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#11
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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 ? |
#12
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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 ? |
#13
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dennis wrote:
snip 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. After getting my private, I was wondering about this, particularly because the airport I usually fly out of (PDK) is surrounded by development that leaves no place, at any time of day, to even dream of setting down safely in the event of an engine failure. Not getting answers that satisfied me, I went out and did some tests myself, at altitude. Used GPS, a partner to log altitudes and waypoints, etc. Came to the conclusion that if everything went *perfect*, and you *knew* it was going to happen, it would take 500' agl to make it back, in a Warrior. But what I did was pick the brains of my friends who were glider pilots, worked on Vms turns, high bank angle turns, popping 10 degrees of flap for the turn and popping it out for the glide, etc., etc. After practicing all that, and knowing what was coming, 500' was the best I could do. Which to me means 800'-1000' in real life, if you practiced it a lot. It was an eye-opener for me to see how little margin for error I have operating out of PDK. It has changed my standard departure. I climb at Vx to pattern altitude, just to gain the most altitude while I'm still within reach of the airport boundaries. The one good thing about PDK is it has 4 runways aligned 3 different ways, and lots of taxiways and ramp space between them, so just getting back to the airport itself you have a better chance of putting it down safely, if not on a runway. Plus the crash trucks don't have as far to go. :-) -- 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 |
#14
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David Hill writes:
After getting my private, I was wondering about this, particularly because the airport I usually fly out of (PDK) is surrounded by development that leaves no place, at any time of day, to even dream of setting down safely in the event of an engine failure. 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. To take a real-world example, an instructor taking a sightseeing flight out of Buttonville (near Toronto) had an engine failure over solid development, so she set the plane down deliberately in a grove of small trees on the front lawn of the IBM plant. The trees smashed up the plane nicely, but in doing so, they dissipated enough energy that she and her passengers walked away. Here's the story (with photo): http://www.thestar.com/NASApp/cs/Con...l=968793972154 I read afterwards that she went back to work later that day. All the best, David |
#15
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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. |
#16
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David Hill wrote:
dennis wrote: snip After getting my private, I was wondering about this, particularly because the airport I usually fly out of (PDK) is surrounded by development that leaves no place, at any time of day, to even dream of setting down safely in the event of an engine failure. 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". Another engine fail on takeoff landing here was at night into a park full of mature oak trees. Front seat guys were seriously banged up, but they also were not wearing seat belts. Three rear seat pax, also unbelted, received minor injuries. Tom Pappano, PP-ASEL-IA |
#17
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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. |
#18
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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. |
#19
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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 ? |
#20
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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. |
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