![]() |
If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below. |
|
|
|
Thread Tools | Display Modes |
|
#1
|
|||
|
|||
![]() "jan olieslagers" wrote Opinions are plenty, and cheap... But you asked, so here goes: The single-engine rate-of-climb seems little relevant to me. I always understood if one engine quits, the mission is to come down safely, not to go up. One of the biggest reasons that some people choose to pay for buying and running an extra engine is so that they do not have to come down, in places like over cold, killing water, and hard granite mountains at night. So that means it can perhaps do one mission, partway. It should be able to stay up over the ocean, with only a light load, perhaps. Rule out higher large bodies of water. For sure, rule out mountains in the night, and with a full load, hills in the night, too. Why bother with a twin, (paying for an extra engine, and its maintenance, and feeding) if you have to crash in those types of bad places, just like a single? Shoot, even worse, with two engines, you double the odds that one will fail! -- Jim in NC |
#2
|
|||
|
|||
![]()
"Morgans" wrote in message
... "Rich S." wrote Isn't that about like a DC-3? Now *there's* a failure as a design! ![]() Is that so? Fuel load for around 4 hours of flight, and only one pilot on board, and it can only do 400 FPM at 3000 feet? Dunno. I would have thought it better than that. I have to get up the road this morning so's I can do some praying, so I don't have time to look up the engine-out specs on the DC-3. You could probably find them he http://www.centercomp.com/cgi-bin/dc3/gallery?25000 or he http://www.douglasdc3.com/index.html See ya, Rich S. |
#3
|
|||
|
|||
![]()
On Jan 27, 12:32*am, "Morgans" wrote:
Anyone else have an opinion on the subject? Yes, and unlike yours it's an informed opinion. 400 fpm climb at 3000 ft lightly loaded is normal performance for a light piston twin. Single engine service ceiling for a twin is defined as the maximum altitude where it can maintain a 50 fpm (not 100 fpm) rate of climb. Most normally aspirated light piston twins have a single engine service ceiling in the 4000-8000 ft range. The bigger ones can boast impressive single engine performance when lightly loaded - but you will pay for it with horriffic fuel burn. The performance may seem marginal, but in fact the only time the performance is marginal is when the engine failure occurs in the climb, before a reasonable (not necessarily planned) cruising altitude is reached. Driftdown is part of the knowledge any twin engine pilot operating in anything other than flat, low terrain needs. Remember that if you are only climbing at 50 fpm at 4000 ft, then you are probably only descending at 100 fpm at 7000 while doing 80+ kts. Reaching an airport and being able to shoot an instrument approach becomes something dependent only on pilot skill and planning, not luck. In the flatlands, it's just skill - no advance route planning for driftdown required. Over water? Now you need to understand the ETOPS concept and specific range. For a pilot with the limited knowledge, training, and skill enjoyed by the typical private pilot, the second engine of a twin is probably of little or no value - certainly not enough to offset the liability of a doubled chance of engine failure. The performance is simply too marginal. That's why twins aren't statistically any safer than singles. For a well trained pilot, there is plenty of performance there to turn a forced landing somewhere (not so fun if dealing with night, low cloud, rough terrain, overwater, or some combination of these factors) into a landing on an airport. But hey, what do I know. Well, maybe a little. Having lost an engine miles from any airport, over forests, in a twin with that sort of performance, in IMC, I am still here to talk about it - because in spite of the ice I picked up (which further degrades performance) when I could no longer remain above the icing altitudes, I completed an ILS approach and normal landing on an airport, repaired the fuel system, and flew home the next morning. How do you suppose I would have fared in a single? Well, with luck I might have fared as well as my friend who lost the only engine in a Bonanza in IMC. No icing, daylight, and the bases were pretty high (1500+ AGL). He picked a field when he came out of the bases (he wasn't within gliding range of an airport) and put it down in the best field available. The plane was destroyed, but he managed to escape with only minor cuts and bruises. He knows he was lucky. Some of us prefer not to rely on luck, but feel comfortable relying on skill. That's why I'm still flying a certified airplane - because nothing homebuilt with two engines comes close to the comfort, performance, and economy of my 1965 Twin Comanche. Michael - ATP, A&P, etc. |
|
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
Twin engine prop rotation? | Chris Wells | General Aviation | 12 | December 19th 07 08:52 PM |
FAA To Change Twin-Engine Airliner Regulations | Larry Dighera | Piloting | 6 | June 13th 06 12:30 AM |
Twin Engine Cessna 172 crashs :) | Robert M. Gary | Piloting | 3 | August 19th 04 04:17 PM |
Twin Engine Cessna 172 crashs :) | Robert M. Gary | Piloting | 2 | August 19th 04 01:13 PM |
pressurized twin-engine, 16 to 19 seats buy | Federico Prüssmann | Owning | 0 | September 25th 03 06:44 PM |