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Aviation History
1986
1986 - 1416.PDF
• u 49 Electrical bay, housing NiCad 25V 38Ahr battery and generator controllers 50 Lockable baggage compartment door (27inx27inapprox) 51 Fully lined baggage compartment (60ft3) 52 Rearfuselage structure, built-up frames and stringers 53 Ram-air intake (Naca duct) to heat exchanger (right side) 54 Heat exchanger and pre-cooler 55 Water separator 56 Engine bleed-air duct to ECS system via control valves 57 Overboard air outlet duct (below aircraft) 1 Carbonfibre honeycombe-cored nosecone housing Collins WXR-250 weather radar and glideslope aerials 2 Avionics bay 3 Pitot head (electrically heated, below foreplane, both sides) 4 Fixed one-piece foreplane (anhedral 5°) 5 Foreplane attachment lugs (adjustable incidence for flight testing) 6 Foreplane flaps lowered electrically with wing flaps 7 Dual electric foreplane flap actuators 8 Two-piece windscreen, production version (electrically heated) 9 Fully shrouded Efis instrument panel 10 Dowty stoerable nose undercarriage (5in x 5in tyres) 11 Hydraulic retraction jack 12 Breaker strut 13 Landing and taxi lamps 14 Forward pressure bulkhead (canted forward) 15 Two-piece passenger door and combined steps (24in x 57in) 16 Dual control columns with autopilot disconnect press buttons 17 Rudder pedals with toe-brakes 18 Centre console with power and propeller levers 19 Fully adjustable crew seats 20 Circuit-breaker panels (both sides) 21 Rolled fuselage frames and longerons 22 Window belt outer skin 23 Inner skin pressings 24 Stretch-formed, compound-curve fuselage panels 25 Emergency oxygen bottle (22ft3) below seats 26 Pull-in emergency exit 27 Cabin insulation blankets 28 Seven-seat passenger cabin (six recline and swivel) c^^E5L FLIGHT INTERNATIONAL, 21 June 1986
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