Optimum altitude
Posted: Thu Oct 05, 2017 10:23 am
Hello Guys and Gals
I am currently working alongside Rich at Checkmate Aviation trying to build a good checklist for our beloved birds. Initially, they won't have every model with all the engine/wing/prop/etc. variances but we're working on a standardized template that can easily be modified with the pertinent information and can even be customized to your liking.
I realize most of you have been flying your Maule for a while and probably have the checklists memorized and don't need one, but I have found my memory sometime formats its self without my permission so a checklist on-hand can take the guess work out of it. Also, It may help the future new Maule owners to give them a baseline to work from.
On to my real question:
Our Flight Manual / POH's state "Optimum Altitude" regarding fuel burn vs RPM vs Manifold Pressure.
Does anyone know of a documented "Optimum Altitude" for any or all of our models??
If not, What do you consider an "Optimum Altitude" for best performance/fuel burn/Ground speed/etc.
I understand the potential variables affecting this altitude number are probably endless and it will be somewhat different for every single aircraft. I'm just trying to get an idea of range and see if anyone has done any real world dynamic testing in search of this data.
Thanks!
I am currently working alongside Rich at Checkmate Aviation trying to build a good checklist for our beloved birds. Initially, they won't have every model with all the engine/wing/prop/etc. variances but we're working on a standardized template that can easily be modified with the pertinent information and can even be customized to your liking.
I realize most of you have been flying your Maule for a while and probably have the checklists memorized and don't need one, but I have found my memory sometime formats its self without my permission so a checklist on-hand can take the guess work out of it. Also, It may help the future new Maule owners to give them a baseline to work from.
On to my real question:
Our Flight Manual / POH's state "Optimum Altitude" regarding fuel burn vs RPM vs Manifold Pressure.
Does anyone know of a documented "Optimum Altitude" for any or all of our models??
If not, What do you consider an "Optimum Altitude" for best performance/fuel burn/Ground speed/etc.
I understand the potential variables affecting this altitude number are probably endless and it will be somewhat different for every single aircraft. I'm just trying to get an idea of range and see if anyone has done any real world dynamic testing in search of this data.
Thanks!