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Mach to Airspeed Transition

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Terry Hunter

Silence!
Joined
Nov 22, 2004
Posts
297
ATC Guru's:
When a controller says "maintain 300 knots during the transition", what is the transition point at which the controller is referring to? I presume at a certain altitude and above, that ATC wants speed in Mach?

Thanks.
TH
 
Basically hold a certian mach number until you get to 300 kts indicated and then hold 300 kts. Altitude will maybe be different each time.
 
Generally, aircraft that cruise at FL300 and above, and normally cruise at .75M and above have an indicated speed in the low to mid 200kt range. As they descend, they fly a constant Mach number, but the indicated speed increases. Once that Mach number matches a particular indicated speed, then that indicated speed is maintained.

The Mach number cannot be maintained at some point because it eventually will increase above the barber pole. There's no flying above that of course.

Typical indicated speeds that are maintained range from 280-340kt. If ATC wants a particular speed, so be it. Hope that helps.
 
FL240, the transition altitude between the highand low sectors. Above 240 Mach, below IAS
 
macdu is correct, between FL270 and FL280. Technically a mach number can be assigned lower than that, and an indicated airspeed higher than that, but it's usually only if they're climbing/descending into the preferred regime.

PilotYip, not sure where you get FL240 from but that's a bit low to be used as a "standard". There isn't an arbitrary transition altitude between high and low sectors.
 
Generally, aircraft that cruise at FL300 and above, and normally cruise at .75M and above have an indicated speed in the low to mid 200kt range. As they descend, they fly a constant Mach number, but the indicated speed increases. Once that Mach number matches a particular indicated speed, then that indicated speed is maintained.

The Mach number cannot be maintained at some point because it eventually will increase above the barber pole. There's no flying above that of course.

Typical indicated speeds that are maintained range from 280-340kt. If ATC wants a particular speed, so be it. Hope that helps.

What a terrific explanation...good job
 
Taught in Ground School

macdu is correct, between FL270 and FL280. Technically a mach number can be assigned lower than that, and an indicated airspeed higher than that, but it's usually only if they're climbing/descending into the preferred regime.

PilotYip, not sure where you get FL240 from but that's a bit low to be used as a "standard". There isn't an arbitrary transition altitude between high and low sectors.

http://www.faa.gov/library/manuals/aviation/instrument_procedures_handbook/media/CH-03.pdf

ATC issues speed adjustments if you are being radar controlled to achieve or maintain required or desired spacing. They express speed adjustments in terms of except that at or above FL 240 speeds may be expressed in terms of Mach numbers in 0.01 increments. The use of Mach numbers by ATC is restricted to turbojets. If complying with speed adjustments, pilots are expected to maintain that speed within plus or minus 10 knots or 0.02 Mach.
 
http://www.faa.gov/library/manuals/aviation/instrument_procedures_handbook/media/CH-03.pdf

ATC issues speed adjustments if you are being radar controlled to achieve or maintain required or desired spacing. They express speed adjustments in terms of except that at or above FL 240 speeds may be expressed in terms of Mach numbers in 0.01 increments. The use of Mach numbers by ATC is restricted to turbojets. If complying with speed adjustments, pilots are expected to maintain that speed within plus or minus 10 knots or 0.02 Mach.
Oops! The aircraft fueler gets smoked again! Thanks for playing!
 
PilotYip,

Did you read my first paragraph? I said exactly that, mach numbers can be assigned lower than FL270-280 (legally FL240 is the lowest, as you pointed out). The only point I questioned you on is that FL240 is a transition altitude between high and low altitude sectors, which is incorrect. There is no arbitrary altitude on that.

Your post only reinforces that fact that FL240 is the lowest a controller can assign a mach number ("may assign..." higher than that) which I never questioned.

Stupidpilot, if you think I got smoked, I'd love to hear you lecture me on this stuff. I'm glad you take my Avatar for face value!!
 
PilotYip,

Did you read my first paragraph? I said exactly that, mach numbers can be assigned lower than FL270-280 (legally FL240 is the lowest, as you pointed out). The only point I questioned you on is that FL240 is a transition altitude between high and low altitude sectors, which is incorrect. There is no arbitrary altitude on that.
Oh really? Is that why they always climb you to FL230, and then you get a freq change prior to climbing above that? I would define that as a transition. If you don't know what you're talking about don't chime in.
 
a litte touchy are we?

PilotYip,

Did you read my first paragraph? I said exactly that, mach numbers can be assigned lower than FL270-280 (legally FL240 is the lowest, as you pointed out). The only point I questioned you on is that FL240 is a transition altitude between high and low altitude sectors, which is incorrect. There is no arbitrary altitude on that.
you asked for a source, I posted one. Would you like me to post one on the boundry between the high and low sectors? Heck I remember glying with there were no hi or low sectors and they still had aural ranges in the SW US and I had to train on flying A and N sectors to get my insturment rating. I would love to see Avbug chime in on this one
 
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I think the subject has been covered, but we're also hearing correctly about two different subjects.

The issue of FL240 is one subject, for ATC phraseology with respect to assigning mach or indicated. It refers primarily to a general guideline as to whether ATC will give an assignment based on mach or indicated airspeed. In general, ATC will assign a mach speed above 240, and indicated below, but this isn't always the case, and this isn't the value to which the question posed by the original poster refers.

The issue of maintaining 300 KIAS at the transition doesn't refer to FL240. It's referring to riding mach during the descent until indicated airspeed reaches a predetermined value, then maintaining that value. In this case, 300 KIAS.

This is a common descent profile, and one I typically use. .84 M1 until transition, then 300 KIAS in the descent until 10'000' or any other restrictions apply.
 
The 230-240 HI/LOW sector boundary is probably the most common, but not the rule. e.g. Denver Center. Plenty of other exceptions as well.

As a rule of thumb, ATC assigns IAS FL280 and below and Mach FL290 and above.
 
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Stupidpilot, you obviously haven't flown to enough regions of the country, I could name NUMEROUS center sectors that go above/below FL240. There are plenty of areas where the separation from high/low sectors is FL280, and the ultra-highs start at FL330. But you knew that...right?

As avbug is saying, there are two questions at hand: when can Mach be assigned, and when do can pilots (or are they required) switch from Mach to Airspeed, vice versa. In the descent, FL270-280 seems pretty standard, but atc will often assign an airspeed at a higher altitude, knowing he's transitioning down and mach numbers may be assigned at FL240 and above, but are usually only assigned below FL280 if they plane is climbing higher (as I mentioned in post #8).

Randy, my only claim to you initially was that FL240 is a bit low to be used as a standard (which is true, most people seem to transition between FL270-280) and that while you are correct ATC "may" assign a mach above FL240 (which I never argued) I also am disagreeing that FL240 is a definitive transition between high and low altitude sectors, at there are tons of sectors out there throughout the NAS that have stratifications higher and lower than that.

Avbug is right on the money...I've never been assigned a mach number at FL240, even though the controller can technically use it....if he's spacing me at FL240 with someone at FL320, there will be a large discrepancy in the mach#'s. Anything below FL280 as a requested final, and you're gonna see a KIAS assigned, imho.
 
no right or wrong

I think the subject has been covered, but we're also hearing correctly about two different subjects.

The issue of FL240 is one subject, for ATC phraseology with respect to assigning mach or indicated. It refers primarily to a general guideline as to whether ATC will give an assignment based on mach or indicated airspeed. In general, ATC will assign a mach speed above 240, and indicated below, but this isn't always the case, and this isn't the value to which the question posed by the original poster refers.

The issue of maintaining 300 KIAS at the transition doesn't refer to FL240. It's referring to riding mach during the descent until indicated airspeed reaches a predetermined value, then maintaining that value. In this case, 300 KIAS.

This is a common descent profile, and one I typically use. .84 M1 until transition, then 300 KIAS in the descent until 10'000' or any other restrictions apply.
so basically everyone is right and it boils down to do what ATC instructs, BTW I am ont going ot change my ground school slide, but wil ldiscuss it thanks for all the inoput
 
Stupidpilot, you obviously haven't flown to enough regions of the country, I could name NUMEROUS center sectors that go above/below FL240. There are plenty of areas where the separation from high/low sectors is FL280, and the ultra-highs start at FL330. But you knew that...right?
Sure, I've flown all around the world in excess of 100X plus I've been flying for over 20 years. I guess I know nothing.
 
Just to throw it out there at FL280 to FL290, 290KIAS-300KIAS ~ .73M-.75M

Most aircraft flying above FL290 climb and descend in the 290 knot range and descend using the same. Above FL280 or FL290 Mach is used for speeds during normal operations. If you climb at 290KIAS and transition to .74M, you will likely see a transition near the FL280-FL290 range.

As for FL240, in my opinion that has nothing to do with transition speeds. It is my understanding, as well as other previous posters, that maintain 300 KIAS in the transition means that when your current Mach number equals 300 KIAS, while descending, you maintain 300 kts. Since most aircraft cruise.75M-.80m This just happens arouns FL280-FL290. Again depending on ISA
 

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