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#21
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EDR wrote
Prior to the flight I calculated a weight and balance and appropriate speeds for the actual takeoff and landing weights. This is required in large airplanes (Vref, anyone) and perfectly reasonable in ANY airplane. All speeds change with weight. I think what you did was fine. On the other hand, lots of people don't do it, and simply use the full-gross speeds as published - and then maybe add a few knots. When we were on the ground, I asked him why he wanted the faster speeds. His answer was that this was not a new airplane, so the book values needed to be increased to allow for age related things that could affect the noted V-speeds. This is nonsense. If you have that much deformation of the wing, or that much weight that is unaccounted for, the plane is not airworthy. I can understand the reasoning for a student pilot I can understand the reasoning for a student pilot too - but I don't agree with it. Better to teach it right from the start. I am thinking in terms of performance as would apply to the Commercial standards. Hence, the reason for calculating the necessary speeds prior to flight. As I said - there's nothing wrong with your thinking. I will add that flying at the instructor's recommended speeds leads to float in the roundout and required more runway. No kidding... What is the perspective of the instructors in this group? My perspective is that at 1200 hours, you might want to start thinking about becoming an instructor yourself. What you experienced is, unfortunately, more the rule than the exception, and is the kind of nonsense that eventually prompted me to become an instructor. Michael |
#22
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#23
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"Snowbird" wrote in message
m... I'll be interested in what others say, but my take on this is: As far as I know, all the V-speeds you're talking about are a direct function of stall speed. For landing, true. For takeoff, not true. Vx and Vy, being the result of excess thrust and excess power (respectively), depend not just on the fixed characteristics of the airframe, but also the declining characteristics of the engine (and are not directly related to stall speed in any case). Now, that said, I agree with the others who point out that if the airplane's performance has changed enough that the published V speeds are not correct, then the airplane needs fixing. A slight reduction in engine power might be expected, but one large enough that Vx and Vy have changed enough for the pilot to notice warrants repair. And as you say, even the airframe can suffer during its lifetime in ways that might affect stall speed. But again, I'd say that if the stall speed has increased above the published speeds, the correct course of action is to fix the airplane. And generally speaking, I wouldn't expect the stall speed to change in a way noticeable to any but the most detail-oriented test pilot; changes in gross weight are going to be much more significant, and those mostly occur due to differences in loading (how many passengers, what weights, amount of fuel carried, etc.). 30 pounds of accumulated junk, while not unheard of, is still unusual, and even that much extra weight isn't going to produce a noticeable change on the airspeed indicator when stalling the airplane. I'm in complete agreement that it's foolish to add airspeed on landing. The extra speed might put you farther away from some problems (premature stall) but it's guaranteed to put to closer to other problems (long landing, porpoising, nose strike, etc.). Adding airspeed to compensate for gusts is reasonable, but adding airspeed just because you think the airplane is old is not, and is unsafe. Pete |
#24
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C J Campbell opined
I think the instructor's reasoning is faulty. Why would the stall speed increase as the airplane ages? If it has increased measurably, then something needs to be repaired. Bugs, dents, dirt would all change the shape of the wing. How much that would change the stall speed is an open question. Perhaps the FAA could be useful and do some research. I don't even teach student pilots to fly faster than necessary. It is too easy for a student to lose control on a fast approach, especially if he balloons or bounces. -ash Cthulhu for President! Why vote for a lesser evil? |
#25
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"EDR" wrote in message
... His answer was that this was not a new airplane, so the book values needed to be increased to allow for age related things that could affect the noted V-speeds. Our airplanes are nearly sixty years old. Age hasn't affected their stalls speed, but engine conversions, modifications, etc... do. All the instructor has to do is go up and stall the airplane in various configurations to get the actual numbers if he really thinks they are not as published. I fear the "more is better syndrome" has affected your CFI. A shame. Deb -- 1946 Luscombe 8A (His) 1948 Luscombe 8E (Hers) 1954 Cessna 195B, restoring (Ours) Jasper, Ga. (JZP) |
#26
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On Thu, 01 Jul 2004 00:09:18 GMT, EDR wrote:
What is the perspective of the instructors in this group? The instructor I fly with knows me. Why would he not hold me to Commercial standards? I'm not an instructor. But my perspective is that the person giving you the checkout is just not doing it correctly. Also, when you did your stall series as part of the checkout, it would be pretty simple to verify the actual vs book stall speeds. And when you did slow flight, it would be pretty simple to see how the a/c behaves at 1.1-1.3 Vso. Ron (EPM) (N5843Q, Mooney M20E) (CP, ASEL, ASES, IA) |
#27
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Nya - Nya! Mines a little heavier than yours. I am hauling around a 400
pound engine. Michelle G.R. Patterson III wrote: Michelle P wrote: Well then this instructor will be really un-comfortable in my airplane. Final is done at 70-65 MPH (61-56 Knots). Final landing is around 55 MPH (48 knots). ;-) Nya - Nya! My Maule's slower than your Maule. My Maule's slower than yours! :-) George Patterson None of us is as dumb as all of us. -- Michelle P ATP-ASEL, CP-AMEL, and AMT-A&P "Elisabeth" a Maule M-7-235B (no two are alike) Volunteer Pilot, Angel Flight Mid-Atlantic Volunteer Builder, Habitat for Humanity |
#28
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"Peter Duniho" wrote in message ...
"Snowbird" wrote in message m... I'll be interested in what others say, but my take on this is: As far as I know, all the V-speeds you're talking about are a direct function of stall speed. For landing, true. For takeoff, not true. Vx and Vy 'Scuse, Peter, but I said "all the V speeds you're talking about", not "all V-speeds". As best I can tell, the original poster was talking about Vr, and landing speed. I don't think he discussed being asked to climb out at a different speed than Vx or Vy, but in any event I think a better argument can be made for that practice in appropriate circumstances. Now, if you want to argue for Vr being a function of excess thrust and excess power -- go ahead. Cheers, Sydney |
#29
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#30
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"Snowbird" wrote in message
om... 'Scuse, Peter, but I said "all the V speeds you're talking about", not "all V-speeds". As best I can tell, the original poster was talking about Vr, and landing speed. Whatever. I find Vx and Vy to be perfectly relevant in this thread, even looking at only the first post. You want to be offended, go right ahead...wouldn't be the first time. |
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