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AR15.COM
5/1/2025 10:29:54 AM EDT
MSFS 2024 Max 8 has the N2 over 100% during much of Level Change climb.  N1 is in the high 80's to low 90's % during Level Change climb.

Using Vertical Speed and setting it to keep N2 below 100% results in slow climb rates.

Is this the actual situation in real aircraft?  Thanks in advance.

5/1/2025 10:36:29 AM EDT
[#1]
It's not uncommon for climb power to be above 100%.
The Marines I have seen around the world have the cleanest bodies, the filthiest minds, the highest morale, and the lowest morals of any group of animals I have ever seen. --Eleanor Roosevelt
5/2/2025 2:06:12 AM EDT
[#2]
My plane gets over 104 % in a full power climb.
5/2/2025 2:07:03 AM EDT
[#3]
Quote History
Originally Posted By bags533:
It's not uncommon for climb power to be above 100%.
View Quote



Thanks
5/2/2025 2:08:00 AM EDT
[#4]
Quote History
Originally Posted By The_Emu:
My plane gets over 104 % in a full power climb.
View Quote


Thank you
5/5/2025 8:24:24 PM EDT
[#5]
T-1A jayhawk regularly would give you numbers above 100% if you pushed the throttles to the firewall.  All it refers to is the rated speed of that section of the engine.  You can, easily in fact, exceed rated turbine speed if you give it enough juice.
5/5/2025 9:52:07 PM EDT
[#6]
Crank it up to 11!
"I will leave when I have your wounded." MAJ Kelly
5/5/2025 10:10:12 PM EDT
[#7]
Normal
5/21/2025 11:51:28 AM EDT
[Last Edit: Senoj][Edited] [#8]
N1/N2 is determined (really estimated) as 100% of a semi-arbitrary RPM while the engine is on the drawing board.

On a Williams FJ44, 100% N1 was 17,245 and N2 41,200 RPM.

Later, during certification testing, it's very common to arrive at acceptable power settings with N1s above 100%.  On the FJ44, I remember takeoff power settings as high as 104.4% N1 if I recall, but the max allowable N2 was 99.3%.

Designing, testing and certifying a turbine engine still have some guesswork involved.  I've often wondered why they don't go back and change the N1/N2 numbers during the course of the process, so that N1 and N2 max limits are 100% when they're done, but neither Williams nor Pratt & Whitney seem to do so.

The PWC engines I fly now are substantially derated (which is cool, because it means they can carry their SL thrust up to a higher altitude than one that isn't, and have longer TBO and theoretically better reliability compared to one that's not), and don't approach 100% N1/N2, normally hovering in the 80's and occasionally (based on temperature/altitude) having a place on the chart that gets into the 90's.

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