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FL210 in a N/A M20E


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Wow!  I never even considered the ceiling of my M20E before.  Wonder what time-to-climb was.


Having done the altitude chamber a few times, my hypoxia onset in the low 20s is gradual yet noticeable, and ideally you'd notice in time to descend or fix your O2 problem.


What's the highest you've had your NA Mooney?  15.5 here.

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Quote: Swingin

Wow!  I never even considered the ceiling of my M20E before.  Wonder what time-to-climb was.

Having done the altitude chamber a few times, my hypoxia onset in the low 20s is gradual yet noticeable, and ideally you'd notice in time to descend or fix your O2 problem.

What's the highest you've had your NA Mooney?  15.5 here.

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FL 260 in a Rocket more than once.


FL170 in my J lowest alt available on MEAs west of Denver.


FL195 in a 182 RG Center gave me a block altitude and I rode the mountain wave over the front range into Denver.


Always with O2. Rocket was still climbing over 1000FPM at 26K.


Why did I buy a J ?


 

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I didn't expect the airplane to do as well as it did. I am not, however, the first guy to try this. The legendary Jonathan Paul, who flew his E non stop coast to coast, did a similar experiment some years ago and went to 230. One thing that's different is that my conclusion is that this altitude is perfectly viable for a long range flight in an NA mooney; Jonathan in his writing, as I recall, thought otherwise. The airplane was stable, not mushing along, the cht's were cool, etc. I think on the right kind of trip - eastbound and solo - you could get phenomenal range with a nice tailwind. 


Based on what I observed, I think the airplane can do 250 at std atmosphere and light weight. I stopped at 210 ot of abundance of caution as I did not have a pulse oximeter (I do now, and want to learn all about it).


For level cruise at 210, I got about 136ktas at between 6.5-7 gph. I made a big table with climb data and fuel to climb as well.


Anyway this is yet another thing I am planning to write about but I got outed :)


 


 

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Quote: Immelman

I didn't expect the airplane to do as well as it did. I am not, however, the first guy to try this. The legendary Jonathan Paul, who flew his E non stop coast to coast, did a similar experiment some years ago and went to 230. One thing that's different is that my conclusion is that this altitude is perfectly viable for a long range flight in an NA mooney; Jonathan in his writing, as I recall, thought otherwise. The airplane was stable, not mushing along, the cht's were cool, etc. I think on the right kind of trip - eastbound and solo - you could get phenomenal range with a nice tailwind. 

Based on what I observed, I think the airplane can do 250 at std atmosphere and light weight. I stopped at 210 ot of abundance of caution as I did not have a pulse oximeter (I do now, and want to learn all about it).

For level cruise at 210, I got about 136ktas at between 6.5-7 gph. I made a big table with climb data and fuel to climb as well.

Anyway this is yet another thing I am planning to write about but I got outed :)

 

 

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I hate to sound curmudgeonly, but I think flying a Mooney into the Flight Levels is, for most people, playing with fire.


Our O2 equipment is primitive (laughable by military/airline standards); and, I suspect most pilots haven't had altitude training (not to mention recurrent chamber rides).


And how quickly could you get down with, say, an inflight fire?


There's also the temptation to top wx you shouldn't be overflying--with no escape route.  


The USAF--with full masks and diluter-demand/100% O2 equipment maintained by pros and tested before each flight--restricts unpressurized flight to FL250, as do Part 121 regs for air carriers.  And this is for equipment that can generate descent rates greater than 4000 FPM.


I've never been accused of excessive caution in aviation matters, but I believe this is an area that warrants considerable trepidation.  


Scott(fromiowa) put it best with his laconic post:  No thank you. 


Happy New Year.

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FL260 in N231BG (79 "K" Rocket) and FL270 in N9154W (91 "M" Liquid Rocket).  The guys at Rocket used 54W as their test aircraft for the Liquid conversion and flew it to FL360 and said it was doing 1,000+ ft/min at that altitude.  If they had a better O2 system, they said they would have gone to FL045.  54W was an impressive Mooney (1 of 5 long bodies with a liquid-cooled TSIO 550L derated to 335 HP)! 

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Quote: xftrplt

I hate to sound curmudgeonly, but I think flying a Mooney into the Flight Levels is, for most people, playing with fire.

Our O2 equipment is primitive (laughable by military/airline standards); and, I suspect most pilots haven't had altitude training (not to mention recurrent chamber rides).

And how quickly could you get down with, say, an inflight fire?

There's also the temptation to top wx you shouldn't be overflying--with no escape route.

The USAF--with full masks and diluter-demand/100% O2 equipment maintained by pros and tested before each flight--restricts unpressurized flight to FL250, as do Part 121 regs for air carriers. And this is for equipment that can generate descent rates greater than 4000 FPM.

I've never been accused of excessive caution in aviation matters, but I believe this is an area that warrants considerable trepidation.

Scott(fromiowa) put it best with his laconic post: No thank you.

Happy New Year.

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Quote: xftrplt

I hate to sound curmudgeonly, but I think flying a Mooney into the Flight Levels is, for most people, playing with fire.

Our O2 equipment is primitive (laughable by military/airline standards); and, I suspect most pilots haven't had altitude training (not to mention recurrent chamber rides).

And how quickly could you get down with, say, an inflight fire?

There's also the temptation to top wx you shouldn't be overflying--with no escape route.  

The USAF--with full masks and diluter-demand/100% O2 equipment maintained by pros and tested before each flight--restricts unpressurized flight to FL250, as do Part 121 regs for air carriers.  And this is for equipment that can generate descent rates greater than 4000 FPM.

I've never been accused of excessive caution in aviation matters, but I believe this is an area that warrants considerable trepidation.  

Scott(fromiowa) put it best with his laconic post:  No thank you. 

Happy New Year.

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Quote: Shadrach

I tend to agree about the risks, but I would not judge someone who felt that they had adequately contemplated and prepared for those risks, unless it was revealed that they'd been negligent.

The rapid decent issue brings up other questions.

In the event of a fire, how quickly could you descend?  I personally would toss things like gear and flap speed limitations out the window as necessary.  I really would not care if I had to replace gear doors that had blown off. The president of the company said in 1961 that:

"the M20 airframe has been dived in excess of 330 mph and withstood static tests in excess of six G's without failure as well as withstanding the flutter test at over 200 mph."

I'm not saying that I'd be winding the airspeed up to 300mph. But if I needed to get down in case of fire, I think that -4000fpm or more might be possible if you knew there was a good chance that this would be the last time the aircraft flew.

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Quote: eldeano

I tend to agree about the risks, but I would not judge someone who felt that they had adequately contemplated and prepared for those risks, unless it was revealed that they'd been negligent.

The rapid decent issue brings up other questions.

In the event of a fire, how quickly could you descend?  I personally would toss things like gear and flap speed limitations out the window as necessary.  I really would not care if I had to replace gear doors that had blown off. The president of the company said in 1961 that:

"the M20 airframe has been dived in excess of 330 mph and withstood static tests in excess of six G's without failure as well as withstanding the flutter test at over 200 mph."

I'm not saying that I'd be winding the airspeed up to 300mph. But if I needed to get down in case of fire, I think that -4000fpm or more might be possible if you knew there was a good chance that this would be the last time the aircraft flew.

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