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#11
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"Jay Honeck" wrote:
Here I had assumed that she was holding it down too long before rotation -- but it had now become apparent that she (and I) were in fact rotating prematurely. Wind conditions were calm, temperatures were in the 80s, humidity was very high, and a ground fog was developing as we landed. Otherwise, everything was done according to Hoyle, with 2 notches of flaps set for take-off. Usually the plane just "flies itself off" the runway in this configuration -- but not that night. Conditions of flight were fairly unusual, for us -- the back seat was empty, no wind, high humidity, fairly light on fuel -- so I suppose it was just pilot error. Is there a reason why you *shouldn't* rotate at the published rotation speed? ... more precisely, is there a reason why continuing the takeoff roll beyond the published rotation speed before lifting off is not safe (assuming you have enough runway ahead of you)? In the C152, rotating at the published rotation speed nearly always produced nice, smooth takeoffs. I recently bought a Shinn/Varga (low wing, tandem, stick, trike), and in early flights, rotating at the published rotation speed often produced a couple of seconds of "can't decide if I'm really ready to take off and start climbing" hesitancy on the part of the airplane (and yes, everything checked out during run-up). We then tried letting it continue the takeoff roll beyond published rotation speed, not really "rotating", but pulling back just enough to take the weight off the nosewheel and letting it lift off in its own time. Presto, all the takeoffs have been nice and smooth ever since, and once it lifts off, there is NO hesitation to begin the climb. How far beyond published rotation speed it lifts off, using this technique, varies depending on temp, humidity and weight. Other than runway length concerns, is there a reason why this technique would not be preferable to abruptly rotating at the published rotation speed? |
#12
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Other than runway length concerns, is there a reason why this technique
would not be preferable to abruptly rotating at the published rotation speed? Particularly with low wing airplanes, this can produce a wheelbarrowing effect where your mains get light, and even lift off, but you are holding the nosewheel on the ground. Not good for the nose gear and any crosswind gust could produce some rather interesting and dangerous effects. Jim |
#13
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In article ,
"Jim Burns" wrote: Other than runway length concerns, is there a reason why this technique would not be preferable to abruptly rotating at the published rotation speed? Particularly with low wing airplanes, this can produce a wheelbarrowing effect where your mains get light, and even lift off, but you are holding the nosewheel on the ground. Not good for the nose gear and any crosswind gust could produce some rather interesting and dangerous effects. With two notches of flaps and two adults in the front seats, your center of lift was way aft and your center of gravity was way forward. Think about it. |
#14
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Jim Burns wrote:
Other than runway length concerns, is there a reason why this technique would not be preferable to abruptly rotating at the published rotation speed? Particularly with low wing airplanes, this can produce a wheelbarrowing effect where your mains get light, and even lift off, but you are holding the nosewheel on the ground. Not good for the nose gear and any crosswind gust could produce some rather interesting and dangerous effects. I think you missread what he wrote: not rotating is a far cry from holding it down. When I accelerate in a Cherokee, I hold the yoke neutral until I'm ready to fly, then rotate and fly off immediately. In a Cessna, I ease the yoke back once I'm at or beyond stall speed and let it fly off when it's ready.... rolling on the mains only until it is. I would agree holding it down is a poor practice. -- Mortimer Schnerd, RN VE |
#15
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What indicated airspeed do you normally rotate at? (no real answer, just
curious) Take off with the twin requires us to hold it onto the runway until 80mph, we definately do not want to rotate prematurely in case of an engine failure. We usually start to rotate (and that's not really what we're doing -- more like applying mild back pressure) around 70 mph -- but that's not a hard and fast figure. It all depends on "feel", in my experience -- which, in turn, is based on weight, wind, temperature, etc. -- Jay Honeck Iowa City, IA Pathfinder N56993 www.AlexisParkInn.com "Your Aviation Destination" |
#16
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![]() "Jay Honeck" wrote We usually start to rotate (and that's not really what we're doing -- more like applying mild back pressure) around 70 mph -- but that's not a hard and fast figure. It all depends on "feel", in my experience -- which, in turn, is based on weight, wind, temperature, etc. Ground fog forms because the ground is cooling the air near it (due to radiational cooling) faster than the air further from it. You already knew that, though. MY guess what happen, is that after you started to rotate, the warmer air above started getting pushed down into the cooler air, warmed it up, (or you got into the warmer air) gave you less lift than the cool ground air, then you started not lifting so good. Just a guess, though. -- Jim in NC |
#17
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It might be worth considering the possibility that something about the
rigging has changed. An extra-careful preflight or even a trip to the shop may be in order. If someone has backed a truck into it while it was parked, the damage might not be immediately obvious. Everything checked out normally before flight. I've had dragging brakes produce interesting effects when breaking ground. Low tire pressure changes things pretty dramatically in our plane. Take-off performance suffers a surprising amount, for one thing. -- Jay Honeck Iowa City, IA Pathfinder N56993 www.AlexisParkInn.com "Your Aviation Destination" |
#18
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My first thought was that perhaps you have less power than you usually do,
causing you to hang at the rotation speed a little longer than usual. Did you rotate by the same point as you normally do? Other things: Mag check normal? Normal RPM on takeoff run? Yep, everything checked out during preflight and run-up. The JPI EDM-700 engine analyzer showed 6 good bars (meaning all six cylinders were firing normally) manifold pressure was 26-27, and RPM was nailed right at 2650 or so at full throttle. -- Jay Honeck Iowa City, IA Pathfinder N56993 www.AlexisParkInn.com "Your Aviation Destination" |
#19
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MY guess what happen, is that after you started to rotate, the warmer air
above started getting pushed down into the cooler air, warmed it up, (or you got into the warmer air) gave you less lift than the cool ground air, then you started not lifting so good. Just a guess, though. Man, that would require a layer just a few feet thick -- is that possible? Actually, I know it is, as I've seen it at altitude. I suppose it can form close to the ground, too, in a calm wind. Strange how I can study weather in college, I can observe it carefully for years, and I can spend so much time in the air -- and yet not understand it very well at all. -- Jay Honeck Iowa City, IA Pathfinder N56993 www.AlexisParkInn.com "Your Aviation Destination" |
#20
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Jim Burns wrote:
Particularly with low wing airplanes, this can produce a wheelbarrowing effect where your mains get light, and even lift off, but you are holding the nosewheel on the ground. Not good for the nose gear and any crosswind gust could produce some rather interesting and dangerous effects. "Mortimer Schnerd, RN" wrote: I think you missread what he wrote: not rotating is a far cry from holding it down. When I accelerate in a Cherokee, I hold the yoke neutral until I'm ready to fly, then rotate and fly off immediately. In a Cessna, I ease the yoke back once I'm at or beyond stall speed and let it fly off when it's ready.... rolling on the mains only until it is. He did misread what *she* wrote. I was not referring to "holding it down", I meant pulling back *just enough* to get the weight off the nosewheel (not enough to pull the nosewheel up), letting the nosewheel and the airplane lift off the runway when it's ready, as you said, rolling on the mains until it does. Is there a reason (other than runway length) NOT to do this vs. abruptly rotating it off the runway at the published rotation speed? The airplane performs better (no second or two of hesitation before beginning the climb) with the former than with the latter technique ... yet some pull the airplane up when they see the ASI reach the published rotation speed even if the airplane doesn't act ready to begin climbing. What say you? |
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