're at 28,000 lbs, which is the max t/o weight. That's enough fuel to go 2,500nm at max cruise power.
Yes.
BOW of 16,400 LBS, 1,600 LBS payload makes you 18,000 ZFW. Add 10,000 lbs of fuel (max) and you're at 28,000 lbs, which is the max t/o weight. That's enough fuel to go 2,500nm at max cruise power.
Who cares? 410 is just fine for us normal folks.Will it go to FL 510?
Who cares? 410 is just fine for us normal folks.
Anybody know if a 800XP with API winglets can carry 1600lb payload over a 2000nm trip (no wind) at intermediate cruise speed and still land with sufficient reserves?
Thanks...
Will it go to FL 510?
From ARINC:
TEB-NYL (Yuma,AZ) 2050nm (optimized route)
Payload -1600lbs
Fuel Required - 9692lbs (assuming 250lb taxi)
Reserves - 1500lbs (I plugged in a 45 minute reserve but it came out to 980lbs. I don't know anyone who would land with that)
T/O Wt - 27,571
Rwy analysis - can depart rwy 1 at 28,000lbs up to 32c flaps 0Am I missing something?
The plane holds 10000 lbs max fuel, and the above trip needs 9692?
Soooooo....are saying you can actually DO that trip?
From ARINC:
TEB-NYL (Yuma,AZ) 2050nm (optimized route)
Payload -1600lbs
Fuel Required - 9692lbs (assuming 250lb taxi)
Reserves - 1500lbs (I plugged in a 45 minute reserve but it came out to 980lbs. I don't know anyone who would land with that)
T/O Wt - 27,571
Rwy analysis - can depart rwy 1 at 28,000lbs up to 32c flaps 0Am I missing something?
The plane holds 10000 lbs max fuel, and the above trip needs 9692?
Soooooo....are saying you can actually DO that trip?
I believe the 9692 is including the reserve.
Oooooo! I'm so jealous!! What are you 12?You obviously haven't made it to a Gulfstream yet.
Ummm, no, it's not a LR60.
Being a person who has had a window depart the aircraft, you can have your FL510. No interest at all. I am sure you guys wear your mask too.
Pretty sure the difference in useful consciousness between an explosive decompression at FL410 and FL510 would be fairly imperceptible - if you're not already on a mask or proficient at the whole "quick don" concept you're going to be just as dead.
How many explosive and/or rapid Ds happen every year, though?
All joking aside, I'm with 400a 100%.
There is no performance reason to be at FL510 in any business jet. Its a sales gimmick that all the OEMs have jumped on.
Also, no departments I know fly up there, and if you did you would be called on to explain your reasoning.
All joking aside....why are you hesitant to operate the airplane to the full extent of its operating envelope?
Is it a risk managment/mitigation decision? Or one based on the fact that many swept-wing airframes simply don't gain much above the mid 40s?
Again, no flame or joke...just trying to learn.
Still don't quite understand why you corporate types love the high FLs... I have issues going higher than 350, not for performance but for solar radiation. Can't count the number of times we're at 350 and I see some high contrail, flick the TCAS to Above and find someone up at 450 or above... just plain craziness. Do you guys realize the amount of radiation you are subjecting yourselves to?
All joking aside....why are you hesitant to operate the airplane to the full extent of its operating envelope?
Is it a risk managment/mitigation decision? Or one based on the fact that many swept-wing airframes simply don't gain much above the mid 40s?
Again, no flame or joke...just trying to learn.
Still don't quite understand why you corporate types love the high FLs...
Do you guys realize the amount of radiation you are subjecting yourselves to?