Not understanding AoA indicators...
#31
Gets Weekends Off
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Joined APC: Jan 2013
Posts: 834

Yes James, could you elaborate. In the meantime... I think lots of pilots confuse AOA with deck angle. They don't realize how small the AOA range is in comparison. Further, many students don't understand high speed stalls, or are never exposed to them.

#32

James, can you clarify the comparison you're making here? It's probably me - I'm having a hard time putting everything together - the AOA discussion in a descending turn vs level flight, ending up in trees at the end of the runway (approach end/departure end?) and the video.
A level turn, which requires higher power, may be done when a pilot is already fairly low on the downwind and base, so he's "saving" for final, but they often start to slow up, put in flaps, etc. This can create an excessively high AOA situation coupled with a turn. The stall warning may help, but this usually comes on pretty fast and some advance notice would be nice.
Then there was the issue of takeoff, when the airplane isn't climbing, but it is in the air and covering ground, there may not be a great appreciation as to where the AOA really is. The pilot may think they have some protection because they are moving fairly fast over the ground, but the AOA is so high and the induced drag so high that it's not going to end well. Maybe with this indication earlier one would fly it to a safe-spot earlier, avoiding trees later.
I think what I'm getting at is that we tend to not appreciate where the AOA is. Plenty of these attitudes are "normal" for flight, I've seen plenty of airplanes in almost level flight "attitude", yet their AOA is nearly off the scale (in terms of right about to stall). That's probably one of the bigger issues with that takeoff video, the plane "appeared" to be in a normal attitude, so the guy probably thought the AOA was "normal". It wasn't.
#33
Gets Weekends Off
Thread Starter
Joined APC: Jan 2013
Posts: 834

JNB, I get what you're saying for the most part; though if they are in the realms you speak of or are not flying the typical/standard profiles, they better know how to fly an airplane if venturing into those zones. Generally speaking, I don't think, a measurable portion... of newer pilots are satisfactorily familiar with those areas or really knowing their envelope, Etc. I could be wrong but it seemed the FAA started emphasizing LOC not long after the proliferation of TAA... If an instructor has roughly X amount of time to train a primary student and the TAA takes somewhat longer than a traditional 6 Pack, something has got to give. I think where it is giving is in the basic flying skills department. I think the FAA should increase the Min for Private Pilot by 10 Hrs. I know guys that have ferried jet airliners on some real raw data, less than a typical ferry kit. They got where they were going, because someone took the time to teach them to fly... If you want, probably, the best and most accurate summation of the state of basic flying skills; talk to the folks who specialize in tail wheel or seaplane ratings...
Last edited by Yoda2; 11-15-2014 at 05:05 PM. Reason: additional
#34

[QUOTE=rickair7777;1763166]Adding AoA indication to GA aircraft would be an unnecessary cost, and would further be pointless unless pilots are trained to use
Unlike say a fighter, there are no normal phases of flight in which the AoA data would be interesting for GA aircraft...comply with the AFM speeds and attitudes and you'll never get near the AoA limit except maybe in the flare.
Those are two of the stupidest sentences I've ever read. You really have no idea how AOA works or what it is trying to tell you. To you it's just a gauge with some pretty colors attached to it. Like USMC says, " I'd take a AOA gauge in every airplane that I've ever flown. In fact I plan on installing one in my personal Comanche at my next annual.
Unlike say a fighter, there are no normal phases of flight in which the AoA data would be interesting for GA aircraft...comply with the AFM speeds and attitudes and you'll never get near the AoA limit except maybe in the flare.
Those are two of the stupidest sentences I've ever read. You really have no idea how AOA works or what it is trying to tell you. To you it's just a gauge with some pretty colors attached to it. Like USMC says, " I'd take a AOA gauge in every airplane that I've ever flown. In fact I plan on installing one in my personal Comanche at my next annual.
#35

I've investigated several accidents where the pilots just didn't realize the AOA they were at. I think there are many accidents where this is the case. I don't think many pilots realize the radical difference in AOA between making a descending power (mostly) off turn descending to base and final vs. doing the same thing at the same airspeed and maintaining level flight. More than one accident I've investigated involved "some flight" but running into trees at the end of the runway. Here is a classic one: LiveLeak.com - (Must Watch!!) Plane crash video from inside cockpit
I think the perception is that due to the forward movement, the AOA must be "ok", but if you were to look at it, it'd be "screaming" the whole time.
Yes, cockpit clutter is an issue, not to mention really using the outside horizon as a pitch reference (rather than just saying "look outside, which can be equally useless as looking inside), but GA accident rates are in the spotlight these days. There's resistance to do anything at any level, whether it's increasing training hours, increasing standards, etc., but this will hopefully have a positive effect, and based many accidents that I've seen, it's likely.
I think the perception is that due to the forward movement, the AOA must be "ok", but if you were to look at it, it'd be "screaming" the whole time.
Yes, cockpit clutter is an issue, not to mention really using the outside horizon as a pitch reference (rather than just saying "look outside, which can be equally useless as looking inside), but GA accident rates are in the spotlight these days. There's resistance to do anything at any level, whether it's increasing training hours, increasing standards, etc., but this will hopefully have a positive effect, and based many accidents that I've seen, it's likely.
#36

I disagree with you're assessment that a level turn poses a higher potential threat than a descending turn. I think an AOA gauge would help a pilot in both scenarios, but IMO, more so to the descending turn pilot, especially if he accidentally strays into the high AOA regime.
What is the low power a good indicator of?
From my perspective, the final turn (i.e. a descending turn with power back) is notoriously dangerous because pilots fail to appreciate the lack of energy available in their aircraft. I’ll go out on the limb and suggest that more pilots have lost control of their aircraft in the final turn than on a level turn from downwind to base. Ask that pilot in the descending turn to level off or tighten his turn to prevent an overshoot and the AOA gauge will water his eyes. His relatively low AOA 3 seconds ago is going to shoot into the danger area far quicker without proper power and flying technique than his buddy in the level turn back up at pattern altitude.
I don’t get the “saving for final” term. Also, is he lower than he would be in the turn to final? Certainly, excessive AOA and a turn are not a good combination. However, adding a descent to those two is worse, IMO. Personally, if I had to choose between encountering a stall in a level turn versus a descending turn, I’ll take level every time. If you’re turning level at high AOA and you stall at pattern altitude, you have altitude to recover. If your AOA spikes in a descending turn, you don’t, plus you already have a significant sink rate you have to counter as well.
Are you saying there are scenarios in a GA aircraft that could result in an “almost level flight attitude” with AOA “nearly off the scales” and the pilot would be unaware were it not for an AOA gauge? I don’t have a huge amount of experience with those aircraft, so perhaps you can give me some of the scenarios you are referring to.
That takeoff was a classic density altitude accident. I think his problem was more of energy deficiency than simply high AOA (at least at first). I could be off base here, so correct me if I’m wrong. I assume he attained the normal takeoff/climb IAS when he got airborne. Because of the density altitude, his TAS was higher to produce the same IAS. With little to no excess thrust for his climb, in order to maintain that IAS and the usual AOA at such an extreme density altitude, he had to hold a lower pitch attitude and he was unable to climb. So, when they were muddling along in semi-level flight after takeoff, wouldn’t the AOA gauge (if he had one) have been indicating something close to normal? Assuming he was holding the IAS he wanted (even if that required a descent), wouldn’t he see the roughly the same AOA he saw every other flight at that IAS?
I think, what would have shown him he was in trouble would have been ANY attempt to turn, climb or just increase back pressure on the yoke when his airspeed began to decrease. Now he would have seen that AOA gauge spike into the danger zone faster and further than with those same inputs at lower density altitude – giving him a true understanding of how low on energy he really was. So, to your point, there were definitely times during that flight an AOA gauge would have clued him about how close to the edge he really was. I’m just not sure he would have had an AOA indication that was “not normal” for the entire flight.
What is the low power a good indicator of?
From my perspective, the final turn (i.e. a descending turn with power back) is notoriously dangerous because pilots fail to appreciate the lack of energy available in their aircraft. I’ll go out on the limb and suggest that more pilots have lost control of their aircraft in the final turn than on a level turn from downwind to base. Ask that pilot in the descending turn to level off or tighten his turn to prevent an overshoot and the AOA gauge will water his eyes. His relatively low AOA 3 seconds ago is going to shoot into the danger area far quicker without proper power and flying technique than his buddy in the level turn back up at pattern altitude.
A level turn, which requires higher power, may be done when a pilot is already fairly low on the downwind and base, so he's "saving" for final, but they often start to slow up, put in flaps, etc. This can create an excessively high AOA situation coupled with a turn. The stall warning may help, but this usually comes on pretty fast and some advance notice would be nice.
Then there was the issue of takeoff, when the airplane isn't climbing, but it is in the air and covering ground, there may not be a great appreciation as to where the AOA really is. The pilot may think they have some protection because they are moving fairly fast over the ground, but the AOA is so high and the induced drag so high that it's not going to end well. Maybe with this indication earlier one would fly it to a safe-spot earlier, avoiding trees later.
I think what I'm getting at is that we tend to not appreciate where the AOA is. Plenty of these attitudes are "normal" for flight, I've seen plenty of airplanes in almost level flight "attitude", yet their AOA is nearly off the scale (in terms of right about to stall). That's probably one of the bigger issues with that takeoff video, the plane "appeared" to be in a normal attitude, so the guy probably thought the AOA was "normal". It wasn't.
I think what I'm getting at is that we tend to not appreciate where the AOA is. Plenty of these attitudes are "normal" for flight, I've seen plenty of airplanes in almost level flight "attitude", yet their AOA is nearly off the scale (in terms of right about to stall). That's probably one of the bigger issues with that takeoff video, the plane "appeared" to be in a normal attitude, so the guy probably thought the AOA was "normal". It wasn't.
That takeoff was a classic density altitude accident. I think his problem was more of energy deficiency than simply high AOA (at least at first). I could be off base here, so correct me if I’m wrong. I assume he attained the normal takeoff/climb IAS when he got airborne. Because of the density altitude, his TAS was higher to produce the same IAS. With little to no excess thrust for his climb, in order to maintain that IAS and the usual AOA at such an extreme density altitude, he had to hold a lower pitch attitude and he was unable to climb. So, when they were muddling along in semi-level flight after takeoff, wouldn’t the AOA gauge (if he had one) have been indicating something close to normal? Assuming he was holding the IAS he wanted (even if that required a descent), wouldn’t he see the roughly the same AOA he saw every other flight at that IAS?
I think, what would have shown him he was in trouble would have been ANY attempt to turn, climb or just increase back pressure on the yoke when his airspeed began to decrease. Now he would have seen that AOA gauge spike into the danger zone faster and further than with those same inputs at lower density altitude – giving him a true understanding of how low on energy he really was. So, to your point, there were definitely times during that flight an AOA gauge would have clued him about how close to the edge he really was. I’m just not sure he would have had an AOA indication that was “not normal” for the entire flight.
Last edited by Adlerdriver; 11-15-2014 at 10:19 PM.
#37

Uh, wow.
JNB was simply saying you trade a good deal of potential to kinetic energy when descending. I'm sure you remember doing power-off approaches in the pattern and being surprised how much altitude you have to trade during the turn.
This is why the "impossible turn" is difficult for people to judge and people tend to attempt it when not advised.
Agree that high DA crash sequence started way before power was applied. An AOA gauge won't fix stupid.
JNB was simply saying you trade a good deal of potential to kinetic energy when descending. I'm sure you remember doing power-off approaches in the pattern and being surprised how much altitude you have to trade during the turn.
This is why the "impossible turn" is difficult for people to judge and people tend to attempt it when not advised.
Agree that high DA crash sequence started way before power was applied. An AOA gauge won't fix stupid.
#38

While I certainly understand considering the value proposition of retrofitting older aircraft....AoA can and should be as much of a "game changa" in GA as avionics-driven safety advances like synthetic vision, or even terrain & traffic awareness devices.
Do you "need" any of them in a piston-driven aircraft? Nope.
Do they provide tangible operational benefits in a variety of situations? Yes.
Do you need training in order to fully take advantage of them? Absolutely!
Do you "need" any of them in a piston-driven aircraft? Nope.
Do they provide tangible operational benefits in a variety of situations? Yes.
Do you need training in order to fully take advantage of them? Absolutely!
#39
Runs with scissors
Joined APC: Dec 2009
Position: Going to hell in a bucket, but enjoying the ride .
Posts: 7,643

Here's one for you guys with light airplanes:
Advanced Flight Systems
About the only place I found the AOA useful was in the final turn in the T38, and in a Scout I was flying for the Sheriff's Dept. where I had to do a lot of low speed steep turns, so the Sheriff in back could take pictures of the grow houses we were circling over.
The airplane had one of those little vanes on the strut called a "Bacon Saver" which was nothing more than a 2" wedge on a card with some red paint in the 'no go' zone.
Because it was mounted on the left strut, it was right in line with my sight as I turned final. I found I looked at that more than the airspeed indicator in the pattern, and certainly while doing the steep turns taking pictures.
But like someone said above, you can't fix stupid. Putting an AOA vane on all airplanes won't stop idiots from killing themselves in airplanes, especially light airplanes, if they try hard enough, they will always find a way!
I tried to find a link for the Bacon Saver, but can't, maybe they are out of business? It was a really low tech, cheap AOA with no electronics required, just bolt it on the strut, but it wouldn't have a place to mount on a low wing airplane, you need the wing strut to mount it on.
Advanced Flight Systems
About the only place I found the AOA useful was in the final turn in the T38, and in a Scout I was flying for the Sheriff's Dept. where I had to do a lot of low speed steep turns, so the Sheriff in back could take pictures of the grow houses we were circling over.
The airplane had one of those little vanes on the strut called a "Bacon Saver" which was nothing more than a 2" wedge on a card with some red paint in the 'no go' zone.
Because it was mounted on the left strut, it was right in line with my sight as I turned final. I found I looked at that more than the airspeed indicator in the pattern, and certainly while doing the steep turns taking pictures.
But like someone said above, you can't fix stupid. Putting an AOA vane on all airplanes won't stop idiots from killing themselves in airplanes, especially light airplanes, if they try hard enough, they will always find a way!
I tried to find a link for the Bacon Saver, but can't, maybe they are out of business? It was a really low tech, cheap AOA with no electronics required, just bolt it on the strut, but it wouldn't have a place to mount on a low wing airplane, you need the wing strut to mount it on.
#40

I disagree with you're assessment that a level turn poses a higher potential threat than a descending turn. I think an AOA gauge would help a pilot in both scenarios, but IMO, more so to the descending turn pilot, especially if he accidentally strays into the high AOA regime.
Here's what happens a lot around here:
People often scout out a landing spot just a few hundred feet above the ground, often with terrain considerations besides trees and brush. Then they start turning to "line up", but because they are already at such a low altitude, they don't descend, but they do start slowing up. This has resulted in more than one landing accident around here, but I think it's equally applicable to guys flying SR22s that get slow making these same turns, often not realizing they have to either get the nose down to speed back up or get rid of the excessive bank and coordination issues, but again, many of those have "spiraled" right in. In the 1st scenario, it's somewhat of a conscious decision to "stay high" and stray into the higher AOA region, but I wonder if those pilots really understand where their AOA is and how much higher it is than a normal descent. In the 2nd scenario, probably not quite as concious, as they get distracted by something like looking for traffic, configuration changes, etc, and don't notice the other warning signs, keeping the nose high while possibly staying fixated on the runway (ever see how a runway is like a magnet for a pilot's head on base? I've witnessed plenty of attitude deviations just due to this)
The other scenario is climbing out, letting the nose get too high, not noticing the decay in airspeed, and a similar result.
From my perspective, the final turn (i.e. a descending turn with power back) is notoriously dangerous because pilots fail to appreciate the lack of energy available in their aircraft. I’ll go out on the limb and suggest that more pilots have lost control of their aircraft in the final turn than on a level turn from downwind to base. Ask that pilot in the descending turn to level off or tighten his turn to prevent an overshoot and the AOA gauge will water his eyes. His relatively low AOA 3 seconds ago is going to shoot into the danger area far quicker without proper power and flying technique than his buddy in the level turn back up at pattern altitude.
I don’t get the “saving for final” term. Also, is he lower than he would be in the turn to final?
Certainly, excessive AOA and a turn are not a good combination. However, adding a descent to those two is worse, IMO.
Personally, if I had to choose between encountering a stall in a level turn versus a descending turn, I’ll take level every time. If you’re turning level at high AOA and you stall at pattern altitude, you have altitude to recover. If your AOA spikes in a descending turn, you don’t, plus you already have a significant sink rate you have to counter as well.
Are you saying there are scenarios in a GA aircraft that could result in an “almost level flight attitude” with AOA “nearly off the scales” and the pilot would be unaware were it not for an AOA gauge? I don’t have a huge amount of experience with those aircraft, so perhaps you can give me some of the scenarios you are referring to.
That takeoff was a classic density altitude accident. I think his problem was more of energy deficiency than simply high AOA (at least at first). I could be off base here, so correct me if I’m wrong. I assume he attained the normal takeoff/climb IAS when he got airborne. Because of the density altitude, his TAS was higher to produce the same IAS. With little to no excess thrust for his climb, in order to maintain that IAS and the usual AOA at such an extreme density altitude, he had to hold a lower pitch attitude and he was unable to climb. So, when they were muddling along in semi-level flight after takeoff, wouldn’t the AOA gauge (if he had one) have been indicating something close to normal? Assuming he was holding the IAS he wanted (even if that required a descent), wouldn’t he see the roughly the same AOA he saw every other flight at that IAS?[/FONT]
Yes, lots of things went wrong there, is it easier for us to re-evaluate every pilot that's gotten a license? Or require FADEC on every airplane? Or require a manifest and weight and balance be transmitted for every GA flight? No, those things are not practical, so the regulators try to see where a practical improvement can be made in safety.
I think, what would have shown him he was in trouble would have been ANY attempt to turn, climb or just increase back pressure on the yoke when his airspeed began to decrease.
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