I flew a Seeker in Albuquerque, New Mexico, with John Winship, a retired Alaskan bush pilot who is Seabird Aviation America’s demo pilot. His first question was whether I had tailwheel experience. I do, but you would never have known it. The Seeker sits quite low to the ground — though it seems high when you’re trying to climb in — and the sight of the pavement approaching at 60 knots just beneath my feet made me flare high repeatedly. The Seeker is no floater; and each time I cut the power and started to round out two or three feet too high, it simply settled out from under me. I managed only one semiacceptable landing; the others were humiliations to me, tests of Winship’s self-control, and demonstrations of the fortitude of the spring-steel landing gear.
With a little more practice, I suppose that I could have landed the Seeker as nicely as the next pilot; once planted, it rolls out straight with no tendency to groundloop. What I could not have done is fully stall or spin it. With drooped leading edges on its outer panels, the Seeker only half-stalls even with full up elevator. There is a good reason for this trait: In its role as a low-altitude observation platform, it is subjected to the kind of distracted piloting that can produce an inadvertent stall.
The drooped leading edges with their sharp break at midspan are one aerodynamic refinement that came to the design about 10 years ago. Another is the truncation of the flaps at the outer edge of the propeller disc, intended to provide sufficient space between wing and prop to “smear out” the wing wake and thereby reduce the interactions that produce noise and vibration. With very little fuselage side area behind the CG and strongly curved cabin sides, which tend to be destabilizing, the airplane must originally have been somewhat shy of directional stiffness. Small fins near the tips of the horizontal stabilizer and long strakes below the tail boom help supply whatever authority the vertical fin, immersed in a destabilizing propwash, lacks. Most unusual and ingenious, however — and a Don Adams suggestion — is a small vane pivoting on an arm beneath the cabin. Mechanically linked to the rudder, it acts like a yaw damper, counteracting any sideslip. Nevertheless, the Seeker’s Skyhawk-like surface-hinged ailerons still produce a fair amount of adverse yaw in feet-on-the-floor turns.
The 44-inch-wide cockpit is fairly spacious, with twin sticks and with the engine and flap controls on a low console between the two occupants. The doors consist of a large upper section and a smaller lower one; the upper, but not the lower, can be removed for flight. Getting aboard is a bit unusual; you swing one leg up into the cockpit, get one buttock on the edge of the seat, and then haul yourself aboard with a handgrip on the upper window frame. It’s not pretty, but it builds character.
On takeoff and climb the Seeker, though at a bit more than 1,300 pounds empty it is not a heavy airplane, was quite sluggish. Winship explained why. In Australia, low-compression pistons (for mogas compatibility) and a 2,500 rpm redline (for noise compliance) derate its 180 hp carbureted Lycoming to 160 hp. The airplane I flew had come to America with those limitations. Albuquerque’s 5,000-foot density altitude brought the power down still further, to 135 hp or so. The standard fixed-pitch prop doesn’t help. American versions — which will be assembled here, after being manufactured and flown in Australia, and will have a U.S. Normal-category type certificate — will use a bored 390-cubic-inch version of the Lycoming IO-360. Rated at 210 horsepower, the new engine will bring the power loading down to 10 pounds per horsepower and should add 600 fpm or so to the rate of climb across the board.
The reasoning behind the Seeker’s design is that many of the jobs performed by helicopters don’t actually require vertical landing and takeoff or stationary hover at altitude; they take place near airstrips or roads and can be performed more economically by an airplane with similar visibility and a low loiter speed. Many airplanes can fly low and slow, but they lack helicopters’ unimpeded forward visibility and the ability to mount sensors, cameras, searchlights and the like under the nose. What sets the Seeker apart is its physical similarity to a helicopter; equipment designed for helicopter use can be mounted on a Seeker without modification.
The bottom line is, of course, the bottom line. At a projected price of $350,000, the 210 hp, glass-cockpit version of the Seeker falls between the Robinson R-22 and R-44. It’s the operating costs that are different, starting with insurance and culminating in the helicopters’ major rebuild — $71,000 for the R-22, $123,000 for the R-44 — at 2,200 hours, an expense that the fixed-wing airplane escapes entirely. Over the long term, the Seeker’s operating costs, as laid out for me by Seabird America director David Boland, work out to half those of the R-22 and a third those of the R-44.
A niche design that has gone through several major revisions and had a lot of time to mature, the Seeker is that rare bird, an airplane that doesn’t look like all other airplanes. It makes a lot of sense to me; it will be interesting to see whether the pipeline-surveyors, reindeer-counters and border-patrollers of this world agree.
