SF 260 MARCHETTI!!
SF260TP-3 SHIP

KICKIN' BUTT IN THE SF260C AND TURBOPROP 260!
Text and photos by Budd Davisson, Air Progress, '78 (or so),


 
PAGE THREE

Lined up and ready to go, I wrapped one hand around the base of the throttle lever and moved it smoothly up towards the stop. With 260 horses on tap, the little Italian is more than eager to reward you with really excellent acceleration. Interestingly enough, it was slightly less than I was used to in an A model. We racked the airspeed indicator up to 60 knots almost immediately and a gentle tug on the stick got the nosewheel off the ground, running on the mains for a short distance until we reached a speed that made that highly tapered wing happy.

geardown 260
SF260 gear is sensitive to rigging and a lot of them have wound up on their noses

Off the ground, I made a mental note to pull out on the gear handle before bringing it up. It's easy to tug at the handle, thinking you have retracted the gear but still have three lights glaring at you. This is one of the better gear retraction systems I have worked with because you really have to work to accidentally get the wrong lever on landing. Takeoff flaps are 15 degrees and once you have airspeed over 90 knots (which is almost as soon as your gear is up) you can bring them in with no fear of settling.
 
Although best rate of climb is somewhere between 90 and 100 knots, I found it much more comfortable to climb out at 110 knots indicated because it gave a much flatter nose attitude and better visibility. Even so, we were going upstairs at well over 1,000 feet per minute. At max rate of climb, it's not unusual to see climb rates from 1,500 to 1,700 feet per minute.
 
ONE OF THE FIRST THINGS I NOTICED WHEN taking off in the turboprop the weeks before was the lightness and quickness of the ailerons, so I was prepared when flying Sterbutzel's airplane. The original A models had quick response but fairly stiff ailerons; not enough to be objectionable, but enough so the breakout forces kept you from doing much meandering away from dead level flight. The story being circulated in SF.260 circles is that some air force wanted to fly the SF.260 with hard hats which required them to lower the seats by several inches. This put the stick up at nose level so they shortened the stick a corresponding amount which reduced the mechanical advantage making the ailerons unacceptably heavy, so the factory designed a set of servo-tabs to lighten the forces. Whether the story is true or not, the bottom line is the 260 C has quite light breakout forces and still has the excellent response of the A model, making for a truly joyous combination. In fact, the combination is so nice it was all I could do to wait until I reached legal altitude and airspace before I started rolling left and right.

 
As with the jet aircraft the 260 is supposed to emulate, the adverse yaw is absolutely zero. In fact, you can jerk the nose up to 20 degrees and put your feet flat up on the floor while jamming the aileron into the corner to produce a perfect aileron roll. I found you could roll from virtually any speed and the extremely clean airframe would let the nose up to indecent angles when doing huge barrel rolls right and left, bleeding one into the other like giant figure eights.
 
I had no idea what the proper entry speeds were for loops, but dropping the nose slightly to get 170 knots indicated seemed to produce a loop that was a might bit slow on the top although the 260 gave no indication of unloading on me and half-snapping around right side up. As long as I didn't put on G when slow, the plane seemed to know exactly where it was going.
 
Shepard had crawled alongside of us by this time in his A model, and we thought we'd see what the C model had given away with a new wing design. We found that almost regardless of the speed, Shepard would indicate a full 2 to 21/2 inches less in manifold pressure. The C model would indicate 160 knots at 23 inches and 2,400 rpm and Shepard was loping along at a mere 201/2 inches. John Stirling had brought one of the airplanes across the Atlantic with Mike Moore and he agreed with Moore that you could flight plan the C models at 165 knots and be fairly sure of getting it. Shepard, on the other hand, said he'd flight plan at least 10 knots faster than that.

What did the 260 gain in modifying the wing? The only way to find that out was to bring the power back and haul the nose up to see how the airplane performed at the low end of the speed spectrum. Letting the speed come down to around 75 knots, I continued holding the nose up until I could feel a sizeable buffet building up. I continued bringing the stick back and, at some number in the vicinity of 60 knots, the stick hit the stop and the airplane dropped its nose and rolled gently off to the left. I tried that several times and then Stirling said, "Let me show you something." Taking the airplane, he flew straight ahead into a stall and as the aircraft stalled, he pulled the stick to the stop and kept it there, keeping the wings level by ailerons with no difficulty whatsoever. This was an entirely different airplane from the A model in that regime. In the same situation, the A model has no ailerons. In fact, a knot or two before the A model stalls, you can't assume you'll have enough aileron for you to pick up a wing should it drop. Also, the stall in the A model is much less predictable and more likely to bite you. I took the C model into accelerated stalls in turns while sliding the ball inside and outside and the aircraft performed exactly as you would expect from any other airplane. Although slower at the top end, the 260 C definitely has much better manners than its predecessors, something which makes a much better primary trainer and certainly brings the C closer to being an everyman's airplane.
 
The question of which is better, the blood and guts "A" model or the more refined "C," is a matter of taste and mission. There's a very slightly different feel on the C model, an indescribable one, that would possibly only be noticeable to one who has flown the airplane a few hours: the A model somehow seems a little more solid and more sure of itself, however, that may be purely a perceptive difference brought about by the tighter ailerons. The C model definitely has the A beat all to pieces in the roll department, and of course its low speed characteristics are so much different it might as well be a different design.

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