poadeleted20
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...about embarassing foul-ups.Considering how it can be done in many types with little to no altitude loss - I'm sure it has happened countless times. It's not like people go around bragging.

...about embarassing foul-ups.Considering how it can be done in many types with little to no altitude loss - I'm sure it has happened countless times. It's not like people go around bragging.

Considering how it can be done in many types with little to no altitude loss - I'm sure it has happened countless times. It's not like people go around bragging.
In any event, the accident files suggest that the problem is not one of people not noticing the throttle has retarded itself until the stall has occurred. And regardless of that, read the title of the thread again -- the PTS is what we're discussing here.
Without the time to look, I think that you'll find a large chunk of such incidents happen at high density altitudes, which means partial power, and can be verified by reading the NTSB reports.Got a hard citation for that first claim? I've never seen anything in the accident record other than "failed to maintain airspeed / departure stall". There aren't categories for "departure stall where engine was definitely producing full power" and "departure stall where engine was producing 65%".
There's usually a "engine was producing power determined by metallurgy" and maybe if it survived "throttle was found in wide open position"... sometimes.
But I think you'll be hard-pressed to prove that the accident record shows a hard difference between known power outputs.
I'm the one who brought up the point about creeping throttles, and more to the point, lower than normal power being produced.
The PTS is teaching you to recognize and pitch, but a good instructor will also teach that the throttle hand goes forward simultaneously to make sure that thing up front is firewalled
(we'll leave engines with throttle handles that can put them above safe operating limits out if this for a minute, but there's an Air Florida crew dead from frozen instrumentation who'd be alive today if they shoved theirs up).
You keep saying it's an exercise to teach about recognizing a stall when no more power is available. If that's the case, I say that particular change to the PTS should include wording to the effect that the student needs to confirm that they really are.
Recognizing is but one step. Pitch is the next. Third is "why?".
How many people know roughly how many inches of MP their engine will put out up here at my home base before they start that takeoff roll, for example? How would that person know if they werent producing full power? How would they know to abort before lifting off on a hot day?
(There's multiple ways to tell, not just MP. My point here is the change to saying "full stall" is fine by me, but we've all seen folks who thought they were producing full power on a high DA takeoff who left the mixture full rich. The few who get it together and figure it out while in the middle of "recognizing" that they're on the edge of a stall after liftoff when they can't get out of ground-effect, survive.
The rest go into the record as a "departure stall" accident because they're not trained in that third step... figure out why it doesn't have enough power. The PTS doesn't require it. And it does get very little attention at lower altitude airports.
If the stall is fully developed, you're going to lose at least a little altitude, right?
Without the time to look, I think that you'll find a large chunk of such incidents happen at high density altitudes, which means partial power, and can be verified by reading the NTSB reports.
Already went through a bunch, and did not find a single one where a throttle slippage was involved.
That makes it speculation on your part, and nothing more. I'll stick with actual recorded data.Not being a pain, but do they specifically say when it wasn't a factor?
I still contend they're wont be reports of it because it's rarely possible to know for sure -- unless there's a specific notation that the position of the control was checked.
That makes it speculation on your part, and nothing more. I'll stick with actual recorded data.
I can list the likely most common causes for stalls in VMC (or IMC with a rated, current pilot) without referring to any statisticalWhich is inconclusive about the topic. The data shows stalls. It doesn't show the reason why.
There's no added risk in asking students to verbalize "power full, and confirmed" at each power-on stall event. If teaching that procedure at high altitude there's no reason in the world to leave out the troubleshooting step. Omitting it will likely end up with a pilot who'll have about a 50/50 chance of brain-lock when it eventually happens to them.
BTW- Since we discussed it earlier, does anyone know someone who got into a FULL power on departure stall and recovered before hitting the ground?
Considering how it can be done in many types with little to no altitude loss - I'm sure it has happened countless times. It's not like people go around bragging.
...about embarassing foul-ups.
How many people know roughly how many inches of MP their engine will put out up here at my home base before they start that takeoff roll, for example? How would that person know if they werent producing full power? How would they know to abort before lifting off on a hot day?
(There's multiple ways to tell, not just MP. My point here is the change to saying "full stall" is fine by me, but we've all seen folks who thought they were producing full power on a high DA takeoff who left the mixture full rich. The few who get it together and figure it out while in the middle of "recognizing" that they're on the edge of a stall after liftoff when they can't get out of ground-effect, survive.
Blind adherence to exactly the letter of the PTS can lead to holes in knowledge and procedures. "Everyone knows" you should check the power if you're slow and sinking and don't expect to be, doesn't cut it for every pilot. Some need to be shown that the pitch stall recovery is just the first step in saving their own butt. Further actions are required after the pitch to ensure survival in some cases.
Why not teach them?
Perhaps if the CFI were able to limit the application of throttle (e.g. by blocking further advance with a hand) opening the throttle would be a good addition to the standard departure stall technique. The problem I see with just letting the trainee go to full power during the recovery of a departure stall is that the resulting surge of thrust isn't likely to be there when the real event occurs at high DA and or when faced with rapidly approaching trees off the end of the runway. It's pretty clear to me that the PTS defined departure stall recovery is intended to ram home the facts that power is not required to break a stall and that additional power is likely to be unavailable at that time. And since the approach stall recovery does include going to WOT I suspect that most pilots are going to react to any stall with throttle as well as elevator. It's not like they're going to analyze the situation to determine if it more closely matches the departure or approach scenario and react differently.

I suspect that most pilots are going to react to any stall with throttle as well as elevator. It's not like they're going to analyze the situation to determine if it more closely matches the departure or approach scenario and react differently.
I hold no such suspicions after AF447 or Colgan, at this point I don't trust the ability for pilots to be screened for ability to react.
Well I don't wait THAT long. Geez.
To resurrect an old thread....
Does anyone have a one pager cheat sheet of the new PTS standards?
SNIP...raise the nose wheel early and smooth, hold the attitude and let it fly off. No reason to even look at the ASI. No reason to stay on the ground longer than necessary. ...SNIP
Depends on the wing. Some airplanes will not respond well to this technique. Mooney and most jets come to mind. All this will do is lengthen the T/O roll.