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Best/Worst Single Engine Performance

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Regul8r

Old School
Joined
Aug 18, 2005
Posts
709
I've heard that on paper, the Twin Beech has the worst single engine performance of any Twin out there. Any other thoughts or opinions?
 
The Baron 56TC is one of the best-23000' single engine service ceiling.
As far as the worst, what about the old Apache? Hydraulic systems all on one side? Never flown one, but I'm sure somebody that has will have something to post here.
 
Yeah, those early model Aztecs had the same deal with the hydraulics on the left side. It would be a handful trying to pump the gear up w/ the left engine out at gross weight shortly after T/O
 
Regul8r said:
I've heard that on paper, the Twin Beech has the worst single engine performance of any Twin out there. Any other thoughts or opinions?

I dunno...when I trained in one in So TX last year, temp was in the mid-80's F, we were about 150lbs under gross, and engine failures as soon as the gear switch was selected "up" didn't require immediate landing. It woulda' been a WIDE pattern back to land, however ;)

Fly safe!

David
 
I thought the Seminole was one of the worst single-engine performers out there. Sure seems like it on a hot day.
 
I flyw Aztecs 14 years, as a personal aircraft, and feel they have good single engine performance. The gear on the Aztec is not that much drag, but they will not climb with flaps down. The 250 HP engines and big wing give much better single engine performance than the twin Comanche. The C-421 I flew at gross on a hot day could only do 600 FPM on both engines! The B-200 does good on one engine and the Cheyenne II has a section in the AFM for single engine take off.

HEADWIND
 
Engine out

Hands down the Champion Lancer 402-engine out 150 neg. rate of climb. I instructed in one back in the 60's.

Google Champion Lance and take a look at this pig.

Mobie
 
How about the Cessna Bobcat/T50/UC78/Bamboo Bomber? As I recall the props were fixed pitch and therefore could not be feathered.
 
Ultraman said:
How about the Cessna Bobcat/T50/UC78/Bamboo Bomber? As I recall the props were fixed pitch and therefore could not be feathered.

Did that have the 300hp engines in some models?
 
I was going to suggest the 150HP Apache until I heard of mobie's Champion Lancer. At least the Apache would hold altitude if you were below 5,000 feet.
 
Regul8r said:
Did that have the 300hp engines in some models?



To my knowledge they all had 275hp Jacobs.
 
I fly a Twin Beech 5 nights a week hauling cargo. I would say that the single engine performance is a bit lacking but not exactly worthy of the reputation it seems to have gotten. I will say it is not forgiving and does not have the performance margins to allow for sloppy technique or improper handling. Like any other twin if it is handled right it will perform as predicted. When it is not it will bite you square in the butt.
 
Don't know why anyone would want to do a single engine take off in a Cheyenne II, but like I said there is a section in the AFM. The point I was trying to make is that if it is certified for single engine take off it must have good single engine performance. The Cheyenne II is a Navajo (which had 2 310 HP engines) with 2 620 HP engines.
 
Headwind said:
...the Cheyenne II has a section in the AFM for single engine take off.
Huh? I flew one for 3 years and don't remember that in the AFM. (However, the last time a flew one was in 1988. I could have forgotten that section in the AFM, but I tend to remember "minutia" like that.) Its performance was good, but I doubt if it was that good.


I flew a Baron 56TC for about a thousand hours. That airplane had far and away the best single-engine performance of any propeller driven twin - piston or turboprop - that I've ever flown.

Regul8r...
With the possible exception of the Baron 56TC, the single-engine performance in any piston-powered light twin is abysmal. Loss of power is the primary culprit. Remember, normally aspirated aircraft lose power with altitude. An aircraft's climb ability is directly proportional to the amount of "excess" power that it has available vs. what is needed to maintain level flight. For example, if a 200 HP normally aspirated airplane requires 100 HP to maintain level flight it would (at SL, ISA day) have 100 "excess" HP to use for climb. At 10,000' MSL, the engine might only be able to produce 130 HP, leaving it with a 30 HP surplus. This is the reason why turbocharged aircraft perform so well - you would be able to maintain SL power up until you reached the "critical altitude" for the particular engine. In some cases, this can be as high as 18,000' MSL.

This is also why light twins typically perform so poorly on one engine. Take, as an example, a Twin Comanche with two 160 HP engines. If that airplane required, say, 150 HP to maintain level flight it would have 170 "excess" HP to climb with. If it lost an engine, it would have lost 50% of its available power, but with just 10 "excess" HP, it may have lost 95% of its ability to climb. This, of course, will also apply to the Baron and all other light twins. If you only learn one thing from this post, it should be that light twins have two engines because they need two engines.

If you're in a single and you loose the engine, the laws of physics dictate what will happen next. Leaving the gear down until you have no more "usable" runway left only makes sense. It will leave the airplane in much better condition should the engine decide to pack it on while you're still over the runway. I've seen some "hotdoggers" rotate and immediately suck the gear up. A while back, I even heard of a guy who would place the landing gear in the up position as he took the runway. His thinking was that the squat switch would keep the gear from coming up while the airplane was on its takeoff roll and immediately start the retraction process as soon as he broke ground. What a weenie - his practice came to light one morning when he rotated a bit too early and the airplane settled back onto the runway. You don't need a PhD in Physics or Aeronautical Engineering to figure out what happened next.

(By the way, these are usually the same guys who immediately pull the throttle back to climb power as soon as the gear is in the wells. Statistically, that's the time when you’re most likely to have an engine come apart.)

Multi-engine aircraft are an entirely different matter - you want to get the airplane cleaned up as soon as possible. In the case of most piston twins, their ability to maintain controlled flight depends upon the pilot getting the gear up, the propeller feathered, and the flaps up. Failure to this often results in the airplane being turned into a lawn dart.

We tend to take engine reliability for granted, but I believe that this is a very dangerous thing to do. Most light twins simply won't maintain altitude with a windmilling propeller and/or the gear down. The old Metroliners had a rocket bottle in the tail to buy the flight crew enough time to get the gear up in the wells. Auto-feather systems are on most, if not all, turboprop twins. The manufacturers wouldn't put up with the increased costs and complexity of doing this if there wasn't a true need for it. They put this stuff on the turboprops that have significantly better single-engine performance than piston-twins. It really ought to be on the "little" twins, but with the exception of the new diesel-powered TwinStar, no one is willing to pay for it. Like I said, light twins lose up to 90%+ of their climb capability. The figure is probably even higher than that - I've seen several non-turbo'd twins that wouldn't climb out of ground effect and several turbocharged twins that could barely achieve climb rates of 100 fpm or so. But never the less, the point is that twin engine aircraft have two engines because they need two engines and under certain conditions they can maintain controlled flight on one engine IF THE PILOT DOES EVERYTHING RIGHT. You don't have time to dawdle, it has to be done right and right now.


'Sled
 
Last edited:
Headwind said:
Don't know why anyone would want to do a single engine take off in a Cheyenne II, but like I said there is a section in the AFM. The point I was trying to make is that if it is certified for single engine take off /quote]

Oh, I WANT to do it. Sounds like fun.

SHOULD I do it? MAY I do it? CAN I do it? Mmmm.

Just bring the power up very slowly and get yourself a very long runway. Wide would help too.
 

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