- Joined
- Dec 29, 2015
- Messages
- 9,306
- Display Name
Display name:
Aztec Flyer
Not really. Stall on a single-engine Comanche is 53 knots, on the Twin Comanche it's 61 knots. 8 knots difference, to me, is not "a hell of a lot slower" even if you multiply by 1.3...
Plus, single-engine service ceiling (the thing most people focus on) is not an altitude which you can't operate above without both engines running. It's the altitude at which you can *climb* 50 feet per minute on one engine. Using a stock non-tip-tank-equipped Twin Comanche as the example, the single-engine service ceiling is 5800 feet, but the single-engine absolute ceiling is 7100 feet. But again, that doesn't mean that you can't fly above 7100 feet with one engine out. 7100 feet is the asymptote of your altitude vs. time after engine failure graph.
Let's say you're over the Rockies at 15,000 feet and lose one. You get it boxed up and trimmed for single-engine flight, and you will be coming down... But your "glide ratio" will be much better than that of a single because you do still have some power, and as you descend and gain more power, your "glide" is extended. Unless you're in a box canyon, you should be able to find yourself an airport before you meet the ground.
The difference in stall and landing speeds? No, not at all. I don't think that has hardly anything to do with the twin safety record - It's pilots who don't train, practice, and plan ahead for the engine failures that cause twins to have a less-than-expected safety record, not airspeeds.
I would also point out the single engine service ceiling figure is based on the airplane being in a clean configuration, critical engine inop, prop feathered, at gross weight. This last item is critical. I have just under 1900 lbs of useful load. Whenever I am going over the Divide I keep the plane light; it is never anywhere near gross. Thus actual single engine service ceiling is thousands of feet higher than the published at gross weight figure (the Aztec has a chart in the POH to calculate it).