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Aviation History
1986
1986 - 2151.PDF
110 All-speed CFRP aileron, operated by electrically signalled twin hydraulic servo jacks (aileron plus spoilers four and five act as load-alleviation function) 111 Electrical wiring raceways attached behind rear spar and through floor beams 112 Machined ribs and diaphragm, fixed leading-edge (Nomex core access panels on upper and lower surface) 113 Single hydraulic slal actuator 114 Slat torque driveshaft via angled gearboxes 115 Five-section leading-edge slat (conventional built-up metal) 116 Rotary slat actuator (two per section) 117 Titanium slat track 118 Track can, incoporporting condensation drains 119 Single hydraulic flap actuator 120 Inboard and outboard Fowler-type single-slotted flap 121 Flap centre-box made of CFRP, leading-edge CFRP and Nomex sandwich, trailing-edge aluminium honeycomb and skin (lightning protection) 122 Flap torque driveshaft via angled gearboxes 123 Rotary drive units 124 Inboard flap track and carriage 125 Outboard flap tracks and carnages 126 ap track i xward wing attachment lugs, ,r qr attachment on rearsp.-ir 127 CFRP flap-track fairings and attachment linkage 128 Engine bleed air to ECS. bled from 5th and 9th stage IP and HP compressors 129 Engine air precooler 130 Duel to air-conditioning pack (both sides) 131 Cooling ram-air intake to conditioning pack 132 Bleed-air duct for slat anti-icing 133 Bleed-air telescopic duct to "piccolo" tube (outboard only) 134 Inboard leading-edge ventilation, Naca intake (below) 135 Twin undercarriage wheels incorporating multi-disc carbon brakes (45in x 16m R20 tyres), four-wheel bogie units optional 136 Breaker strut and downlock actuator 137 Hydraulic retraction jack 138 Hydraulic bay and reservoir (three independent systems, plus ram air turbine) 139 Forward pylon/wing multi-lug attachment fitting 140 Thrust spigot 141 Rear pylon attachment 142 Integrally machined ribs 143 Front engine attachment and sway links 144 Rear engine attachment 145 Freon gas fire-extinguisher bottles (two per pylon) 146 General Electric/Snecma CFM56-5 turbofan 25.000 take-off thrust 147 Full-authority digital electronic engine control (Fadec) unit 148 Engine pylon services disconnect panel (both sides) 149 Engine slarting-air supply duct 150 Engine cowling intake anti-icing bleed- air duct 151 Hydraulically actuated thrust-reversing blocker doors 152 Rear engine core nozzle and cent re body 153 Hmced engine access doors (access to oil tank on leftside) 154 Engine cowlings (CFRP/aluminium alloy) built by Rohr France 155 IAE V.2500 turbofan 25,000lb take-off thrust with Fadec control (alternative engine) 156 Cascade-type thrust reverser and translating cowl "M50 CFM56-5 engine Undercarriage support rib FLIGHT INTERNATIONAL, 30 August 1986 Alternative engine IAE V2500 157 Inner fuel tank 158 Outer fuel tank (total capacity 15,588lit) 159 Surge tank 160 Overwing fillers (both sides) 161 Naca intake and flame arrester 162 Refuel coupling (standard option): refuelling panel in left rear wing fairing 163 Vent line from centre wing tank 164 Diffuser 165 Tank capacitators (four per wing) 166 Engine feed pipe 167 Fuel booster pumps (two per wing), situated between ribs one and two 168 Navigation lights (provision for strobe lights) 169 Landing lamps below lower wing shroud 170 CFRP static-discharge wicks © Business Press International Ltd 198* 89
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