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       Thorp T-18
 
      
       
            
            The T-18 design was originally developed with the 
            Lycoming 0-290G (ground auxiliary power unit) in mind, by John 
            Thorp. Which was easily converted to a Lycoming 0-290D engine 
            producing 125 HP.  The T-18 is an all metal 2 place side-by-side 
            high performance aircraft. Control response is exceptional and 
            control forces are well harmonized. The T-18 is a very capable 
            cross-country airplane. It will carry 2 people, 80 lbs. of baggage, 
            and depending on engine and prop, can cruise around 180 mph. 
            Powerplants range from Lycoming O-235 (115hp) to IO-360 (180).  The T-18 was designed to be built from twelve 4' 
            x 12' sheets of aluminium ranging in thickness from 0.016 to 0.040. 
            Ribs and fuselage frames were designed to be hand formed with a 
            mallet over plywood form blocks. Simple aluminium angle extrusions 
            are used for stringers and longerons. The main wing spar caps are 
            made from 1/4 "U" channel on top and angle on bottom with flat sheet 
            for spar webs.  John Thorp designed the aircraft to be small, yet 
            strong with excellent take-off and climb performance. The landing 
            gear is a simple "A" frame of heavy wall 4130 steel tubing, heat 
            treated to 180,000 lbs./sq. in. and bolted to the firewall with (3) 
            3/8" bolts. The engine mount is also attached to the "A" frame 
            allowing landing stresses not to be transmitted directly to the 
            fuselage. This landing gear system has proven to be rugged and 
            durable. The T-18 incorporates the "flying tail" which John Thorp 
            held the patent for. This design also incorporates a sliding bubble 
            canopy, like a fighter style.  The T-18 is a very historic aircraft. It was one 
            of the first all metal homebuilts. It was the first homebuilt to use 
            the stabilator or all-flying-tail. The stabilator was designed by 
            John Thorp and was later used by Piper on their line of Cherokee 
            aircraft. Today you can see the extensive use of this design on 
            military aircraft. The T-18 was the first homebuilt aircraft to fly 
            around the world. It was also the first homebuilt airplane to fly to 
            both the geographic and magnetic north poles. The legendary Don 
            Taylor completed all of these feats in the early 1970's. His famous 
            T-18 is now on display in the EAA museum in Oshkosh, Wisconsin.   T-18 plans are available again through Eklund 
            Engineering. They are also developing a kit version, using laser cut 
            parts and of course John Thorp's matched hole tooling concept. The 
            laser cut parts are beautiful and it promises to be a wonderful kit. 
            For more information contact Eklund Engineering at: thorpt18@jps.net 
            or by phone at: (209)727-0318  No other homebuilt has done all the things that 
            have been done by this airplane. It is no doubt one of the best 
            designed aircraft in the world.  
             T-18 Designations / Models  T-18        The original design by John Thorp in about 1963
 T-18CThe original T-18 fuselage design, but incorporating Lu Sunderlands 
            new Convertible or folding wing. Plans were available through John 
            Thorp. The folding wing was a supplement to the original T-18 
            drawings. The plans were taken off the market in 1984 when John 
            Thorp retired.
 T-18W      Not many of these exist, but is the wide body version of the 
            fuselage as designed by Lu Sunderland, using the standard T-18 wing 
            platform. Plans were available through John Thorp. The wide body 
            modification was a supplement to the T-18 drawings. The plans were 
            taken off the market in 1984 when John Thorp Retired.
 T-18CWThis is the predecessor to the S-18. It is the wide body version of 
            the fuselage, and also the Convertible or folding wing as designed 
            by Lu Sunderland. Drawings were available from John Thorp and they 
            contained supplements for the fuselage and wing modifications. The 
            plans were taken off the market in 1984 when John Thorp retired.
 T-18LThis is my own designation for this model and I hope it will be 
            accepted. This model uses both the standard fuselage and the 
            standard wing plan form, but incorporates the LDS airfoil designed 
            by Lu Sunderland and used on the S-18. There are no actual drawings 
            for the "L" version, as builders have taken it upon themselves to 
            make the airfoil change.
 S-18This is the redesigned version of the T-18 by Lu Sunderland. A 
            complete new set of drawings were done and offered in 1985. It is 
            basically the T-18CW
 
             
              
               | specifications 
 
              
                | powerplant propeller
 length
 height
 wing span
 wing area
 seats
 empty weight
 useful load
 gross weight
 fuel capacity
 range
 | Lyc. HP Range180/125-180 x
 18.9 
                ft
 5.1 
                ft
 20.8 
                ft
 x
 2
 x940 
                lb
 x
 1500 lb
 29 gal
 500 n.m
 |  
            performance 
            
             
              
                | takeoff 
                distance, ground roll rate of climb
 max speed
 cruise speed
 landing distance, ground roll
 service ceiling
 | 1000 ft 1500 fpm
 210 mph
 201 mph
 1800 ft
 18,000+ ft
 |  
            limiting and recommended speeds
             
              
                | design 
                manoeuvring speed (Va) never exceed speed (Vne)
 stall, power off (Vsl)
 landing approach speed
 | x x
 60 mph
 x
 |  All specifications are based on 
            manufacturer's calculations
 |  |