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Aviation History
1986
1986 - 1417.PDF
~ ^z Moulded carbonfibre honeycomb core tailcone and fin structure Forward fin spar/fuselage attachment bolted to machined titanium fitting One-piece moulded, variable incidence tailplane (5' anhedral) Tailplane pivot point (titanium) Single tail-safe tailplane electric actuator Elevator control cables and bellcrank assembly Counterbalance spring and linkage Rudder cables and quadrant 66 Rudder trim-tab (fail-safe electrically actuated) 67 Upper rotating beacon 68 White rear position light 69 VHF nav (both sides) 70 Ventral fin panels (both sides) may be omitted on production aircraft 71 Tail over-rotation tail bumper 72 VHF No. 2 aerial 73 Pre-opening and closing main undercarriage bay door (Kevlar moulding) 74 Machined undercarriage pivot truss frames (two per side) 75 Drag brace strut and retraction jack 76 Wishbone and shock absorber strut 77 Main undercarriage single wheel (6.50in x lOin tyres) incorporating multi- disc carbon brakes 78 Hydraulic single-pack reservoir and pump 79 Electric fail-safe flap actuator BO Flap drive torque shafts 81 Single-slotted inboard flap screw jack actuator 82 Flap track and rollers (both sides) 83 Two-spar wing torsion box, stiffened by integrally milled stringer skin panels (sealed for tankage) 84 Tank inspection panels on lower surface U 68 TAILPLANE INCIDENCE <-11° FLIGHT INTERNATIONAL John Marsden AMRAeS Genoa '86 85 Machined front and rear spars 86 Web plate wing ribs 87 Left and right wing multi-bolt assembly forming continuous wing 88 Wing carry-through riveted to fuselage frames 89 Detachable aluminium leading edge 90 Leading-edge "piccolo" tube, thermal de-icing duct 91 Flap shroud (carbonfibre reinforced plastic) 92 Detachable moulded Kevlar wing tips 93 Navigation lights 94 Fowler-type outer wing flaps and rear vane (aluminium honeycomb skin) 95 Torque driveshaft and universal couplings 96 Screw-jack and flap actuators 97 Machined flap tracks 98 Track/wing attachment brackets FLIGHT INTERNATIONAL, 21 June 1986 99 Flap carriage and roller assembly 100 Kevlar flap track fairings 101 Fuel tank end ribs (246 US gal. Total fuel capacity 416 US gal) 102 Aileron-control changeover quadrant from cable to linkage 103 Aileron-control brackets and push-pull linkage 104 Aileron actuating crank and rod 105 Aileron trim tab (fail-safe electrically actuated) 106 Aileron aluminium honeycomb panels and ribs with built-in rubber aerodynamic seal 107 Pratt & Whitney PT6A-66 800 s.h.p. turboprop engine 108 Hartzell 85in-diameter fully feathering and reversing constant-speed propeller, Kevlar reinforced plastic blades, de-iced by engine exhaust (shown feathered) 109 Area-ruled spinners 110 Propeller pitch and synchronisation control units 111 Exhaust ducts 112 Engine fuel injectors 113 Stainless steel firewall 114 Support frame and engine isolators 115 Engine air intake (cowling forms plenum chamber) Fire extinguisher bottle (one per engine) Machined titanium engine support frames 118 Engine support steel truss thrust members Truss/wing attachment lugs Area-ruled Kevlar moulded engine nacelles Engine air intake with built-m-inertial ice separator 122 One-piece moulded bifurcated intake duct 123 Internal dual-vane electric actuator 124 Nacelle upper venting panel 125 Generator air cooling duct 126 Wing ice inspection light 127 Engine intake deicing not finalised (may be thermal or electric) 128 Static electric discharge wicks (glassfibre) 116 117 119 120 121 45 © Business Press International Ltd 1986
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