Tom-D
Taxi to Parking
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Tom-D
New term. I have my pencil ready. Can you clarify that one?
It's a term use to describe the process of keeping power on until you have runway under you.
New term. I have my pencil ready. Can you clarify that one?
There are many of us pilots that were taught to close the throttle at the down wind to base turn and leave it closed for landing.
It's certainly true for the space shuttle orbiters.
15 deg glideslope was SOP for those.
Very expensive bricks. And EVERY landing was a "glide" (well, a controlled fall with a flare at the end).
It's a term use to describe the process of keeping power on until you have runway under you.
New term. I have my pencil ready. Can you clarify that one?
I'm confused, I think we both made a minor mistake. The best glide angle is 79 mph on the 140 and 85 knots or almost 100 mph on the Cherokee 235. mph. According to Piper.org
__________________Originally Posted by Tom-D
There are many of us pilots that were taught to close the throttle at the down wind to base turn and leave it closed for landing.
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And are still being taught as evidenced by what my CFI tells me to do. Control speed with elevator and alt. with rpm [if necessary].
The definition of "making power" is to be adding energy. It is simple to measure.... flip the mags off and tell me what you feel.
There was I time I felt that way, too, but folks just keep doing the same old dumb things again and again. After 40 years and almost 10,000 hours, I've concluded that there are just some forms of stupidity our training and testing processes cannot detect and eliminate.Something that I just cannot understand...Pilots running out of fuel.
Before I was even able to ride a bicycle, it was burned into my brain to always know how much fuel you have. My grandfather was and is OCD about this. I could never grasp how others would even chance running out of fuel.
I'd be interested to see the source of that statement.I read that high wing aircraft have more fuel out landings.
I'd like to see you do that in, say, a Baron. Or a King Air. Or an F-16.There are many of us pilots that were taught to close the throttle at the down wind to base turn and leave it closed for landing.
Always heard that the glide ratio of the F4 Phantom was similar to that of a brick.
I am assuming from TheTraveler's posts that he is referring to single-engine planes. If there is a non-turboprop single with a feathering prop I am unaware of it.
Bob
And, FWIW, the rate of landing accidents has dropped significantly since we stopped teaching the 180 power-off approach as "normal" in favor of the partial-power stabilized VFR approach, even in light singles.
Only the turboprop C-models, not the piston powered A's and B's.T-34's had a full feathering prop.
Engine failure is not a "normal" procedure.Because engines dont fail?
I teach emergency procedures, too. But I teach the partial power stabilized VFR approach recommended by the FAA as the "normal" way to approach a landing.I still teach it, chit happens, be prepared
Only the turboprop C-models, not the piston powered A's and B's.
Then they were modified after the Navy sold them. The ones in VT-1 were not full feathering, and yes, even though I was an NFO, I went through VT-1 in 1973.The -B's I flew had them.
even though I was an NFO, I went through VT-1 in 1973.
After 40 years and almost 10,000 hours, I've concluded
The prop is real draggy when not turning.
As noted, a windmilling prop will create more drag than one that is fully stopped because it takes energy to rotate the internal components of the engine. The only energy you have in this scenario is the potential energy that your altitude provides for you. The windmilling engine will use up some of this energy and you won't glide as far as you would have if the propeller were stopped.
Darwin Conrad's Mooney Missile conversion, I believe puts one of the C414 engines, with full feathering, up front.....I am assuming from TheTraveler's posts that he is referring to single-engine planes. If there is a non-turboprop single with a feathering prop I am unaware of it.
Bob
Actually, they all did. And no T-34B left the factory with a full-feathering prop.As most NFO's of that time did.
The problem with that is if you have an oil pressure loss, the prop feathers and you're at zero thrust, without the option of keeping the engine running as long as possible, an option most SE pilots would probably want to have.Darwin Conrad's Mooney Missile conversion, I believe puts one of the C414 engines, with full feathering, up front.....
The problem with that is if you have an oil pressure loss, the prop feathers and you're at zero thrust, without the option of keeping the engine running as long as possible, an option most SE pilots would probably want to have.
The problem with that is if you have an oil pressure loss, the prop feathers and you're at zero thrust, without the option of keeping the engine running as long as possible, an option most SE pilots would probably want to have.
Have you ever flown a single? Do you tell your SE students to shut down the engine immediately on loss of oil pressure? And why do you think every production piston single has a prop which goes low pitch rather than high if oil pressure is lost? Could it be that some power is better than none when you only have one engine to start with? And that trading what's left of your only engine in order to make it to a suitable field might be better than having a salvageable engine at the crash site?And how long do you suppose an engine with zero oil pressure will continue to operate before a seizure and no possibility of a feather much less selecting low pitch?
Have you ever flown a twin? Do you suggest to your multi engine students to keep an engine running with no oil pressure?
You missed the point. An idling engine is still adding thrust or energy to the airplane. They is a difference in performance in gliding an airplane idling and an airplane with a dead engine.
Have you ever flown a single? Do you tell your SE students to shut down the engine immediately on loss of oil pressure? And why do you think every production piston single has a prop which goes low pitch rather than high if oil pressure is lost? Could it be that some power is better than none when you only have one engine to start with? And that trading what's left of your only engine in order to make it to a suitable field might be better than having a salvageable engine at the crash site?
Or did you think the Mooney Missile is a twin?
Its been a while and surely a corner case, but I believe the Seebee by Republic offered a featherable and reversible prop. Allowing one to back out of a dockage, if one were so brave.
That's a good point, in my opinion a fair assumption, and is completely related to the post I just made about fuel.
Can you elaborate? Meaning that...typical training aircraft are not as suitable for this?
As long as occupants are not significantly damaged, I don't care about the plane.
And how long do you suppose an engine with zero oil pressure will continue to operate before a seizure and no possibility of a feather much less selecting low pitch?
Have you ever flown a twin? Do you suggest to your multi engine students to keep an engine running with no oil pressure?
The problem with that is if you have an oil pressure loss, the prop feathers and you're at zero thrust, without the option of keeping the engine running as long as possible, an option most SE pilots would probably want to have.
Reverse taxiing cautiously, it is not excessively risky when executed properly.
Can you name 1 light civil twin that requires hydraulic/electrical power to fly safely?
I can tell that this is something that bothers you. Yes, even jets can land without power. Several years ago, Neal Armstrong set some time-to-climb records in a Lear 28. In order to minimize their weight, they only carried enough fuel to get to their desired altitude. Their engines flamed out and they glided back and did it again, and again and again. Think about the space shuttle or do a google search on the "Gimli Glider". I would also recommend that you, as part of your training, go take a few flights in a glider. You'll quickly figure out that (excuse the paraphrasing) "Engine? We don't need no stinking engine." As the others have pointed out, it's all about training and proficiency. It's a skill that you will develop before solo and demonstrate many times during your training. It's also perishable, so you'll want to get periodic recurrent training along the way. Have fun and enjoy the process.This came up in a conversation recently, and it's something that I have been extremely curious of...landing without engine power. Engine failure, out of fuel, or whatever the reason, as far as I've been told, it should technically be possible to glide, and land, any airplane without power.
What I would like to know is not in theory, but in practice and reality, how difficult is this to do?
I'm sure the debate could go on and on about where to actually land the aircraft if there isn't an airport or landing strip nearby. There's also the conversation about doing this at night, hoping that dark spot isn't a lake. I don't want to avoid those debatable variants, but the main question, making a few assumptions...
1. Controls are still intact, but engine has failed
2. It's daytime
3. You are in a relatively flat area, with few obstructions
4. You are in very reasonable weather
-How practical, and how difficult is it to actually land the plane without engine power?
-Does this differ with high-wing vs. low-wing?
-If you have done this, has it been a scary situation, trying to keep control without power? Or a calm, quiet situation, just kind of minding your own business, and gliding back down to land?
I am really interested in hearing what everyone says about this.
This is going to sound like a stupid question but is there such a thing as an electrically controlled pitch mechanism for props? I have never heard of nor seen one but that doesn't mean they don't exist.
The subject was the Mooney Missile, a single. Twins would be another story. That is why piston twins are built with props that feather on loss of oil pressure, and piston singles are built with props that go low pitch. In fact it was the use on that single of an engine/prop off a twin on that triggered my comment, which I thought was clearly limited to SE airplanes, although in retrospect, I suppose some might have thought "SE" stood for "spare engine."The only twin I knew of that was dependent upon hydraulic power and electrical power for safe flight was the E-2, it has a feature that prevents the last prop to be feathered to not go below 25 degrees of blade pitch. That will keep one engine turning to provide rotation of the Alternator and both hydraulic system pumps.
All other recip. twins I've dealt with (S2/E1) that require hydraulic power to fly, you can feather one, but not both.
Can you name 1 light civil twin that requires hydraulic/electrical power to fly safely?
the TC-4C did not need either to fly safe.
There are probably some light jets that do, But I'm not familiar with them.
I can tell that this is something that bothers you. Yes, even jets can land without power.