This is the radio controlled, electric powered, foam construction
              GWS-262 Airplane Kit with the EDF64 Brushless Power System.
                            For Advanced Pilots.

FEATURES: Construction: White colored foam wing and tail sections with two-
            piece fuselage
          Wings: One piece, foam construction
          Radio Component Placement: Accessible over wing
          Power System: EDF64 with preinstalled Gray ducts and wiring harnesses
          Landing Gear: .08" (2mm) diameter prebent main and tail wire
            prebent wire
          Wheels: Foam, two 2" (51mm) diameter main, 1.75" (38mm) tail-ultra
            lightweight design
          Hardware: Included
          Aileron Control: Dual servo
          Warranty: GWS, guarantees this kit free from defects in both
           materials and workmanship at the date of purchase

INCLUDES: Foam wing and tail sections, 2mm diameter wire landing gear, three
            ultra light wheels, clear plastic nose cone, decals, two-piece
            fuselage, power Y-harness, hardware and instruction manual

REQUIRES: Speed Control: Two GWESC 25A (GWSM2201) or 25A equivalent
          Battery: 11.1V 1300-2200mAh LiPo
          Charger: Lipo Compatible.
          Radio: 3-4 channel with four micro servos  (1-elevator,
            1-rudder, 2-aileron)
          Y-Harness: One for aileron servos
          Building and field equipment

SPECS:    Wingspan: 41.34" (1050mm)
          Wing Area: 263.5 sq in (17 sq dm)
          Weight: 24.7 - 27.9oz (700 - 790g)
          Wing Loading: 13.5 - 15.3 oz/sq.ft (41.2 - 46.5 g/sq.dm)
          Length: 33.6" (853mm)
          Airfoil: Flat bottom, low wing placement
          Center of Gravity: 3.1" (80mm) behind leading edge of wing
          Control Throws-
            Elevator: Up & Down 30-35°
            Aileron: Up & Down 30-30°
            No range given for rudder

COMMENTS: Other kits in this series include;
             GWSA1201 Slope Glider

                                                                    jxs 5/03/07
                                                                         ir/jxs
                                                                 UPD OA 6/25/07