Jaybird180
Final Approach
Hello all
First Post. Visited here many times (lots of search engine hits).
I am an adult student pilot (looking forward to check-ride day), thinking about the future purchase of my “ideal” plane and thought I should get a sanity check and a few suggestions from the community. I have plenty of time to make this decision.
My ideal plane is fast and can transport me and my family up to 500 miles non-stop and performs well in Cross-Country IFR conditions. It is a certified- production design that is reasonably inexpensive to operate and maintain. I can find safe, clean, well-maintained examples for well-under $150K before any negotiating and bang-for-the-buck makes it more attractive. High and Low wing types are equal in this regard, but I seem to be more attracted to low-wing types.
I’m thinking a normally aspirated single is preferred due to added complexity and operating, maintenance costs. I’m also concerned that there may not be as much value for me based near sea-level and without a pressurized cabin, I just don’t know if I’ll spend much time in the Flight Levels after I get my Instrument Rating. I’m also thinking that it should be something that I would like to fly 10+ years, transfer, and its new caretaker could do the same. I know very little about how composite designs fare in this area.
I’ve invested many hours into reading about the Mooney M20, and identified the M20J as my baseline for comparison except one thing that nags me. I haven’t been able to obtain reliable data on its true useful load.
I think my ideal plane should be able to carry up to 850lbs + fuel for the occasion where I need to depart from a Class-D airport with myself and 3 other high density adults and their baggage. From what I can ascertain of the M20J, (1100lb Max Gross weight???) , it falls just shy of being able to do 500 miles on even minimum fuel (160ktas cruise + reserves = 244-264lbs fuel @ 10.5-11GPH @75%). Some sources suggest it will, some say it won’t, hence the useful load data question marks.
I’m hoping for comments, suggestions and learning resources to allow me to re-evaluate some of my assumptions and get pointed in the right direction.
First Post. Visited here many times (lots of search engine hits).
I am an adult student pilot (looking forward to check-ride day), thinking about the future purchase of my “ideal” plane and thought I should get a sanity check and a few suggestions from the community. I have plenty of time to make this decision.
My ideal plane is fast and can transport me and my family up to 500 miles non-stop and performs well in Cross-Country IFR conditions. It is a certified- production design that is reasonably inexpensive to operate and maintain. I can find safe, clean, well-maintained examples for well-under $150K before any negotiating and bang-for-the-buck makes it more attractive. High and Low wing types are equal in this regard, but I seem to be more attracted to low-wing types.
I’m thinking a normally aspirated single is preferred due to added complexity and operating, maintenance costs. I’m also concerned that there may not be as much value for me based near sea-level and without a pressurized cabin, I just don’t know if I’ll spend much time in the Flight Levels after I get my Instrument Rating. I’m also thinking that it should be something that I would like to fly 10+ years, transfer, and its new caretaker could do the same. I know very little about how composite designs fare in this area.
I’ve invested many hours into reading about the Mooney M20, and identified the M20J as my baseline for comparison except one thing that nags me. I haven’t been able to obtain reliable data on its true useful load.
I think my ideal plane should be able to carry up to 850lbs + fuel for the occasion where I need to depart from a Class-D airport with myself and 3 other high density adults and their baggage. From what I can ascertain of the M20J, (1100lb Max Gross weight???) , it falls just shy of being able to do 500 miles on even minimum fuel (160ktas cruise + reserves = 244-264lbs fuel @ 10.5-11GPH @75%). Some sources suggest it will, some say it won’t, hence the useful load data question marks.
I’m hoping for comments, suggestions and learning resources to allow me to re-evaluate some of my assumptions and get pointed in the right direction.