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On Wed, 22 Oct 2003 01:52:18 GMT, Tom Pappano wrote
in Message-Id: : Front seat guys were seriously banged up, but they also were not wearing seat belts. Three rear seat pax, also unbelted, received minor injuries. Life may be "like a box of chocolates for some folks," but the laws of physics are seldom broken. :-) Anyone who doesn't faithfully use lap and shoulder belts, is a damn fool. |
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David Megginson wrote:
Confirm this with someone who knows better, but from what I've heard, you need only about 20 ft of deceleration to have a chance of surviving a landing in a Cherokee/172/Musketeer-class aircraft. That suggests that setting down in a developed area (an unoccupied part, preferably) might be survivable. Tom Pappano wrote: I would think, in a "172" or similar class airplane, if you have your seatbelts and shoulder harnesses on, flaps down, minimum controllable airspeed, and *maintain control*, you should be able to land on (or into) almost anything and survive with minor injury. I know of two landings on top of houses that were both "walk aways". I've heard this too. And it makes sense to me. And I would shoot for trees if that were the best option and I had time and altitude to pick the spot. The problem with the area surrounding PDK is that it is so densely developed one would be hard pressed, especially in a low altitude emergency situation, to pick an appropriate and unoccupied place. I personally would not deliberatly shoot for a house; can't tell who's inside. The biggest issue for me around PDK is powerlines. There are multiple multilane roads on three sides of PDK, but even if they weren't *always* occupied by heavy traffic, they are criss-crossed with power lines every few hundred feet. Snag a powerline, and you've lost control, at the very least. Take a look at www.terraserver.com; search for Lat: 33.873596938 and Lon: -84.30184815. All the trees you see surrounding the airport are in someone's (tiny) yard, except for a stretch just off the end of 27 (the least used runway). There's a golf course off west, but if you can glide to that, you're high enough to get back to the airport; plus it's at 90 degrees to the main runways anyway. Like I said, I figure in this particular place, the best way to increase my chances of survival is get as much altitude within the shortest distance as possible. -- David Hill david at hillREMOVETHISfamily.org Sautee-Nacoochee, GA, USA filters, they're not just for coffee anymore The following needn't bother to reply, you are filtered: Juan E Jimenez, Barnyard BOb, Larry Smith, John Nada |
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True on all counts...
BT "dennis" wrote in message k.net... The glider has a couple of things going for it. Power planes are seldom over 12:1 glide ratio and it is achieved at a higher speed than the glider. This means that the power plane covers about half the THEORETICAL glide distance of the glider. Said loudly. The speed ratio between the wind and the aircraft is a factor. A given wind speed will be a higher percentage of the glider's best glide speed and will result in a greater advantage to it's L/D downwind compared to a power plane with the same wind. The wind also works to advantage for the glider's on tow part by decreasing the distance that it covers on climb, compared to a power plane at typical climb speeds. Finally, for some ancient and illogical reason, power plane standard procedure is to stay on center line of the runway for climbout. It's considered bad form to put yourself in a safer position for a turn back to the field. The exception is an IFR departure. They typically maintain runway heading. Lots of luck making a turn back under IFR. You subtract reaction time, reconfiguration time, screw around trying to get the thing to run, and it is very, very unlikely that a power plane will get back to the runway at any time during their climb out. Unless it is a long runway and you started from the end. In article afjlb.63635$La.24804@fed1read02, "BTIZ" wrote: Most gliders can do this and the pilots train to that standard.. Departure problems below 200ft AGL, tow plane power problems.. rope breaks or tow hook failures.. and the idea is to land straight ahead as quickly as possible and get stopped. Above 200ft AGL (which most glider/tow combinations can get to about 3000ft after start of take off roll), if the rope breaks, tow plane says.. GET OFF!!.. the glider pilot can pitch down for airspeed and begin a turn back to the departure runway.. land opposite the direction of take off and have enough energy to roll back to the starting point. A nice tow pilot will allow the tow to "Drift down wind the cross wind" on climb out, so if something does happen the glider can turn into the wind when returning to the runway.. turning away from the wind can push the glider to far away (tailwind on base) and make returning to the runway more difficult. This maneuver is part of the practical test standards, though most DE's will wait until 300ft or higher and most CFIGs will review the procedure on BFRs. Our "Training glider" has a L/d of 23-1. Schweizer 2-33. BT "Harold" wrote in message . .. If a small single engine plane can out-climb its engine-out glide ratio from take off through the top of climb point, wouldn't it follow that it can always theoretically make it back to the departure airport in the event of engine failure ? Assuming straight out departure, no wind, and the altitude loss in the 180 turnback is offset by the runway portion you didn't use. If my best glide is 85 KTAS and it loses 700 fpm at that speed, shouldn't I be guaranteed I can make it back if I climb at 84 KTAS and 701 fpm ? |
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![]() Harold wrote: If a small single engine plane can out-climb its engine-out glide ratio from take off through the top of climb point, wouldn't it follow that it can always theoretically make it back to the departure airport in the event of engine failure ? Sure, except that you have to get turned around first. There is always some altitude below which you will not be able to return to the airport. This tends to be between 600 and 900' AGL in a typical powered aircraft. George Patterson To a pilot, altitude is like money - it is possible that having too much could prove embarassing, but having too little is always fatal. |
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George.. where do you get all these neat quotes for your sig line
BT "G.R. Patterson III" wrote in message ... Harold wrote: If a small single engine plane can out-climb its engine-out glide ratio from take off through the top of climb point, wouldn't it follow that it can always theoretically make it back to the departure airport in the event of engine failure ? Sure, except that you have to get turned around first. There is always some altitude below which you will not be able to return to the airport. This tends to be between 600 and 900' AGL in a typical powered aircraft. George Patterson To a pilot, altitude is like money - it is possible that having too much could prove embarassing, but having too little is always fatal. |
#6
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![]() BTIZ wrote: George.. where do you get all these neat quotes for your sig line This particular one comes from "To War in a Stringbag", by Commander Lamb, RN. IIRC, he was relating an incident early in the war in which he was scud-running in Scotland. When I run into something in my reading that I like, I change my sig file for a while. When I get tired of it, I'll change it to one of my favorites, such as this one. George Patterson To a pilot, altitude is like money - it is possible that having too much could prove embarassing, but having too little is always fatal. |
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"Harold" wrote:
If a small single engine plane can out-climb its engine-out glide ratio from take off through the top of climb point, wouldn't it follow that it can always theoretically make it back to the departure airport in the event of engine failure ? Assuming straight out departure, no wind, and the altitude loss in the 180 turnback is offset by the runway portion you didn't use. I'm not clear what you mean by that. If my best glide is 85 KTAS and it loses 700 fpm at that speed, shouldn't I be guaranteed I can make it back if I climb at 84 KTAS and 701 fpm ? If by your statement above, you mean that the runway is long enough that if you can't turn back, you can land straight ahead, then of course your statement is trivially true. If not, how can you turn back from 10'? -- Alex Make the obvious change in the return address to reply by email. |
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![]() If by your statement above, you mean that the runway is long enough that if you can't turn back, you can land straight ahead, then of course your statement is trivially true. If not, how can you turn back from 10'? Do it the way the Space Shuttle does it (theoretically). If they have an abort between liftoff and 4 min 20 sec (I think), they are supposed to execute an RTLS abort (Return to Launch Site). Problem is that no matter what the situation is, they can't do squat until the SRB's are off the stack. Once those puppies are lit, your in for a 2 minute ride whether you want one or not. After the SRB's seperate, the shuttle is supposed to fly around with just the External Tank attached for long enough to burn up fuel and then they cut the engines (if there are any burning) and drop the tank, then glide safely home (again...theoretically). After the 4:20, I guess they file a missed approach and are diverted.....to SPAIN!!!! I truly hope that it is never required, but I've always wondered if this thing would actually work. We all know that the Shuttle has a glide ratio somewhere between my Ford Ranger and a brick 0, so it would be interesting to see how this thing would actually play out. I don't think this procedure is ever going to make it into our C150 POH's. But who knows. 100 years ago, we weren't supposed to be able to fly either. Hrmmm. "Introducing the all new 2067 Model Cessna 150, complete with your choice of Wheel Pants or JATO packs....." Jeff wow...sorry, way off topic........More on RTLS if you ca http://makeashorterlink.com/?G2B044B46 |
#9
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Not unless you are planning to glide straight ahead. You will lose a lot of
altitude in the turn. Mike MU-2 "Harold" wrote in message ... If a small single engine plane can out-climb its engine-out glide ratio from take off through the top of climb point, wouldn't it follow that it can always theoretically make it back to the departure airport in the event of engine failure ? Assuming straight out departure, no wind, and the altitude loss in the 180 turnback is offset by the runway portion you didn't use. If my best glide is 85 KTAS and it loses 700 fpm at that speed, shouldn't I be guaranteed I can make it back if I climb at 84 KTAS and 701 fpm ? |
#10
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"Harold" wrote in message .. .
If a small single engine plane can out-climb its engine-out glide ratio from take off through the top of climb point, wouldn't it follow that it can always theoretically make it back to the departure airport in the event of engine failure ? Assuming straight out departure, no wind, and the altitude loss in the 180 turnback is offset by the runway portion you didn't use. If my best glide is 85 KTAS and it loses 700 fpm at that speed, shouldn't I be guaranteed I can make it back if I climb at 84 KTAS and 701 fpm ? I have a close friend who was an experienced pilot (IFR rating - 6 years of flying - owned his own plane) and had engine failure on takeoff and did not make it back to the airport. He was practicing a short field take off which probably didn't help the situation but impacted terrain about 1/4 mile short of the runway (he hit power lines that were right next to this airport). Anyway, he died of injuries from the crash. The wing sheared during the impact dumping fuel into the cockpit and started a bad fire but fortunately death occurred upon impact. Reports placed him at about 700 ft of altitude when engine failure occurred but it could have been lower than this value. |
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