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Ryan

Active member
Joined
Mar 15, 2002
Posts
39
Just started my comm and have a few questions about throttle/prop/mixture control. BTW its in a Piper Arrow.

I understand having all three forward on T/O, this makes sense. I also understand throttle back to 24"/2400rpm at cruise and back on mixture to 10gpm.

Im a little confused though on landing. Throttle comes back to 15"( I get that) but prop to full forward? Is this done just in case of a go around?

Also, just say for instance my instructor becomes incapacitated(God forbid) and I cant remember what to do with the prop/mixture would I damage anything or get myself into trouble just by leaving everything full forward?

Im sure after a few more lessons this will all make sense Im just a little lost right now. Thanks
 
keep your prop rpms higher than your manifold pressure setting -- i.e. you don't want to overstress the engine by having a higher manifold setting than your prop setting.

and obviously you don't want your throttle full forward to land. The props full forward on landing is made in case of a go around. Also the full forward setting of the props will increase drag, and add a little to your descent as well.
 
Ryan said:
Im a little confused though on landing. Throttle comes back to 15"( I get that) but prop to full forward? Is this done just in case of a go around?
yes
Also, just say for instance my instructor becomes incapacitated(God forbid) and I cant remember what to do with the prop/mixture would I damage anything or get myself into trouble just by leaving everything full forward?
probably not.
Im sure after a few more lessons this will all make sense Im just a little lost right now. Thanks
good luck
 
Goose Egg said:
Just keep 'em both in the green arc. Probably wouldn't hurt you to look in the POH either.

-Goose

I agree with you 100% about looking in POH. Im in the nuclear power field and its all about procedural compliance. Im just one of those people that needs something explained to me and to understand it before I can remember it.
 
check out the performance section of the POH and look at the Manifold pressures vs. the RPM section. You will begin to see a relation between the two, and you will be good to go if you stick to what the manufact. says. As a rule of thumb, you do not want to "oversquare", as in lots of throttle/MP and little RPM's. You can relate this to a manual transmission of a vehicle. It will not be good to be in 4th gear, 10mph and full throttle.
Props go forward on landing in case of a go-around. They also act as a "brake" to help you slow down on final. Do you notice it when pushing the prop forward? If you were to lose an engine, you could pull the props out, and get a slightly further glide, also.
 
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I use all 3 full forward for takeoff, 25"/2500rpm for climbout, and 21"/2400rpms for cruise in the non t-tailed version..... If you look in the chart in the POH there are actually settings that have you keep the throttle on top of the prop, Its definitly harder on the engine though.
 
Ryan said:
would I damage anything or get myself into trouble just by leaving everything full forward?

Im sure after a few more lessons this will all make sense Im just a little lost right now. Thanks


Just don't jam everything forward quickly...I hear it's rough on the governor
 
I've heard the "oversquared" rule, which I guess is playing it safe if you don't know the airplane. Look in the POH though and I'm pretty sure the arrow has some power settings that or "oversquared." In a turbocharged a/c it can be way "oversquared." I the Navajo for instance I think we used 38'/2400 or something like that for climb, and 33'/2400 cruise.
 
The oversquare stuff you hear is not necesssarily true. It came from years ago and applied to radials. If you look at the poh on a seneca, arrow, baron, 206 etc etc you will see plenty of oversauare settings as these are fuel efficient. The props are forward on approaches because if you had to go around and jammed the throttles to the stops with the props at 2100 you'd blow the cylinders off, especially on turbocharged engines.
 
The "oversquare stuff" most certainly did not apply to radial engines, most all of which were turbocharged, supercharged, or turbocompound boosted. Most large radial engines are operated with manifold pressures well in excess of RPM values. There is NO correlation between manifold pressure and RPM.

keep your prop rpms higher than your manifold pressure setting -- i.e. you don't want to overstress the engine by having a higher manifold setting than your prop setting.

A myth, perpetuated by inexperienced flight instructors who don't know better.

Particularly in a normally aspirated engine, just how are you going to overboost it?? You can never develop more than barometric pressure...if you're operating above sea level, you're always developing less pressure in those cylinders than the engine was designed to handle.

The highest pressure you can develop with the engine running at full throttle is whatever you would develop with the engine shut off, no matter what position of the throttle. Think about that.
 
In our Arrow, it was recommended to wait until the base leg and/or <90 KIAS to put the prop full forward. (I know that it doesn't flow very well with the checklist)

Our power settings are slightly different..like almost everyone else, we used the 25 squared for climbout, mix back to 12GPH, but we used 20" and 2300 RPM for cruise.

This was for a 2003 Arrow...that 20-23 setting worked very well for eights on pylons, steep power turns, and lazy eights.

HELPFUL HINT (perhaps): the 20-23 setting gave me a gps GS readout of @95 knots...until I saw that, I was having a hell of a time with my 8's because of an artificially high pivotal altitude caused by using too high of an airspeed in the calculation.

Good luck with your commercial...I recently passed my checkride. It's much more enjoyable than instrument training.:)
 
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I was wondering when someone was going to chime in on this and set the record straight. Avbug is very correct. How about rather than using numbers that are mentioned on here, fly the aircraft according to the POH. As for most, if not all of the power settings on the Arrow, just flip down the sun visor, and the engine manufacturer has put them all there for you. A very quick and easy reference.
 
mayday1 said:
well, it's also what the FAA written exams (private, commercial) have the answer as..

Of which we all know that the FAA written exams are the final authority on every subject matter imaginable in regards to aviation.



Sense the sarcasm....
 
avbug said:
The "oversquare stuff" most certainly did not apply to radial engines, most all of which were turbocharged, supercharged, or turbocompound boosted. Most large radial engines are operated with manifold pressures well in excess of RPM values. There is NO correlation between manifold pressure and RPM.



A myth, perpetuated by inexperienced flight instructors who don't know better.

Particularly in a normally aspirated engine, just how are you going to overboost it?? You can never develop more than barometric pressure...if you're operating above sea level, you're always developing less pressure in those cylinders than the engine was designed to handle.

The highest pressure you can develop with the engine running at full throttle is whatever you would develop with the engine shut off, no matter what position of the throttle. Think about that.

Av Bug that is the most ignorant thing you could possibly say about an internal combustion engine. You are confusing manifold pressure with cylinder pressures. Yes manifold pressure is lower than atmospheric pressure because in a normally aspirated engine there is suction pulling the intake charge into the cylinder. However when the valves close and the cylinder starts its compression stroke the cylinder pressure is most definately MUCH higher than atmospheric pressure. If you open the throttle all the way and pack the biggest charge possible into the cylinder while restricting the rpm of the engine with the prop governor you will most certainly destroy the engine.

Yes most of the later radials were turbo and/or supercharged but the square power settings came from older engines which were sensitive to high CYLINDER pressures due to their designs (read early Wright engines). As most every one knows All turbocharged or supercharged engines do in fact run positive manifold pressures however the engines are designed to handle the higher cylinder pressures that result.

Trust me if you run too much cylinder pressure on any engine turbo or naturaly aspirated it will come apart.
 
Yellow Snow said:
Trust me if you run too much cylinder pressure on any engine turbo or naturaly aspirated it will come apart.

The point is, what is "too much?" Is it a value determined by the people who designed the engine, equipped with specialized equipment and years of engineering experience?

Or is it the relationship between a unit of length based on the length of a barley seed and a unit of time based on Earth's rotation (all in a number system based on the number of fingers humans have)? What does the latter have anything to do with anything? Ladies and gentlemen of the supposed of the jury, that does not make sense! If Chewbacca lives on Endor, you must acquit!

P.S. The poor little C-65 on the Taylorcraft L-2 I fly that makes only 2100 RPM on takeoff should have disintegrated into atoms long ago since it's run oversquare, no?
 
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Too much would be more than the settings recommended by the engine manufacturer. I never said that engines shouldn't be run oversquare. If you look at my original post I said they are more efficient when run that way and it is common to see oversquare settings on cruise charts. I did say however if you shove the throttles open with the prop governor set for a lower RPM you may grenade the engine. I have seen it. I was backseat on a training flight guy did a go-around and shoved the throttles forward before the props and cracked two cylinders, melted a valve, and blew a hole in a piston. That is overboosting.
 
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POH & GUMP. And when you fly turbo charged engines, you'll see higher MP values, of course. At least at cruise and above. And overboost can be a consideration on takeoff in those airplanes. When I got my Citation type, they at first had to get on me to unhestitatingly advance the thrust levers (non-flying pilot usually sets pre-calculated takeoff N-1, after Captain/flying pilot initially advances the levers, but I was advancing too gingerly at first) as I had been flying a Seneca II, where ramming the throttles full forward on takeoff can potentially overboost.
As for the normally aspirated Arrow, full forward for takeoff, but consult POH as to possibility of leaning mixture for high density altitude takeoffs.
In the Twin Otter, we called out "props to go" on our pre-landing checklist, because, as in the Arrow, advnacing the prop(s) early will result in an apparent surge of RPM. And why bother the passengers with that. Just some random comments.
 
Im a little confused though on landing. Throttle comes back to 15"( I get that) but prop to full forward? Is this done just in case of a go around?

Yeah, as has been mentioned, it's to be prepared for a go-around. Consider this, instead of automatically putting the prop control in at 15" MAP, how about putting the prop control forward when the RPM starts to dropa as you reduce power and slow down. This will prevent an increase on prop RPM.


and I cant remember what to do with the prop/mixture would I damage anything or get myself into trouble just by leaving everything full forward?

You'd be fine like that. I wouldn't embark on any long cross country flights like that, but then hopefuly you wouldn't embark on any long cross countries with your instructor incapacitated in the right seat.
 
Depending on the model of Arrow you're flying, you might have a 'avoid continuous operation' range marked on the tach. In my 1973 Arrow, it's 2100 to 2350 rpm, which means I either cruise at 2100 rpm or 2400 rpm. The POH cruise setting chart has several over-square settings in it. I most often cruise at 24/2400, 24/2100, or 21/2100 (75%, 65%, and 55% respectively).
 

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