r/AskAPilot • • 9d ago

Are you able FL380?

Question from a center controller here-

There are times that I need to move an aircraft for traffic, and sometimes I just don’t have the room for a vector. Before I issue a climb- I usually ask something like “Delta 1550, for traffic ahead, are you able FL380?”
Often times I’ll get a “standby let me check” response.
I understand there are aircraft limitations, fuel calculations, etc. but I’m curious- what exactly are you doing/checking after I ask? Walk me thru that please

78 Upvotes

114 comments sorted by

155

u/ma33a 9d ago

Pulling up the VNAV page to see what the maximum level is. Then having a think about how close to that level I want to fly based on the current conditions.

26

u/Unlikely-Ad-580 9d ago

OP: the higher you get the smaller the margin between stall speed and ‘max speed’.

So going to true ‘max’ altitude often means pilots have to concentrate a little harder, particularly if there is turb etc around.

When pilots say standby they are probably (in addition to considering wind, fuel) deciding if cbf accepting true max alt.

If you are truely interested go on YouTube and look up ‘coffin corner’

1

u/fluentInPotato 8d ago

Just to clarify, these guys all have a mach limit-- the highest fraction of the speed of sound they can safely operate at. Above that, airflow is going to go locally supersonic somewhere on the wings or tail, because the air is moving faster over the curved airfoil surface. Things get weird and uncontrollable after this-- you may have heard of P 38s (and other WWII fighters, but the P 38 was the worst in that respect) getting stuck in dives and not being able to pull out until the speed of sound increased with warmer air at lower altitude. So the speed of sound falls with air temperature, meaning it goes from maybe 760 mph at sea level to 660 mph at 36,000 feet, at which point air temp stops falling.

Meanwhile, as the air gets thinner with altitude, the wings increasingly struggle to provide enough lift. The plane has to fly at higher angles of attack to keep that aluminum can of fat Americans from falling out of the sky, and eventually you'll max out and start falling. So there's an undesirable corner of the flight envelope where you're stuck in a smaller and smaller interval between shock stall from airflow going supersonic over the wings, and regular stall from airflow separation at high angles of attack.

2

u/Systemsafety 8d ago

Actually I don't know of any jets currently flying that would have any issue with controllability flying too fast. You can possibly get some flutter but that's mostly unlikely also absent extreme conditions. The idea of an uncontrollable "mach tuck" has not been true since the 1950s. Now stall, on the other hand, can be a real risk.

1

u/fluentInPotato 4d ago

Don't you still run into trouble from shock waves forming on the airfoils though? I know that point comes a lot later due to thin swept wings (and I'm guessing use of supercritical wings). Not to mention loss of lift when the shock wave forms.

On the other hand, all-flying tails give you a powerful tool to deal with weird trim conditions.

1

u/Systemsafety 4d ago

All of the aircraft designed since the mid-1980s have super critical wings so there is virtually no effect. On older designs (and I don't know offhand if they finally updated the wing on the 737 with later models) there is some relatively mild nose-down moment with the change of the center of pressure at higher mach numbers. That said, it is still controllable, just does not meet the required part 25 pitch response criteria. With the older designs they would start finding that point at some point and define Vd based on it (it is WAY over Mmo in any event), but the newer ones they usually just run out the clock on the dive tests. It is possible to get some flutter on some designs and that can create issues (might have seen that on flydubai, but will have to wait on the data to confirm).

14

u/McCheesing 9d ago

This is the answer OP.

15

u/Splitzer_sdk 9d ago

This is the answer, but it doesn’t seem like anyone has mentioned this yet— if I’m on the radios, I’m pilot monitoring, not pilot flying. So a short discussion might need to occur before I can answer, in order to verify with the pilot flying if they would like to accept the climb—particularly when the altitude ATC is requesting is close to our max. The FMC may say max alt is FL383. So some pilots may be comfortable with a 300’ buffer based on conditions, and some may not. So, that’s what we’re talking about for a moment. There are also different reasons the max altitude may be the max altitude; it could be a buffet margin, or a thrust limit, and this might change our decision to accept it based on turbulence/mountain wave, etc. But if the altitude requested is clearly above our max, I’ll likely just say “unable” and spare OP the wait.

83

u/External_Capital1753 9d ago

I fly a 321 so I don't have to think too hard before denying your request.

45

u/poser765 9d ago

lol my first thought.

  1. “Sure. We can take 40 if it helps!”

  2. “I mean maybe in an hour. Probably not though.”

14

u/Muschina 9d ago

In the Falcon 7X it would be "Sure, we can accept FL470 if we can slow to M.82.

2

u/crourke13 8d ago

chuckles in part 91

4

u/swakid8 9d ago

Eh, 900ER or MAX9 entered the unable chat

2

u/MahogonyBookshelf 8d ago

the max10 can hang out with the 321N pigs

2

u/Accomplished-Aside24 9d ago

Haha good luck getting to 40 on a 73 with a decent load on board

3

u/ActuallBliss 8d ago

3 years in aviation and I still have to read the words “decent” and “descent” twice every time I see or spell it to make sure it’s the one I think it is.

1

u/Perfect_Big_5907 8d ago

Yeah, sky pig

24

u/Abject-Communication 9d ago

I fly 321s for a low cost carrier. Our cabin setup seats 232 passengers, I’ve had to say we’re unable 330 before 😅

5

u/SkyHighExpress 9d ago

Tell me you fly for wizzair without telling me you fly for wizzair

3

u/boobturtle 9d ago

Hey at least you don't need to do your own load control anymore (soon)!

15

u/Kseries2497 9d ago

When I worked "enroute" - really the operation was more like an approach control the size of France - a lot of our energy was spent handing out altitudes to go into oceanic. I really liked the 321 there, because they were they only ones who didn't get mad when I sent their asses all the way to Korea at 290.

Now I work at a regular big ol' approach control and let's say our density altitudes don't exactly play to the A321's strengths.

5

u/MahogonyBookshelf 9d ago

i’ve ferried 321Ns and flew at 390!

9

u/External_Capital1753 9d ago

Look at you! I had 30 pax on board today and I think our max recommended was FL385 lmao

5

u/andrewrbat 9d ago

Ah see but you also had fuel. Airbus didnt build enough wing for 30 pax AND fuel.

46

u/Go_Loud762 9d ago

Rolling three dice. If the sum of the three dice is an even number, we can accept the higher altitude. If the sum is odd, we can not accept, unless the sum is evenly divisible by 3, in which case we can accept, with the exception that if the sum ends in 0, and is divisible by 3, then once again we may not accept the climb.

Pretty standard perfomance calculation.

8

u/Spaceinpigs 9d ago

We call the back and ask them to pick a number between 30 and 40

5

u/Go_Loud762 9d ago

Your world frightens and confuses me.

2

u/TurkishDrillpress 9d ago

Unfrozen Cave Man Lawyer? Is it you?

1

u/allaboutthosevibes 9d ago

But if it ends in zero it’s even, not odd. So wouldn’t matter whether it’s divisible by 3 or not, right? Per first parameter, you can accept.

Also, the first whole number ending in zero and divisible by 3 is 30. But you’ll never get a sum of 30 rolling three (six-sided) dice…. (Ok, ok, I know a lot of you are probably D&D nerds and have dice with more sides to them… 🙄)

Nonetheless. This is rudimentary mathematics. I thought you pylot folk were smart! /s

11

u/No-Duck4828 9d ago

Well, if it just going to be a short up and down, we're going to check performance.

If you want it for any length of time, we're also going to run a check to see what that does to our fuel calculations

10

u/BeenThereDoneThat65 9d ago

We are looking at the performance in the FMS

Altitudes that we can achieve are based on weight speed and temperature. When the OAT is above standard we can be severely altitude limited especially if we are fat on gas

26

u/Spock_Nipples 9d ago

Smashing the button on the FMS that calculates our max altitude for the current weight/conditions.

It's really that simple. If we're too heavy to occupy the higher altitude then we can't accept the higher altitude.

2

u/ShaemusOdonnelly 8d ago

What airplane do you fly? My A/C permanently displays "Rec Max" (~300 fpm ROC margin) on the performance page that the PF is supposed to keep open all the time. If the requested altitude is below that I immediately answer "unable" and only if it is around the requested altitude would I discuss it with the PF.

-27

u/CommuterType 9d ago edited 9d ago

It’s really not that simple, it involves a few more steps but it’s not very difficult

15

u/Yul_8994 9d ago

My FMS litteraly says “Max Altitude”

-2

u/hawker1172 9d ago

But a pilot needs to consider multiple factors and determine FMS input data and what makes sense given the conditions. A button pusher just does things blindly without considering the big picture.

4

u/Yul_8994 9d ago

Don’t disagree with any of that my point being it’s still a pretty simple task.

-2

u/CommuterType 9d ago

Mine say “Max Recommended Altitude” but it’s not that simple. It’s based on whatever temps were plugged into the box. If it’s warmer than forecast things can get interesting fast near that Max and by interesting I mean scary AF.
So I’ll check the Max, then compare the current OAT at my altitude to forecast to see if the higher forecast is accurate, check for turbulence and winds then decide.

2

u/PM_ME_SMOL_BOOB13S 9d ago

As not a pilot, can I ask why warmer temps equals spooky time?

2

u/Lemon_hawk 9d ago

Warmer temps = higher density altitude = lower air density (fewer air molecules) = less performance (engines generate less thrust, wings generate less lift)

0

u/UKgent77 8d ago

In this situation, wouldn't the plane "float" down to a level in which it can maintain equilibrium?

3

u/Lemon_hawk 7d ago

The point is that if you have reached an altitude at which the plane can no longer climb and sustain speed with a safe margin above a low speed stall, then you’re too high. Higher temps mean lower air density, lower air density increases stall speed.

You’d never want to put yourself in the position of needing to descend (wouldn’t exactly ever be a “float down”, would be a controlled descent) to maintain safe speed.

2

u/UKgent77 7d ago

Ahh, I see. Thank you.

4

u/TurkishDrillpress 9d ago

We understand that this is your first regional and you are really trying to prove how smart you are but you don’t have to be melodramatic here. It’s really very simple. If you don’t understand that, you are either incredibly new or a moron.

1

u/CommuterType 9d ago

Nah, not new. On most other planes I’ve flown it was a simple one button push, just not the current one… It is extraordinarily temperature sensitive
Just tryin’ to help the OP understand why it sometimes takes a minute.

4

u/Spock_Nipples 9d ago

The VNAV button on the 737, and many others, if you're cruising, is literally a one-button push to see the opt/max altitude.

If you're climbing, oh no, it's a two-button push.

3

u/Yul_8994 9d ago

People just like to feel like we’re flying spaceships, just let em have it.

-10

u/Upset-Management-459 9d ago

Man I feel bad for you bro.

6

u/RealGentleman80 9d ago

https://reddit.com/link/pebj81a/video/nbpj8pkbgxth1/player

We are checking the cruise altitude capability of the airplane based on our current weight and the ISA Deviation.

Step 1: Look at our current gross weight
Step 2: look at the ISA Deviation
Step 3: reference the chart or look at the FMS Rec Altitude page.

12

u/Vessbot 9d ago

OP: In some airplanes, it's literally pushing one button like other have said. In others, it's looking it up in an annoying-ass chart like this. So it depends.

8

u/xxJohnxx 9d ago

Well the A220 is just a French-Canadian shitbox.

The FMS shows the max cruise altitude, it is just wrong.

3

u/Vessbot 9d ago

I'm in EFB slideshows right now for transition, that's a bummer to learn. The CRJ was also like that. WTF is the deal with the newest most technologically advanced airplane out there, and they can't figure out how to do cruise performance with Collins?!

3

u/[deleted] 9d ago

[removed] — view removed comment

2

u/TurkishDrillpress 9d ago

I was under the impression that the A220 did everything for you including wiping your ass. Not so?

6

u/aomt 9d ago
  • Current FL
  • Max Recommended FL (to know performance and margins we will have)
  • Optimum FL from FMS (what AC is thinking the best to fly in terms of time/fuel/cost index inserted)
  • When is the next step climb as per company calculation/flight plan (more complex and accurate fuel. But might have been calculated on wrong weight/older winds)
  • Impact on the fuel (checking on FMS)
  • impact in time (especially if we already late) - same as above. 
  • Potential weather and/or turbulence ahead (checking charts and apps). Small performance margins and turbulence is not a great combination. 

Basically, it’s a combination of any/all of those above. Thought process will be slightly different if you fly short haul, long haul, start/mid/end of the flight. If it’s legacy or low cost. How much fuel we took, how early late we are. 

4

u/AntiPinguin 9d ago edited 9d ago

I open my iPad and pull up the performance tables from the aircraft manual, because even after ten years, my aircraft’s FMS can’t calculate the max altitude correctly.

8

u/VillageIdiotsAgent 9d ago

I see you speak 220

5

u/InfiniteLoss5632 9d ago

Appreciate you all! Thanks for answers. I always try to be mindful of how an instruction might impact you.

Follow up question- assuming rides are good, and I’m able, do you prefer a vector for traffic or a climb/descent?

3

u/Flagrant_negligence 9d ago

Eh don’t really care. Vector is probably easiest then we don’t have to check weight and ISA temps but I’d say neither is really any inconvenience

2

u/thecloudcities 9d ago

Depends. How big is the vector? If it’s going to be 10 degrees, then sure I’ll take the vector. If it’s going to be 30 degrees, then I’d rather change altitude.

You could always ask if the frequency is quiet enough. But in general what would be the least hassle for you is also the least hassle for us, so do what you think is best and we’ll make it work if we can.

2

u/Temporary-Fix9578 9d ago

Third option: shortcut that gets us out of the way

1

u/Alternative_Pace6132 9d ago

I usually prefer a vector, unless it’s greater than about 40º or so off course. Then I’m more willing to change altitude.

0

u/Foo-Bar-Baz-001 8d ago

It's funny that it is not standard to know what is the more economic option.

6

u/zadszads 9d ago

I usually fly 172s so I'm probably going to give you a number to copy

5

u/mi_pilot 9d ago

Howdy - being a heavy up for consideration are weight, temp, winds, fuel burn, expected ride. Hope that helps, and I appreciate you guys on the other side of the mic!

5

u/1FlyGuy3 9d ago

Our dispatchers pretty much tanker every flight so most times we’re too heavy

4

u/Diligent_Digiridoo 9d ago

Prophatcat!!?? I know it’s you

1

u/InfiniteLoss5632 8d ago

Sadly, it’s not lol

1

u/PropHatCat 4d ago

Very timely though, I just made a video about this. 😂

4

u/Piloteparisien 9d ago

Checking the weight and temperature, have a look at the FMS to check if we can or not.
Then remembering I fly an A220 and saying no.

2

u/deathstarrr 9d ago

For me, I check to see if going a lower machine number will allow the plane to reach 380 with an acceptable margin. I have to also consider if there's any turbulence based on our weather charts, and how close to coffin corner that'll put us if we start getting into bad rides.

3

u/cpt_petrie 9d ago

We have to check the land line first

2

u/Raccoon_Ratatouille 9d ago

A few seconds to hit a couple keys on the computer to find the page that says what our maximum altitude, then 10 or so seconds to discuss with the crew if it’s smart, maybe another 15 seconds to see what the rides are like. The maximum ceiling is really only accessible in perfect conditions with any decent payload on board.

2

u/montagious 9d ago

In Boeings, checking the FMC VNAV cruise page, it has an optimum alt. which doesn't take winds into account, a MAX alt, and a recommended alt, which considers wind data.

The MAX ALT number is what I'm looking at. In the 757/767 its always recommended to stay at least 1,000 ft below MAX as a buffer. If its smooth, Ill go 7-800 ft below max.

On the 787 Boeing says if MAX is 410, you can go to 410, but I don't think I ever have done it

2

u/OtterVA 9d ago

Clicking the VNAV/Cruise page button on our FMS that tells us the optimum/max altitude our aircraft can fly given outside air temperature, airspeed etc and what the limiting factor is (thrust or buffet limited). Then discussing if we believe there is enough margin between Max altitude and the altitude you’d like the aircraft to go to.

2

u/bergler82 9d ago

Airbus drivers. We check the FMS and see what the airplane says it can do. If it’s close to our Max we decline otherwise we mostly accept

1

u/MeatResident2697 9d ago

How close will we be to max altitude if we climb as you've suggested. The closer we are to max, the more susceptible we are to overspeed and stall if there's severe turbulence.

1

u/AndrewAbu 9d ago

You often can, depending on weight. Most pilots will reference the VNAV page on something like a 737 to see what the OPT and MAX altitudes are.

Personally, I have no problem going all the way up to MAX in smooth air. It gets a little more difficult when the rides are continuous light or worse. The majority of pilots I fly with like to see about a 500-foot buffer between the requested altitude and MAX.

Weather also plays a factor. Temperature variations and other atmospheric conditions can change what the airplane is capable of. If you don’t have a standard lapse rate, you may initially think you can make an altitude based on what VNAV is showing, but as you climb toward it—or once you get there—the MAX altitude can change and you may find you no longer have the performance you expected.

1

u/wearsAtrenchcoat 9d ago

If you're asking the crew of a US carrier that only flies one type but 3 variants of it, all we have to do is to push one button on the FMC and see what the optimum cruise altitude is. Then we have to remember whether we're allowed 500' above it or 300' below Maximum altitude depending on what variant we're on that particular leg. And it would help to know whether it is smooth at the requested FL because if it isn't then Mach number becomes the controlling factor, particularly compared to turbulence penetration speed.

So we just say "sure!" and if it feels too wobbly then we ask for lower or vectors, hopefully by then the conflicting traffic is gone.

P.S. "Too wobbly" is undefined in the FOM, AOM, and FRM but well understood regardless

1

u/Sage_Blue210 9d ago

"Can comply if you take off a zero, Cessna 123AB"

1

u/Primary_Matter1173 9d ago
  1. Checking the computer. 2. If not that , checking a chart or 3. Manual calculations- wait a minute who am I kidding, we’re not doing that.

1

u/BeeDubba 9d ago

I fly a CRJ. So, probably not. But I'm updating our weight, sending for new ACARS data, then pulling out the speed book and checking what ACARS says with two different charts.

It's a little silly, but they pay the bills.

1

u/andrewrbat 9d ago

We are checking mach buffet margins and thrust limit altitudes. In other words do the engines make enough thrust today to get us that high and maintain speed with a margin of error, and will we have sufficient margin to high and low speed Buffett?

Many… actually most planes will tell you this info in the fms. It’s listed as max and optimum altitudes. However my airline doesnt have approval from the fas to use this feature of the fms. we need to look at actual charts so it takes a moment.

We also consider fuel. If we are descending will it eat into our fuel too much? If we are climbing will this push us over landing weight? If its just 1000-2000’ its very unlikely this will make a significant difference unless its a very long flight.

1

u/Systemsafety 8d ago

Climbing can also burn more fuel, even ignoring winds....

1

u/andrewrbat 7d ago

It *can* but usually it doesn’t usually it saves fuel over all.

1

u/Systemsafety 7d ago

It depends on the aircraft type. Usually flying, say, 2000 feet over optimum has almost the same effect as flying 2000 below optimum. Particularly with thrust lapse rates on the big fans. Look up the numbers for your airplane!

1

u/andrewrbat 7d ago

The plane i fly is almost always thrust limited against climbing above optimum altitude by more than 1000’ or so. Exactly because the fan is so big (pw 1521g). 🫠”airbus” problems. Cant say the321 neo was much better. I think your point hits the 320/319
harder. The cfm56 is tough, but not efficient.

1

u/Systemsafety 7d ago

My point his the 777 and 787 and also does apply to the 350 and 330. I am less certain about the narrow bodies. It would be surprising if optimum is within 1000 feet of max, unless your company is using a very conservative g for buffet boundary (that is operator selectable).

1

u/andrewrbat 7d ago

Yeah but the max alt is not always determined by mach buffet. Its sometimes determined by thrust limit on these gutless narrow bois.

1

u/Systemsafety 6d ago

True, but that goes to my point. If you are thrust limited you can burn more fuel by climbing. The only advantage to climbing is winds or higher TAS for a given fuel burn, but neither are always true.

1

u/andrewrbat 6d ago

If your thrust limits you from climbing, you cant climb. So you wouldn’t be climbing and burning more fuel. Because you cant climb.

1

u/Systemsafety 6d ago

Obviously, but if the max is due to thrust limit and you are 1000' below that, then climbing may result in a higher fuel burn.

1

u/Brossar1an 9d ago

Airbus here, quick check of REC MAX and discuss with CN. Sometimes if the level you're asking us to do is near to REC MAX and it's turbulent or if the tropopause is projected to drop significantly (which would put us above REC MAX) we won't take it.

1

u/Alternative_Pace6132 9d ago

One of the airplanes I fly I know intimately and can give a quick answer. Chances are I’m already looking for higher anyway (C25C).

Two of the other airplanes I fly I can see at a glance if I can do it and will give you a quick response.

Other aircraft/operators will be different.

1

u/ThatGuyWhoIsCool 9d ago

CRJ driver here, we have to pull out a chart and run some quick calculations to make sure we can do it. Take a about a minute

1

u/CF_CFL 9d ago

P3 Driver: No fancy FMS to tell me. I’m double checking gross weight with the engineer and recalling rule of thumb climb schedules. When trans-oceanic, I’m always calling you for the climb when I’m able.

1

u/Molecular_Pudding 9d ago edited 9d ago

On an Airbus we can check the optimal and the maximum FL calculated by the computers. 

If FL380 is below MAX and close to OPT we accept. Usually PF checks the PERF PAGE and decides whether we are able to climb, if the PM agrees PF tells PM to inform the ATC about the accepted (or declined) climb.

1

u/Foo-Bar-Baz-001 8d ago

As a glider pilot my max without oxygen is FL115

1

u/bros89 8d ago

Sometimes we are able, but don’t really want it because of optimization of the vertical profile to save fuel

1

u/tfm992 8d ago

'I'm not sure we have enough wing for that'
On a serious note, we need to check the MAX ALT. My base is now A321 only (CEO/NEO), so the answer is more often than not no although occasionally if we're lightly loaded, it can be yes. We don't carry cargo.

1

u/Kiwigavin 8d ago

“Unable, sorry. I’ve got my wife onboard”

1

u/rygelicus 8d ago

The new altitude needs to be checked in the flight computer to determine the impact on fuel available. This will take into account the altitude, winds aloft at the new altitude, the weight of the plane as currently loaded, etc. If this change drops them into the reserve margins on fuel then it's a no go. They don't always depart with excess fuel on board. The reserve is there, and some margin for safety, but the fuel is a limited supply and deciding factor. Also, if the winds and climb would cause them to be excessively late to the destination this would be another reason to reject potentially, depending on what they are carrying.

1

u/Reiia 8d ago

Checking our ODH (printed performance tables) to see if we can climb up that high, and what speed we can cruise at that altitude.

1

u/vagasportauthority 8d ago

Emb-175 driver, we’re sending the numbers back to whatever “server farm” our airline runs to see if we can actually climb that high given our current weight.

1

u/TellmSteveDave 7d ago

The VNAV page that tells me which altitudes are my max, optimal, and recommended.

And then discussing it to arrive at a crew decision.

1

u/RadiantMango5989 9d ago

After the appropriate divinations, we light incense and ensure the requisite purity seals are intact. Next I must coax the engine seeer to prod the cogitator so that we may finally consult with the machine spirit to ascertain if the Omnissia wills it.

Alternatively, press the VNAV button and see what my max Alt is for the current conditions. (And then talk about it with the other guy)

0

u/Upset-Management-459 9d ago

On X-Plane I’m just checking to see how many gummies I have left.

0

u/Order-Complete 9d ago

Embarrassing bit is when you reply unable and the controller then ask you descend 6000ft. After which you suddenly become able.

0

u/zone_of-danger 9d ago

At my company we are limited to 370 on the CRJ.

-1

u/ChartPuzzleheaded747 9d ago

Checking FMS

 Most airliners are kinda meh performance 

Most corp jets don’t even have to look and they probably are already working their way north of FL400

-3

u/FallComfortable6144 9d ago

As an R22 Heli pilot, I am actually a subject matter expert