You misspelled POA. Which means of course you do something randomly different every time.I’m all for trying new techniques but I’m pretty by the book and usually just default to whatever the POH says.
You misspelled POA. Which means of course you do something randomly different every time.I’m all for trying new techniques but I’m pretty by the book and usually just default to whatever the POH says.
This guy seemed pretty responsible. I doubt if he teaches things like that to primary students. It was just a rental checkout for me, I have a commercial certificateI’m all for trying new techniques but I’m pretty by the book and usually just default to whatever the POH says.
Go fly Vx without flaps and again with. Choose which is the better tool for rapid climbs. Cessna guys should try it at 30 and 40* flaps, too. Very educational.
Where are there trees at the end of the runway out here?Do that at our altitude and you’ll probably get to see how crashworthy the airframe is into the trees at the end of the runway.
Where are there trees at the end of the runway out here?
Do that at our altitude and you’ll probably get to see how crashworthy the airframe is into the trees at the end of the runway.
Why’s that?
Never have departed to the north there...LXV. North end.
Never have departed to the north there...
Definitely.who do you think writes the PoH.....marketeers?
You mean ‘modern Cessna’.Cessna's never going to tell you that you can reduce your takeoff roll if you save flap deployment towards the end because they're worried that increasing pilot workload will cause an accident, and that a jury will find it's their fault for making things too complicated for the pilot.
Procedures and speeds specified in the POH are often listed for reasons other than performance. Cessna's never going to tell you that you can reduce your takeoff roll if you save flap deployment towards the end because they're worried that increasing pilot workload will cause an accident, and that a jury will find it's their fault for making things too complicated for the pilot. But people who have tried it find that it does indeed result in a shorter takeoff in most aircraft.
Best glide speed is another one to be careful of. In most planes, the speed listed is not best L/D (furthest glide), and it's not minimum sink speed (longest time in the air). Both of those speeds will change with the weight of the airplane, and few manufacturers list different engine out glide speeds for different weights.
They're also not going to tell you that your longest glide can be accomplished by diving for ground effect and using the excess energy to stretch your glide where there's less induced drag, but it works quite well.
You mean ‘modern Cessna’.
The short field takeoff technique described in the owner’s manual for the 1948 Cessna actually tells you to start the takeoff roll with zero flaps and as you approach takeoff speed, put the flaps full (Johnson bar).
And that’s in a tailwheel airplane.
Sorry I left it out. That was the 1948 Cessna 170. Flaps very small, and created a lot more lift than the drag of the later 170s.That's interesting! Which model? I wonder if they did that for all models, even though the flaps in the 140 are far less effective than the bigger models.
The oldest Cessna manual I've seen was for the early era of electric flaps, mid-late 60s. It was around the time of Superbowl I, so I guess that makes it the "modern" era
I wonder if it's a procedure that was taken out when they changed to first style of electric flaps, where you have to turn the flaps off when they've moved as far as you want them to, rather than set-and-forget like the modern ones. Putting the flaps out late is quick and easy with the Johnson bar or with the newest ones, but not a good idea
That makes me want to ask another question. I know this is a logically sound statement, but, if this is true, then why do you have to trim up for each notch of flaps in a mooney?
5 whole mph. woooo!
Definitely true, but again, with twice as much runway as needed, does that matter? Maybe getting off the ground asap is a good idea for other reasons...
how exactly?
If you dive for ground effect around here, well, the ground effect you’re going to get is not gonna buff out. Unless you’re flying over a flat, relatively smooth surface, how in the world does your last sentence make sense? I’m imagining someone losing an engine at 3000’ agl and deciding to dive to ground effect. How steep of a dive? Should it be configured clean so that there’s a chance of exceeding Vne? What’s the proper technique for this so I can practice it next time I’m out? (I think there’s definitely a reason that, as you said, “(t)hey’re also not going to tell you that your longest glide can be accomplished by diving for ground effect...”)
I guess it depends on the airplane. In a Cessna 120, I never bothered with flaps at any time.
Was this somewhere on short approach where he ducked down and made it to the strip? Or was he 10 miles from the field at 3K and he dove into ground effect and buzzed along fields? Genuinely curious. I also imagine winds and lift could be different lower down. My brother in law had a few outfield landings up in Canada and there are a lot of sailplane tricks they had up their sleeves that I'm not sure necessarily all translate to powered flight (wasn't Gimli glider and Hudson pilots glider pilots?)My late uncle did it on his commercial glider checkride after losing some lift in the late afternoon
I was taught that ground effect happens at about an altitude that is half of the aircraft's wingspan.. so in most GA planes that's around 10-15' off the runway.. which makes sense, as that's where you can feel the plane behave differentlygetting down into ground effect
The drag profile of an aircraft is not constant, unless the airspeed stays constant (as you allude), so, honest question then:This isn't one of those theory things that can only be duplicated in lab conditions; it's a pretty straightforward application of the science. Your total energy state is the combination of your kinetic energy (determined by your speed) and your potential energy (altitude). Assuming you keep your airspeed constant, your total energy is only affected by drag. So you get yourself into the region of substantially reduced drag quickly, and you get to keep that potential much longer.
how do you keep your airspeed constant and yet quickly get yourself into a reduced drag environment, IE, ground effect? If you "dive" down to ground effect you'll naturally pick up airspeed, no? The reason I mentioned "drag dynamics" is because it is well know that total drag increases with parasitic drag as speed goes up. Yes, induced drag goes down, but at a lower rate, while parasite drag goes up at an increase rate. So if you "dive down" into ground effect you've dramatically increased your drag coefficient and sacrificed a ton of energy by doing so, and hence glide distance, just to get down to a lower altitude, IE, closer to terrain and obstructions, and have also reduced your glide range. The unknown to me is, how much does ground effect reduce your total drag? Perhaps it reduced a ton, and so the tradeoff is in your favor.. but this doesn't really pass the sniff test to me. Maybe glider dynamics are different.. but this sounds a little bit like the whole "getting up on step" thing with cruise speed, were people overshoot their altitude by 100' feet then dive down to get a bump in airspeed (not to open another Pandora's box though!)Assuming you keep your airspeed constant, your total energy is only affected by drag. So you get yourself into the region of substantially reduced drag quickly
So, are there glider pilots cruising along for miles at 20' off the ground? How do the dynamics work? Do they crank it up to Vne then dart over the landscape?
Two miles! Man. I went up a few times but it's been years. Over due!
My plane stalls at 72 when clean. I’m not going to rotate at 70. Even at 75 I was getting stall horn every takeoff, so I settled on 80.I’m back to using flaps as prescribed in the POH. I did not like staying on the ground the extra 5-10mph it takes to get off without them. A lot of bouncing around that definitely felt less safe than getting off quicker. Also, the stall horn went off a lot more than I’d like if there was gusty wind, albeit with plenty of buffer still, and only very early before the effects of raising the gear could be attained.
I can see a definite difference, and after comparing both, much prefer a flaps takeoff in my mooney.
Can you clarify this statement? I rotate at the same speed all the time, flaps or no, 70 mph. The book says 65-75, so I compromise and use 70. May go to 75 if the wind is gusty, or I'm heavy on a shorter field [with Takeoff flaps]. But the overwhelming majority of my takeoffs are Flaps Up. If I'm near gross, I may go to 75 mph, depending on how it feels and looks.
--first 7 years at obstructed 3000' field
--last 3 years on open-at-one-end/cliff-at-the-other 3200' field
--1½ years in between getting spoiled at wide open 5000' field with multiple approaches
My plane stalls at 72 when clean. I’m not going to rotate at 70. Even at 75 I was getting stall horn every takeoff, so I settled on 80.
I can only tell you my experience. I wasn’t comfortable with rotating earlier and having the stall horn blaring at me while still in ground effect.My previous Tiger stalled and rotated at 60mph with an 88mph Vx and 100 Vy. I don't hold aircraft on the ground trying to gain speed, I let the plane rotate when ready (which was always 60), and stayed in ground effect/leveled until near mid 80's then the climb.
I can only tell you my experience. I wasn’t comfortable with rotating earlier and having the stall horn blaring at me while still in ground effect.
My previous Tiger stalled and rotated at 60mph with an 88mph Vx and 100 Vy. I don't hold aircraft on the ground trying to gain speed, I let the plane rotate when ready (which was always 60), and stayed in ground effect/leveled until near mid 80's then the climb.